TW539933B - Controller for optical scanner - Google Patents
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- TW539933B TW539933B TW90129323A TW90129323A TW539933B TW 539933 B TW539933 B TW 539933B TW 90129323 A TW90129323 A TW 90129323A TW 90129323 A TW90129323 A TW 90129323A TW 539933 B TW539933 B TW 539933B
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539933 經濟部智慧財產局員工消費合作社印製 A7 B7 五、發明説明(1 ) 【發明所屬之技術領域】: 本發明係關於具有角度檢測裝置,並於旋轉軸之周圍 上決定支撐於旋轉軸之鏡子之位置之光學掃描機之控制裝 置。 使用於雷射標記及印刷電路板之雷射開孔加工等之光 學掃描裝置,以內藏之電動馬達將裝設於旋轉軸之鏡子加 以旋轉,藉由改變鏡子之角度,將從雷射振盪器所輸出之 雷射光照射於被加工物之所定之位置。 【先行技術】: 第1 2圖係顯示光學掃描裝置中之可動部分之構成圖 。鏡子1 1裝設於旋轉軸1 2之一端。旋轉軸1 2則藉由 則藉由軸承1 4及軸承1 5被加以支撐,以與旋轉軸1 2 爲一體之移動線圏1 3來接受驅動轉距(Torque )並加以旋 轉,其位置並被決定於所定之位置。以下將一同旋轉之鏡 子1 1及旋轉軸1 2及移動線圈1 3合稱爲光學掃描機1 〇 於光學掃描機1中,設置了圖中所省略之檢測旋轉軸 1 2之旋轉角度之角度檢測感應器,例如可變容量型感應 器。可變容量型感應器係以,裝設於旋轉軸之介電體之平 板於兩枚一組之固定極板之間與旋轉軸一同旋轉之方式加 以構成,而旋轉軸之角度則做爲靜電容量之變化由電氣訊 號加以檢測。關於可變容量型感應器之技術可參考例如美 國專利第3 5 1 7 2 8 2號公報及美國專利第 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) ^ 裝 ; 訂 . (請先閲讀背面之注意事項再填寫本頁) -4 - 經濟部智慧財產局員工消費合作社印製 539933 A7 1 ' ___ B7 五、發明説明(2) 4864295號公報以及日本特開平7 — 55500號 公報。 此外,於日本特開平4 一 1 2 7 9 8 1號公報中,公 開著藉由將角度測定用雷射照射於鏡子並將該反射光以線 性感應器加以檢測,並將鏡子角度加以回饋控制之技術。 再者,於日本特開昭6 3 — 1 4 7 1 3 8號公報中,公開 著將反射面形成於將鏡子固定於旋轉軸之零件(鏡框), 藉由以受光元件檢測來自於反射面所反射之發光元件的光 ,以決定鏡子之位置之技術。 第1 3圖係爲光學掃描機之控制碍塊圖。爲了將角度 檢測訊號2 2負向回饋至由上位之控制裝置所指定之角度 目標値訊號2 Γ,並使常態中之偏差訊號2 3設定爲0, 將偏差訊號2 3以積分補償電路2 4進行積分。此外,爲 了保持此伺服機構之安定性,將角度檢測訊號2 2輸入於 比例補償電路2 5及微分補償電路2 6,從積分補償電路 2 4之輸出訊號中將這些電路之輸出訊號之和進行減算, 並設定爲控制輸入訊號2 7。而馬達驅動電路2 8係將與 控制輸入訊號2 7成比例之馬達驅動電流2 9供給至光學 掃描機1。馬達驅動電流2 9於移動線圈1 3中流動,並 於移動線圈1 3中產生與電流値成比例之驅動轉距。 於藉由雷射光針對印刷電路板進行開孔加工之情況下 ,爲了於精細之電路圖上進行精密加工,有必要將用於加 工之雷射光之位置決定之誤差降至約1 0 A m以下。此外 ,爲了降低加工時間,有必要求得從開1個孔之後進行下 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) ' -5- ^ 裝 „ 訂 . (請先閲讀背面之注意事項再填寫本頁) 經濟部智慧財產局員工消費合作社印製 539933 A7 ‘ B7 _____ 五、發明説明(3) 1個開孔加工之動作之高速化,例如,於每秒開1 〇〇0 個孔之情況下,有必要將孔間移動時間降至平均1 m S未 滿。 而雷射光有其能量分布,並以具有廣泛面積射入於鏡 子1 1。因此,爲了進行高品質之開孔加工,鏡子1 1最 好是較大(面積較廣)一些。 然而,若將鏡子1 1變大的話,則旋轉軸1 2之扭轉 振動及彎曲振動將會變大,並阻礙了鏡子位置決定之高度 應答能力。 首先,關於扭轉振動之影響加以說明。因爲鏡子1 1 變大的話,旋轉軸1 2之周圍之慣性扭矩(Moment)亦隨 著增大,因此旋轉軸1 2之扭轉彈簧之扭轉振動的固有振 動數亦會降低。而扭轉振動1次模式爲固有振動數最小之 扭轉振動,於旋轉軸1 2之長形方向存在著1個扭曲的節 點,夾住此節點之兩側互相以逆相位來產生角度位移。此 外,扭轉振動2次模式爲固有振動數次低之扭轉振動,於 旋轉軸1 2之長形方向存在著2個扭曲的節點,針對夾住 此2個節點之中央部位,兩側之部位係以逆相位來振動。 例如,於鏡子的旁邊配置著角度檢測感應器之情況下 ,藉由將扭轉振動的節點設置於角度檢測感應器與移動線 圈1 3之間,使得兩者形成逆相位。於此情況下,於上述 之伺服機構中,角度檢測訊號2 2之振動數成分變成正向 回饋,產生不安定之控制。從鏡子位置決定之高度應答會g 力與低頻率外部干擾之抑制特性來考慮,雖然控制頻寬最 ^氏張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) I — ;------^裝 I----:---訂-------AW (請先閲讀背面之注意事項再填寫本頁) -6- 經濟部智慧財產局員工消費合作社印製 539933 A7 B7 五、發明説明(4) 好是愈寬愈好,但是因扭轉振動數而使控制頻寬被限制。 此外,於扭轉振動之節點與感應器之位置重疊或是極 爲接近之情況下,因爲無法以角度檢測感應器來觀測其振 動模式,因此無法進行控制的安定化,使雷射光之位置決 定精密度降低。 接下來針對彎曲振動之影響加以說明。第1 2圖所示 之光學掃描機中之可動部分最好是於旋轉軸1 2之周圍維 持均衡。然而,例如若是接收移動線圈1 3的驅動轉距之 長形方向之兩邊或是關於旋轉軸1 2之軸線之鏡子之質量 產生左右不均衡的話,其質量差將產生重量上的不均衡。 而藉由伴隨著光學掃描機1之動作之重量不均衡的慣性力 ,將於軸承1 4與軸承1 5與旋轉軸1 2之支撐點上產生 彎曲振動。其結果爲,鏡子與鏡面呈平行或是直角方向來 振動。一般於光學掃描機1中,並不具備可檢測出旋轉軸 1 2之彎曲振動之感應器,或是於旋轉軸1 2加上抵銷彎 曲振動之調節器。此外,於上述之伺服機構之回饋控制中 ,無法使已發生之彎曲振動衰減。因此,無法提昇雷射光 之位置決定精密度。 【發明之開示】: 本發明之目的爲提供,不僅降低於裝設了鏡子之旋轉 軸上所產生之扭轉振動及彎曲振動並縮短鏡子之位置決定 時間,並可以提昇雷射光之位置決定精密度光學掃描機之 控制裝置。 本紙張尺度適用中國國家標準(CNS ) A4規格(210><297公釐) I ^ „ 訂 . (請先閲讀背面之注意事項再填寫本頁) 539933 經濟部智慧財產局員工消費合作社印製 A7 B7 五、發明説明(5) 爲了達成上述目的,本發明之第1特徵爲,於基於角 度目標値與角度檢測値,將被支撐於旋轉軸的鏡子,於上 述旋轉軸之周圍上決定其位置之光學掃描機之控制裝置中 ,將關於上述旋轉軸之扭轉振動之補正値附加於上述角度 目標値與上述角度檢測値之偏差之積分値。藉由此,可以 降低旋轉軸之扭轉振動。 於此情況下,可以將上述補正値,做爲附加於上述旋 轉軸之驅動轉距所帶來之上述旋轉軸之扭轉振動之到r次 (r爲正整數)的角速度爲止之傳達函數之輸出値,再者 ,可從供給至產生上述驅動轉距之馬達之電流値中,來運 算上述傳達函數之輸出値。 此外,於基於角度目標値與角度檢測値,將被支撐於 旋轉軸的鏡子,於上述旋轉軸之周圍上決定其位置之光學 掃描機之控制裝置中,不僅將目標軌道做爲位置之時間函 數,還從此目標軌道與基於此目標軌道之目標速度及目標 加速度之和當中,將特定之頻率數成分去除以做爲上述角 度目標値。藉由此,可以降低彎曲振動。 於此情況下,可以將上述特定之頻率數成分,做爲上 述旋轉軸之彎曲振動之固有振動數成分,或是做爲上述旋 轉軸之扭轉振動之固有振動數成分。 本發明之第2特徵爲,於基於角度目標値與角度檢測 値,將被支撐於旋轉軸的鏡子,於上述旋轉軸之周圍上決 定其位置之光學掃描機之控制裝置中,具有檢測出鏡子之 角度之鏡子角度檢測手段,以及檢測出上述旋轉軸之角度 本紙張尺度適用中國國家標準(CNS ) Α4規格(210Χ297公釐) I ^ 裝 „ 訂 _ (請先閲讀背面之注意事項再填寫本頁) -8- 539933 •ω 一 • · ·(式i) 經濟部智慧財產局員工消費合作社印製 A7 B7 五、發明説明(6) 之旋轉軸角度檢測手段,以及檢測出供給至使上述旋轉軸 產生旋轉之馬達之電流之電流檢測手段,以及基於上述電 流之値使扭轉振動安定化之扭轉振動安定化補償手段,並 將,採用旋轉軸角度檢測値以進行比例補償及微分補償後 的値以及上述扭轉振動安定化補償手段之値,負向回饋至 將上述角度目標値及鏡子角度檢測値之偏差加以積分補償 後之値上,並決定供給至馬達之電流値。藉由此,可以降 低旋轉軸之扭轉振動。 【發明之實施型態】: 首先,再次參考第1 2圖及第1 3圖來說明本發明之 原理。 從移動線圏1 3所接收之驅動轉距至移動線圈1 3之 角位移爲止之頻率數應答(自我順應性)是以第1式之傳 達函數G (s)來表示。539933 Printed by the Consumers ’Cooperative of the Intellectual Property Bureau of the Ministry of Economic Affairs A7 B7 V. Description of the invention (1) [Technical field to which the invention belongs]: The invention relates to an angle detection device, and it is decided to support the rotation axis around the rotation axis. Control device for the position of the mirror in the optical scanner. An optical scanning device used for laser marking and laser drilling of printed circuit boards. The built-in electric motor rotates the mirror mounted on the rotating shaft. By changing the angle of the mirror, the laser oscillator will be changed. The output laser light is irradiated to a predetermined position of the workpiece. [Advanced Technology]: Figure 12 shows the structure of the movable part in the optical scanning device. The mirror 11 is mounted on one end of the rotating shaft 12. The rotating shaft 12 is supported by the bearings 14 and 15 and the moving wire 圏 1 3 integrated with the rotating shaft 12 receives the driving torque (Torque) and rotates. Determined at the given location. Hereinafter, the mirror 11, the rotating shaft 12, and the moving coil 13, which rotate together, are collectively referred to as an optical scanner 1. In the optical scanner 1, an angle for detecting the rotation angle of the rotating shaft 12 which is omitted in the figure is set. Detection sensors, such as variable capacity type sensors. The variable-capacity type inductor is constructed by rotating a flat plate of a dielectric body mounted on a rotating shaft between two sets of fixed plates and rotating the shaft, and the angle of the rotating shaft is used as static electricity. Changes in capacity are detected by electrical signals. Regarding the technology of the variable capacity sensor, please refer to, for example, US Patent No. 3 5 7 2 8 2 and US Patent No. This paper is applicable to the Chinese National Standard (CNS) A4 specification (210X297 mm). (Please read the notes on the back before filling this page) -4-Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs 539933 A7 1 '___ B7 V. Description of Invention (2) Gazette No. 4864295 and Japanese Patent Application Laid-Open No. 7-55500 Bulletin. In addition, Japanese Unexamined Patent Publication No. 4-1 2 7 9 8 1 discloses that a laser for angle measurement is irradiated on a mirror, and the reflected light is detected by a linear sensor, and the angle of the mirror is feedback-controlled. Technology. Furthermore, Japanese Patent Application Laid-Open No. 6 3-1 4 7 1 3 8 discloses that a reflecting surface is formed on a part (mirror frame) in which a mirror is fixed to a rotation axis, and the light coming from the reflecting surface is detected by a light receiving element. A technique for determining the position of a mirror by reflecting the light of a light-emitting element. Figure 13 is a block diagram of the control of the optical scanner. In order to feed the angle detection signal 2 2 negatively to the angle target designated by the upper control device 値 signal 2 Γ, and set the deviation signal 2 3 in the normal state to 0, the deviation signal 2 3 is used to integrate the compensation circuit 2 4 Integrate. In addition, in order to maintain the stability of this servo mechanism, the angle detection signal 2 2 is input to the proportional compensation circuit 25 and the differential compensation circuit 26, and the sum of the output signals of these circuits is output from the output signal of the integral compensation circuit 24. Subtract and set to control input signal 2 7. The motor drive circuit 28 supplies a motor drive current 29 to the optical scanner 1 in proportion to the control input signal 27. The motor driving current 29 flows in the moving coil 13 and generates a driving torque in the moving coil 13 which is proportional to the current 値. In the case where a laser light is used to perform hole processing on a printed circuit board, in order to perform precise processing on a fine circuit diagram, it is necessary to reduce the error of the position determination of the laser light used for processing to about 10 A m or less. In addition, in order to reduce the processing time, it must be required to open the paper size after opening a hole. The Chinese paper standard (CNS) A4 size (210X297 mm) is applicable. -5- ^ Assemble. (Please read the back first Please pay attention to this page, please fill out this page) Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs 539933 A7 'B7 _____ V. Description of the invention (3) The speeding up of a hole-cutting operation, for example, opening at 1 00 per second In the case of 0 holes, it is necessary to reduce the moving time between holes to an average of 1 m S. The laser light has its energy distribution and is incident on the mirror 11 with a wide area. Therefore, in order to perform high-quality For the hole-cutting process, the mirror 11 is preferably larger (the area is wider). However, if the mirror 1 1 is enlarged, the torsional vibration and bending vibration of the rotating shaft 12 will become larger and hinder the mirror. Position-dependent high response capability. First, the effect of torsional vibration will be explained. As the mirror 1 1 becomes larger, the moment of inertia (Moment) around the rotation axis 12 also increases, so the rotation of the rotation axis 12 Of Spring The natural vibration number of the rotational vibration will also decrease. The primary mode of the torsional vibration is the torsional vibration with the smallest natural vibration number. There is a twisted node in the longitudinal direction of the rotation axis 12 and the two sides of this node are clamped to each other. The inverse phase is used to generate angular displacement. In addition, the 2nd mode of torsional vibration is torsional vibration with low natural vibration several times. There are 2 twisted nodes in the longitudinal direction of the rotation axis 12. The central part and the parts on both sides vibrate in an inverse phase. For example, when an angle detection sensor is arranged beside a mirror, a node of torsional vibration is placed between the angle detection sensor and the moving coil 13 In this case, in the above-mentioned servo mechanism, the vibration number component of the angle detection signal 22 becomes a positive feedback, resulting in unstable control. The height response determined by the mirror position will be g-force. Considering the suppression characteristics of low-frequency external interference, although the control bandwidth is the largest standard scale applicable to the Chinese National Standard (CNS) A4 specification (210X297 mm) I —; ------ ^ I ----: --- Order ------- AW (Please read the notes on the back before filling out this page) -6- Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs 539933 A7 B7 V. Invention Explanation (4) It is better to be as wide as possible, but the control bandwidth is limited due to the number of torsional vibrations. In addition, when the node of torsional vibration overlaps or is extremely close to the position of the sensor, it cannot be detected by the angle The sensor observes its vibration mode, so the stability of the control cannot be controlled, and the precision of the position determination of the laser light is reduced. Next, the effect of bending vibration will be described. The movable part of the optical scanner shown in Figure 12 It is preferable to maintain balance around the rotation axis 12. However, for example, if the left and right sides of the mirror receiving the driving torque of the moving coil 13 or the length of the mirror about the axis of the rotation axis 12 are uneven, the difference in quality will cause an uneven weight. And by the imbalanced inertial force of the weight accompanying the operation of the optical scanner 1, a bending vibration will be generated at the support points of the bearings 14 and 15 and the rotating shaft 12. As a result, the mirror vibrates in parallel or at right angles to the mirror surface. Generally, the optical scanner 1 does not include a sensor capable of detecting bending vibration of the rotating shaft 12 or an adjuster for offsetting bending vibration is added to the rotating shaft 12. In addition, in the feedback control of the above-mentioned servo mechanism, the bending vibration that has occurred cannot be attenuated. Therefore, the precision of the laser light position determination cannot be improved. [Invention]: The purpose of the present invention is to provide, not only reduce the torsional vibration and bending vibration generated on the rotating shaft on which the mirror is installed, and shorten the position determination time of the mirror, but also improve the precision of the position determination of the laser light. Control device for optical scanner. This paper size applies the Chinese National Standard (CNS) A4 specification (210 > < 297mm) I ^ „Order. (Please read the precautions on the back before filling this page) 539933 Printed by the Consumers’ Cooperative of Intellectual Property Bureau of the Ministry of Economic Affairs A7 B7 V. Description of the invention (5) In order to achieve the above object, the first feature of the present invention is that, based on the angle target 値 and the angle detection 値, a mirror that will be supported on the rotation axis is determined around the rotation axis. In the control device of the position optical scanner, a correction 値 for the torsional vibration of the rotation axis is added to the integral of the deviation between the angle target 値 and the angle detection 値. Thus, the torsional vibration of the rotation shaft can be reduced. In this case, the above-mentioned correction 値 can be used as an output of a transfer function up to r times (r is a positive integer) the angular velocity of the rotation shaft of the rotation shaft caused by the driving torque of the rotation shaft.値 Furthermore, the output 値 of the above-mentioned transfer function can be calculated from the current 値 supplied to the motor which generates the drive torque described above.値 and angle detection 値, the mirror that is supported on the rotation axis, and the control device of the optical scanner that determines its position around the rotation axis, not only the target track as a function of position time, but also from this target track and Based on the sum of the target speed and the target acceleration of the target orbit, a specific frequency number component is removed as the angle target 値. Thus, the bending vibration can be reduced. In this case, the above specific frequency number can be reduced The component is used as the natural vibration number component of the bending vibration of the rotary shaft, or as the natural vibration number component of the torsional vibration of the rotary shaft. A second feature of the present invention is based on the angle target 基于 and the angle detection 値, The control device of the optical scanner that determines the position of the mirror supported by the rotation axis around the rotation axis includes a mirror angle detection means that detects the angle of the mirror, and a paper that detects the angle of the rotation axis. Standards are applicable to Chinese National Standard (CNS) Α4 specification (210 × 297 mm) I ^ Order „(Please read first Note on the back, please fill in this page again) -8- 539933 • ω 1 • · · (Formula i) Printed by the Consumers ’Cooperative of the Intellectual Property Bureau of the Ministry of Economic Affairs A7 B7 V. Description of the invention (6) Rotation axis angle detection method, and A current detection means for detecting a current supplied to a motor that rotates the above-mentioned rotating shaft, and a torsional vibration stabilization compensation means for stabilizing torsional vibration based on the above-mentioned current, and the rotation axis angle detection is used for proportionality After the compensation and differential compensation, and the above-mentioned torsional vibration stabilization compensation method, the negative feedback is fed back to the angle after the deviation of the angle target 角度 and the mirror angle detection 加以 are integrated and compensated, and the current supplied to the motor is determined 値. This can reduce the torsional vibration of the rotating shaft. [Implementation Mode of the Invention]: First, the principle of the present invention will be described with reference to FIGS. 12 and 13 again. The frequency response (self-compliance) from the driving torque received by the moving wire 圏 13 to the angular displacement of the moving coil 13 is expressed by the transfer function G (s) of the first formula.
G{s) = + X 在此,s爲拉普拉斯轉換之複數變數,n爲扭轉振動 之第η次模式(η爲正整數),Γ η爲扭轉振動之第η次模 式之衰減係數,k 〇爲關於剛體模式之常數,k η爲扭轉振 動之第η次模式之模式常數。 在此’若注目於特定之扭轉振動模式(第r次模式) 的話’顯示於第2式之傳達函數G r ( s )爲,從驅動轉距 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) 11 ;------HI 裝----Ί.--訂------- (請先閲讀背面之注意事項再填寫本頁) -9- 539933 •(式2) …(式3) A7 · B7 五、發明説明(7) 至移動線圈1 3之位置中之% r次模式之角變化爲止之傳 達函數,顯示於第3式之H r ( s )爲,從驅動轉距至移動 線圈1 3之位置中之第r次模式之角位移爲止之傳達函數 +2ζτωΓΞ + ωΓ W杨; 因爲傳達函數H r ( s )爲顯示在驅動轉距所作用之位 置上之應答,因此模式常數k r爲正。因此,若是將傳達函 數H r ( s )之値負向回饋至控制輸入訊號2 7的話,則可 以賦予控制性的衰減至第r次模式來加以安定化 於馬達驅動電路2 8爲電流控制方式之情況下,一般 而言,因爲移動線圈1 3之驅動轉距與馬達驅動電流2 9 成比例,因此可以藉由測定馬達驅動電流2 9來得之移動 線圏1 3之驅動轉距。而對應於馬達驅動電流2 9之値之 電流檢測訊號,例如將馬達驅動電流2 9流至電阻値較小 (0 · 1至數Ω以下)之電流檢測電阻中,藉由將此電阻 之端子間電壓輸入至差動輸入型減算電路中,可以做爲差 動輸入型減算電路之輸出來加以獲得。 以下,基於圖示之實施形態來說明本發明。 第1圖係爲本發明之光學掃描機之控制磚塊圖。而與 已說明之第1 2圖相同或是具有同一功能之處則賦予相同 本紙張尺度適用中國國家標準(CNS ) A4規格(21〇χ297公釐) I ^ 裝 ^ 訂 . (請先閱讀背面之注意事項再填寫本頁) 經濟部智慧財產局員工消費合作社印製 -10- 經濟部智慧財產局員工消費合作社印製 539933 A7 , B7 五、發明説明(8) 符號並省略其說明。將角度檢測訊號2 2負向回饋至角度 目標値訊號2 1而得到偏差訊號2 3,並將偏差訊號2 3 以積分補償電路2 4加以積分。此外,爲了保持此伺服機 構之安定性,將角度檢測訊號2 2輸入於比例補償電路 2 5及以及之後所述之角速度觀測電路3 2。 此外,將對應於供給至移動線圈1 3之電流値大小之 電流檢測訊號3 1 ,輸入至角速度觀測電路3 2及之後所 述之扭轉振動一次補償電路3 3及扭轉振動二次補償電路 3 4。並將比例補償電路2 5與角速度觀測電路3 2及扭 轉振動一次補償電路3 3及扭轉振動二次補償電路3 4之 輸出訊號之和的値4 2,從積分補償電路2 4之輸出訊號 減去,以做爲控制輸入訊號2 7。而關於鏡子角度指令電 路2 0與鏡子振動抑制因子4 1之後詳述。 接下來說明扭轉r次補償電路。 藉由實際測定鏡子1 1之頻率數應答,可以得知r次 之固有振動數與衰減係數。此外,可藉由電子線路來構成 具有於第3式之相同符號成比例之頻率數應答特性之二次 濾波器(以下稱爲扭轉r次補償電路)。 第2圖係顯示本發明之扭轉r次補償電路,係由3個 運算放大器3 3 3〜3 3 5,以及6個電阻Roi-Roe, 以及2個電容器CQ1及CQ2所構成。運算放大器3 3 3〜 3 3 5之正極側輸入端子爲接地。而運算放大器3 3 3之 負極側輸入端子則接續於電阻R。i之一端之端子及C。i之 一端之端子。運算放大器3 3 3之輸出端子接續於C 〇 i之 本紙張尺度適用中國國家標準(CNS ) A4規格(210 X 297公釐) I ^ ^ 訂 (請先閲讀背面之注意事項再填寫本頁) -11 - 539933G {s) = + X Here, s is a complex variable of Laplace transform, n is the η-th mode of torsional vibration (η is a positive integer), and Γ η is the attenuation coefficient of the η-th mode of torsional vibration K is the constant for the rigid body mode, and k η is the mode constant for the η-th mode of torsional vibration. Here, 'if you pay attention to a specific torsional vibration mode (rth-order mode)', the transfer function G r (s) shown in the second equation is that the driving torque is applied to the paper standard of China National Standard (CNS) A4 (210X297 mm) 11 -------- HI equipment ---- Ί .-- Order ------- (Please read the notes on the back before filling this page) -9- 539933 • ( (Equation 2)… (Equation 3) A7 · B7 V. Explanation of the invention (7) The transfer function until the angle change of the% r-order mode in the position of the moving coil 13 is displayed in H r (s) of Equation 3 The transfer function from the driving torque to the angular displacement of the r-th mode in the position of the moving coil 13 is + 2ζτωΓΞ + ωΓ W Yang; because the transmission function H r (s) is shown to act on the driving torque Position response, so the mode constant kr is positive. Therefore, if the negative of the transfer function H r (s) is fed back to the control input signal 2 7, the controllable attenuation can be given to the r-th mode to stabilize the motor drive circuit 28 as the current control method. In this case, in general, since the driving torque of the moving coil 13 is proportional to the motor driving current 2 9, the driving torque of the moving wire 圏 13 can be obtained by measuring the motor driving current 29. The current detection signal corresponding to 値 of the motor drive current 29, for example, flows the motor drive current 29 to a current detection resistor with a small resistance 0 (0 · 1 to several Ω or less). The inter-voltage input to the differential input type subtraction circuit can be obtained as the output of the differential input type subtraction circuit. Hereinafter, the present invention will be described based on the illustrated embodiments. Fig. 1 is a control block diagram of the optical scanner of the present invention. The same or same function as the first and second pictures shown in Figure 12 are given the same paper size as the Chinese National Standard (CNS) A4 specification (21〇297 mm). I ^ Binding ^. (Please read the back first Please note this page, please fill in this page) Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs -10- Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs 539933 A7, B7 V. Description of Invention (8) Symbols and descriptions are omitted. The angle detection signal 2 2 is negatively fed back to the angle target 値 signal 21 to obtain the deviation signal 2 3, and the deviation signal 2 3 is integrated by the integral compensation circuit 2 4. In addition, in order to maintain the stability of this servo mechanism, the angle detection signal 2 2 is input to the proportional compensation circuit 25 and the angular velocity observation circuit 32 described later. In addition, a current detection signal 3 1 corresponding to the magnitude of the current supplied to the moving coil 13 is input to the angular velocity observation circuit 3 2 and the torsional vibration primary compensation circuit 3 3 and the torsional vibration secondary compensation circuit 3 4 described later. . The sum of the output signals of the proportional compensation circuit 25 and the angular velocity observation circuit 3 2 and the primary torsional vibration compensation circuit 3 3 and the secondary torsional vibration compensation circuit 3 4 is subtracted from the output signal of the integral compensation circuit 2 4. Go as a control input signal 2 7. The mirror angle command circuit 20 and the mirror vibration suppression factor 41 will be described in detail later. Next, the torsion r-time compensation circuit will be described. By measuring the frequency response of the mirror 11 actually, the natural vibration number and attenuation coefficient of r times can be known. In addition, a secondary filter (hereinafter referred to as a torsion r-th order compensation circuit) having a frequency response characteristic proportional to the same sign in Equation 3 can be constructed by an electronic circuit. Figure 2 shows the torsion r-time compensation circuit of the present invention, which is composed of three operational amplifiers 3 3 3 to 3 35, six resistors Roi-Roe, and two capacitors CQ1 and CQ2. The positive input terminals of the operational amplifiers 3 3 3 to 3 3 5 are grounded. The negative input terminal of the operational amplifier 3 3 3 is connected to the resistor R. i terminal and C. i terminal. The output terminals of the op amp 3 3 3 are connected to the original paper size of C 〇i. Applicable to China National Standard (CNS) A4 (210 X 297 mm) I ^ ^ Order (please read the precautions on the back before filling this page) -11-539933
S (式4) A7 ' B7 __ 五、發明説明(9) 另一端之端子及R〇3之一端之端子。而R。3之另一端之端 子則接續於R ◦ 2、R ◦ 4、c ◦ 2之一端之端子及運算放大 器3 3 4之負極側輸入端子。運算放大器3 3 4之輸出立而 子接續於C ^ 2之另一端之端子及R ◦ 4之另一端之端子及 R ◦ 5之一端之端子。運算放大器3 3 5之負極側輸入端子 接續於R。5之另一端之端子及R ^ 6之一端之端子。運算放 大器3 3 5之輸出端子接續於R ◦ 6之另一端之端子及R 0 1 之另一端之端子及端子3 3 2。而R〇2之另一端之端子接 續於端子3 3 1。此外,R ◦ 2爲可變電阻。 於此電路中,若使電阻値R。5與電阻値R Q 6相等的話 ,則從輸入於端子3 3 1之輸入訊號至由端子3 3 2所輸 出之輸出訊號爲止之傳達函數G c ( s )如第4式所示。 ^02^02 S + 而若是將電阻値Rqi、R〇3、R〇4及電容器之靜電 容量C〇1、,以第4式之分母多項式之常數項與第3 式之分母多項式之常數項相等,並且第4式之分母多項式 之一次項之係數與第3式之分母多項式之一次項之係數相 等之方式加以設定的話,則此線路之固有振動數與衰減 係數Γ r等於第I·次振動模式。 而若將電流檢測訊號3 1輸入於端子3 3 1的話’則 由端子3 3 2所輸出之輸出訊號以相同符號與移動線圈 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) I — ^------^裝----„---訂------ (請先閲讀背面之注意事項再填寫本頁) 經濟部智慧財產局員工消費合作社印製 -12- 539933 Μ , Β7 五、發明説明( 1 3之位置中之r次模式之角速度成比例。因此,藉由將 來自於端子3 3 2之輸出訊號負向回饋至積分補償電路 2 4之輸出訊號,可以將r次之振動模式加以安定化,亦 即可降低r次之振動。 於此實施形態中,因爲係將電阻値R 0 2與固有振動數 與衰減係數互相獨立而設定,因此可藉由將電阻値R。2設 定爲可變電阻,來調整扭轉r次振動補償電路之輸出訊號 之振幅。 此外,於第1圖所示之控制碍塊圖中,係顯示了設置 扭轉振動一次補償電路3 3及扭轉振動二次補償電路3 4 ’以使扭轉振動之一次及二次模式安定化之情況,而於針 對更多數之振動模式進行補償之情況下,可於每個模式中 設置如第2圖所示之扭轉振動補償電路,並藉由將這些扭 轉振動補償電路與扭轉振動一次補償電路3 3及扭轉振動 二次補償電路3 4等並列接續,可達到所希望之次數之扭 轉振動之安定化。 接下來,關於角速度觀測電路3 2加以說明。於本發 明中,取代第1 3圖之微分補償電路2 6而設置角速度觀 測電路3 2,以推定對應於第1式之第一項之剛體模式之 角速度。而藉由將所得之推定訊號負向回饋至積分補償電 路2 4之輸出訊號,可以針對第1圖所示之伺服系統進行 安定化。 第3圖係顯示本發明之角速度觀測電路3 2,係由2 個運算放大器3 2 4、3 2 5,以及6個電阻R i i〜r i 6 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) ----- (請先閱讀背面之注意事項再填寫本頁) 、言 經濟部智慧財產局員工消費合作社印製 -13- 經濟部智慧財產局員工消費合作社印製 539933 A7 B7 五、發明説明(11) ,以及電容器C!1所構成。運算放大窃"3 2 4、3 2 5之 正極側輸入端子爲接地。而運算放大器3 2 4之負極側輸 入端子則接續於電阻R 1 1〜電阻R 1 3之一端之端子及 C 1 1之一端之端子。而R 1 1之另一端則接續於端子3 2 1 與R 1 4之一端之端子,而R 1 2之另一端則接續於端子 3 2 2。而運算放大器3 2 4之輸出端子接續於C ! i之另 一端之端子及Rl3之另一端之端子及Ris之一端之端子。 運算放大器3 2 5之負極側輸入端子接續於R 1 4及R i 5之 另一端之端子及Rie之一端之端子。運算放大器3 2 5之 輸出端子接續於R ^ 6之另一端之端子及端子3 2 3。 於此電路中,若將電阻値R 1 1、R 1 3、R 1 4、R 1 5 之値設定爲滿足第5式之關係的話,則輸入於端子3 2 1 、3 2 2之訊號與從端子3 2 3輸出之訊號之關係如第6 式所示。 l£r -*· 及"W丨4 ··:(式5)S (Equation 4) A7 'B7 __ 5. Description of the invention (9) The terminal at the other end and the terminal at one end of R03. And R. The terminal at the other end of 3 is connected to the terminal at one end of R ◦ 2, R ◦ 4, c ◦ 2 and the negative-side input terminal of the operational amplifier 3 3 4. The output of the operational amplifier 3 3 4 is connected to the terminal of the other end of C ^ 2 and the terminal of the other end of R ◦ 4 and the terminal of one end of R ◦ 5. The negative input terminal of the operational amplifier 3 3 5 is connected to R. The terminal at the other end of 5 and the terminal at one end of R ^ 6. The output terminal of the computing amplifier 3 3 5 is connected to the terminal at the other end of R ◦ 6 and the terminal at the other end of R 0 1 and the terminal 3 3 2. The terminal at the other end of Ro2 is connected to terminal 3 31. In addition, R ◦ 2 is a variable resistor. In this circuit, if the resistor 値 R is made. If 5 is equal to the resistance 値 R Q 6, then the transfer function G c (s) from the input signal input to the terminal 3 3 1 to the output signal output from the terminal 3 3 2 is shown in the fourth formula. ^ 02 ^ 02 S + And if the resistance 値 Rqi, R〇3, R〇4 and the capacitance of the capacitor C01, the constant term of the denominator polynomial of Formula 4 and the constant term of the denominator polynomial of Formula 3 If the coefficients of the first term of the denominator polynomial of Formula 4 and the coefficients of the first term of the denominator polynomial of Formula 3 are set equal, then the natural vibration number and attenuation coefficient Γ r of this line are equal to the I · th order. Vibration mode. And if the current detection signal 3 1 is input to the terminal 3 3 1 ', then the output signal output from the terminal 3 3 2 uses the same symbol and the moving coil. The paper size applies the Chinese National Standard (CNS) A4 specification (210X297 mm) I — ^ ------ ^ Installation ---- „--- Order ------ (Please read the notes on the back before filling out this page) Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs- 12- 539933 Μ, B7 V. Description of the invention (The angular velocity of the r-order mode in the position of 1 3 is proportional. Therefore, the output signal from the terminal 3 3 2 is negatively fed back to the output of the integral compensation circuit 2 4 The signal can stabilize the vibration mode of the rth order, that is, reduce the vibration of the rth order. In this embodiment, since the resistance 値 R 0 2 and the natural vibration number and the attenuation coefficient are set independently from each other, it can be set. By setting the resistance 値 R.2 as a variable resistor, the amplitude of the output signal of the torsional vibration compensation circuit is adjusted. In addition, the control block diagram shown in Fig. 1 shows that the torsional vibration is set once. Compensation circuit 3 3 and torsional vibration secondary compensation circuit 3 4 'To stabilize the primary and secondary modes of torsional vibration, and to compensate for a larger number of vibration modes, a torsional vibration compensation circuit as shown in Figure 2 can be set in each mode By connecting these torsional vibration compensation circuits with the torsional vibration primary compensation circuit 33 and the torsional vibration secondary compensation circuit 34 in parallel, it is possible to stabilize the torsional vibration at a desired number of times. Next, regarding angular velocity observation The circuit 32 will be described. In the present invention, an angular velocity observation circuit 3 2 is provided instead of the differential compensation circuit 26 of FIG. 13 to estimate the angular velocity of the rigid body mode corresponding to the first term of the first equation. The obtained estimated signal is negatively fed back to the output signal of the integral compensation circuit 24, which can stabilize the servo system shown in Fig. 1. Fig. 3 shows the angular velocity observation circuit 32 of the present invention, which is composed of two Operational amplifiers 3 2 4, 3 2 5 and 6 resistors R ii ~ ri 6 This paper size is applicable to China National Standard (CNS) A4 specification (210X297 mm) ----- (Please read the back (Please fill in this page on the matters needing attention), printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs -13- printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs 539933 A7 B7 V. Description of Invention (11), and capacitor C! 1 The positive input terminal of the operational amplifier "3 2 4, 3 2 5 is grounded. The negative input terminal of the operational amplifier 3 2 4 is connected to the terminal of one of the resistors R 1 1 to R 1 3 and C 1 1 terminal. The other end of R 1 1 is connected to the terminal of terminals 3 2 1 and R 1 4, and the other end of R 1 2 is connected to terminal 3 2 2. The output terminal of the operational amplifier 3 2 4 is connected to the terminal at the other end of C! I, the terminal at the other end of R13, and the terminal at one end of Ris. The negative input terminal of the operational amplifier 3 2 5 is connected to the other terminal of R 1 4 and R i 5 and the terminal of one terminal of Rie. The output terminal of the operational amplifier 3 2 5 is connected to the terminal at the other end of R ^ 6 and the terminal 3 2 3. In this circuit, if the resistance 値 R 1 1, R 1 3, R 1 4, R 1 5 is set to satisfy the relationship of the fifth formula, then the signal input at the terminals 3 2 1 and 3 2 2 and The relationship between the signals output from terminals 3 2 3 is shown in Equation 6. l £ r-* · and " W 丨 4 ··: (Eq. 5)
Eo{s) = ~R^ 1—(-竭 + ㈠ J +- S +- ·_·(式6)‘ 在此,E i i ( s )爲輸入訊號3 2 1之拉普拉斯轉換 ,爲角度檢測訊號2 2之進行過符號反轉後之訊號。此外 ,E i 2 ( s )爲輸入訊號3 2 2之拉普拉斯轉換’爲電流 本紙張尺度適用中國國家標準(CNS ) A4規格(210X 297公釐) ---------^裝----^—訂------ (請先閲讀背面之注意事項再填寫本頁) -14- 539933 A7 B7 五、發明説明(12) 檢測訊號3 1。E ^ ( s )爲輸入訊號3 2 3之拉普拉斯轉 換,爲角速度推定訊號。 (請先閲讀背面之注意事項再填寫本頁) 第6式之第一項及第二項之一次傳達函數具有共通之 分母多項式,而常數項1 / R 1 3 C i i爲各個傳達函數之折 角點頻率數。而對應於第6式之第一項,並且於比此折角 點頻率數還低之頻率區中,主要是角度檢測訊號之微分爲 角速度推定訊號,此外,對應於第6式之第二項,並且於 比此折角點頻率數還高之頻率區中,主要是角度檢測訊號 之積分爲角速度推定訊號,因此可以以高精密度之方式來 推定移動線圈1 3中之位置之剛體模式之角速度。 經濟部智慧財產局員工消費合作社印製 於角度檢測感應器配置於遠離移動線圏1 3中之位置 之情況下,接近扭轉振動之頻率數區域中之角度檢測訊號 ,偏離了移動線圏1 3之位置中之角位移。因此,於角度 檢測感應器配置於遠離移動線圏1 3中之位置之情況下, 最好是以折角點頻率數比扭轉振動一次模式還低之方式, 來決定電阻R 13及電容器之靜電容量C 1 1之値。若是如此 做的話,因爲可降低角度檢測訊號之扭轉振動數成分被正 向回饋之程度,因此即使將伺服頻寬延伸至比以往之伺月g 系統還寬之情況下,亦可確保伺服系統之安定性。 接下來,針對抑制旋轉軸之彎曲振動所帶來之鏡子振 動之實施形態加以說明。 第4圖係爲第1圖所顯示之本發明之鏡子振動抑制因 子之磚塊圖。目標軌道4 1 1爲鏡子1 1之旋轉角之目標 軌跡。而於之鏡子振動抑制因子4 1中,角度目標値係從 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) -15- 539933 A7 B7 五、發明説明(13) 鏡子角度指令電路2 0被供給。 在此,將目標軌道4 1 1設定爲,以第7式所示之 a m a X爲最大加速度並且並於相同時間內進行最大加速及 最大減速之慣性體之最短時間軌道。而L爲從時刻〇開始 旋轉至時刻Τ μ停止之行程。於此情況下,加速度之時間函 數a ( t ),速度之時間函數v ( t ),位置之時間函數 X (t)各以第8式,第9式,第10式來表示。Eo {s) = ~ R ^ 1 — (-exhaustion + ㈠ J +-S +-· _ · (Equation 6) 'Here, E ii (s) is the Laplace transform of the input signal 3 2 1, It is the signal after the sign inversion of the angle detection signal 2 2. In addition, E i 2 (s) is the Laplacian conversion of the input signal 3 2 2 'for the current. The paper standard applies Chinese National Standard (CNS) A4 Specifications (210X 297mm) --------- ^ Installation ---- ^-Order ------ (Please read the precautions on the back before filling this page) -14- 539933 A7 B7 V. Explanation of the invention (12) The detection signal 3 1. E ^ (s) is the Laplacian conversion of the input signal 3 2 3 and is the estimated signal of angular velocity. (Please read the precautions on the back before filling this page) Section 6 The first- and second-order transfer functions of the formula have a common denominator polynomial, and the constant term 1 / R 1 3 C ii is the frequency of the corner points of each transfer function. And corresponding to the first term of formula 6, And in the frequency region lower than the frequency of the corner point, the differential angular velocity estimation signal of the angle detection signal is mainly, in addition, it corresponds to the second term of formula 6 and the frequency of the corner point is In the high frequency area, the integral of the angle detection signal is the angular velocity estimation signal, so the angular velocity of the rigid body mode of the position in the moving coil 13 can be estimated with high precision. When the angle detection sensor is placed away from the position in the moving line 圏 13, the angle detection signal in the frequency region near the torsional vibration is deviated from the angular displacement in the position of the moving line 313. Therefore, In the case where the angle detection sensor is located away from the moving line 313, it is best to determine the capacitance of the resistor R13 and the capacitance C1 of the capacitor in such a way that the frequency of the corner point is lower than the one-time torsional vibration mode. 1 値. If this is done, the degree of torsional vibration of the angle detection signal can be reduced to a positive degree, so even if the servo bandwidth is extended to be wider than the conventional servo system, Ensuring the stability of the servo system. Next, the embodiment of suppressing the mirror vibration caused by the bending vibration of the rotating shaft will be described. Figure 4 is a block diagram of the mirror vibration suppression factor of the present invention shown in Figure 1. The target track 4 1 1 is the target trajectory of the rotation angle of the mirror 11 and the mirror vibration suppression factor 4 1 The angle target does not apply the Chinese National Standard (CNS) A4 specification (210X297 mm) -15- 539933 A7 B7 from this paper scale. 5. Description of the invention (13) The mirror angle command circuit 20 is supplied. Here, the target The orbit 4 1 1 is set to the shortest time orbit of the inertial body that uses the ama X shown in Equation 7 as the maximum acceleration and performs maximum acceleration and maximum deceleration in the same time. And L is the stroke that starts from time 0 and stops at time T μ. In this case, the time function a (t) of acceleration, the time function v (t) of velocity, and the time function X (t) of position are each expressed by Equation 8, Equation 9, and Equation 10.
4L aMAX (式7) a 0:(/) = < MAX aMAX 0 (0</<0.57^) (0^</<7^) (式8) a4L aMAX (Equation 7) a 0: (/) = < MAX aMAX 0 (0 < / < 0.57 ^) (0 ^ < / < 7 ^) (Equation 8) a
bAAX %-t] 經濟部智慧財產局員工消費合作社印製bAAX% -t] Printed by the Consumer Cooperative of the Intellectual Property Bureau of the Ministry of Economic Affairs
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L-05aMAX{t -L {〇<t<〇5TM) (05TM<t<TM) · ·(V 0 (0</<0^)Tj (05TM<i<TM) •(式 9) •(式 10) 不僅將位置之時間函數x ( t )設爲目標軌道4 1 1 並將微分因子4 1 2之輸出與二階微分因子4 1 3之輸 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) —.------^裝----—訂—----- (請先閲讀背面之注意事項再填寫本頁) 16- 539933 A7 __B7_ 五、發明説明(Μ) 出加算至目標軌道4 1 1並輸入於陷波濾波器(NotchL-05aMAX {t -L {〇 < t < 〇5TM) (05TM < t < TM) · (V 0 (0 < / < 0 ^) Tj (05TM < i < TM) • (Equation 9) • (Equation 10) Not only the time function x (t) of the position is set to the target orbit 4 1 1 and the output of the differential factor 4 1 2 and the output of the second order differential factor 4 1 3 are used. The paper scale is applicable to the Chinese National Standard (CNS) A4 specification (210X297 mm) —.------ ^ equipment ----— order —----- (Please read the notes on the back before filling this page) 16- 539933 A7 __B7_ V. Invention Explanation (Μ) is added to the target orbit 4 1 1 and input to the notch filter (Notch
Filter )。而將陷波濾波器之輸出訊號做爲角度目標値訊號 2 1。做爲陷波濾波器之常數,角振動數ω b等於旋轉軸 1 2之彎曲振動之固有角振動數。此外,分母多項式之常 數Γ b與分子多項式之常數t bn係設定爲C b〉Γ bn。 在此,將目標軌道4 1 1之時間函數之拉普拉斯轉換 設爲X ( S ),此外將角度目標値訊號2 1之拉普拉斯轉 換設爲R ( s )的話,X ( s )與R ( s )之間具有如第 1 1式所示之關係,而藉由陷波濾波器之分子多項式之零 點,可使旋轉軸1 2之彎曲振動數成分除去。 (請先閱讀背面之注意事項再填寫本頁) S2+^bnC〇bS + C〇l S2+2ζόω^ + ωΙ 2ζ,Filter). The output signal of the notch filter is used as the angle target signal. As a constant of the notch filter, the angular vibration number ω b is equal to the natural angular vibration number of the bending vibration of the rotating shaft 12. In addition, the constant Γ b of the denominator polynomial and the constant t bn of the numerator polynomial are set to C b> Γ bn. Here, the Laplace transform of the time function of the target orbit 4 1 1 is set to X (S), and if the Laplace transform of the angle target 値 signal 2 1 is set to R (s), X (s ) And R (s) have a relationship as shown in Equation 11, and the zero point of the molecular polynomial of the notch filter can remove the bending vibration component of the rotating shaft 12. (Please read the notes on the back before filling this page) S2 + ^ bnC〇bS + C〇l S2 + 2ζόω ^ + ωΙ 2ζ,
•S 斗) (式 11) 因此,一旦將角度目標値訊號2 1輸入於第1圖所示 之回饋控制系統的話,則可以抑制伴隨著位置決定動作之 鏡子振動。 經濟部智慧財產局員工消費合作社印製 此外,雖然陷波濾波器具有以分母多項式之係數決定 之相位延遲,但是可藉由將目標軌道4 1 1與微分因子 4 1 2之輸出與二階微分因子4 1 3之輸出加算,使陷波 濾波器之分母多項式被加以抵銷。其結果爲,可以使從目 標軌道4 1 1至角度目標値訊號2 1爲止之相位延遲消失 ,並使目標軌道4 1 1之位置決定動作之延遲變小。 如上所.述,將已發生之彎曲振動以回饋控制來使其衰 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) -17 539933 A7 B7 五、發明説明(15) (請先閲讀背面之注意事項再填寫本頁) 減是極爲困難,但是於本發明中’因爲是藉由輸往回饋控 制系統之輸入,亦即藉由以鏡子振動抑制因子4 1來產生 角度目標値訊號2 1 ’來預防旋轉軸1 2之彎曲振動’因 此可以降低鏡子振動之雷射光位置決定之誤差。 將爲目標軌道之時間函數之一階微分之目標速度之拉 普拉斯轉換設爲V ( s ),此外,將爲目標軌道之時間函 數之二階微分之目標加速度之拉普拉斯轉換設爲A ( s ) 的話,則可將第1 1式轉變爲第1 2式。 Κ{ή = X{s) + sX{s) + ^rs2X(s) ^X(s) + ^V(s) + ^ A{s) 、J \ cob cob ①b • · * (式12) 經濟部智慧財產局員工消費合作社印製 第5圖係爲本發明之振動控制因子之磚塊圖,爲實現 第1 2式之圖。於同圖中,增益因子4 1 7,4 1 8爲以 陷波瀘波器4 1 4之常數來決定之權重之係數。若是如此 之構成的話,則可藉由將目標軌道(第1 0式)與目標速 度(第9式)與目標加速度(第8式)賦予權重來加算, 即使無法實現陷波濾波器4 1 4,亦可產生第4圖所示之 鏡子振動抑制因子與等價之角度目標値訊號2 1。 在此,第4圖與第5圖所示之振動抑制因子可藉由微 處理器來容易實現。於此情況下,第1圖之回饋控制系統 爲類比控制之情況下,藉由以D A轉換器將數位之角度目 標値訊號轉換至類比訊號,可適用本發明。 而除了於算出目標軌道與目標速度與目標加速度之際 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐)— -18- 539933 A7 B7 五、發明説明(16) (請先閱讀背面之注意事項再填寫本頁) 進行加算之外,亦可將這些時序列値預先計算並記憶於記 憶體中,並於位置決定動作之際將所記憶之資料依序讀出 。於此情況下,若以行程L將各個目標値加以正規化並記 憶於記憶體的話,則可以減小記憶體容量。 此外,亦可藉由行程L之大小來設定數種動作時間Τ μ 〇 再者,目標軌道並不限定於第1 0式所表示者’亦可 將目標軌道設定爲,可以以等於或是大於陷波濾波器 4 1 4之分母多項式之次方數來微分之時間波形。 此外,若將陷波濾波器4 1 4之角振動數ω b設定爲等 於掃描機可動部分之扭轉振動之固有角振動數的話,則可 以以與上述之扭轉振動補償電路不同之構成來降低扭轉振 .動。於此情況下,伺服機構並不限於第1圖所示之伺服機 構,亦可採用如第1 3圖所示之以往之伺服機構。 經濟部智慧財產局員工消費合作社印製 第6圖係顯示光學掃描機之控制裝置之其他實施例。 於第6圖中,除了第1圖所示之要素之外,還加上鏡子 1 1以及附隨於鏡子1 1之要素,以及感應器角度檢測電 路3 5,透過此,角度檢測訊號2 2僅僅被供給至角速度 觀測電路3 2與比例補償電路2 5,於此點上與第1圖有 所不同。其他構成則與第1圖相同,在此省略其詳細說明 。參照第6圖,於光學掃描機1之旋轉軸1 2中,配置了 檢測角度之角度感應器1 6。 於鏡子1 1中,具有將加工用雷射光加以反射之鏡面 ,以及配置於此鏡面之被面之鏡面1 7 a。夾著鏡面1 7 本紙張尺度適用中國國家標準(CNS ) A4規格(2淑297公釐) -19 - 539933 經濟部智慧財產局員工消費合作社印製 A7 B7 五、發明説明(17) a ,發光元件1 7 b與受光元件1 7 c被配置。做爲發光 元件1 7 b例如爲半導體雷射元件,此外,做爲受光元件 1 7 c 例如可採用 P S D (Position Sensitive Device)兀件 ο 接下來關於訊號之流程及伺服機構加以說明。 從受光元件1 7 C中被輸出之鏡子角度檢測訊號1 7 e (與鏡子1 1之角度成比例之電壓訊號)是藉由放大器 1 7 d來被放大,並被負向回饋至由鏡子角度指令電路 2 0中所輸出之角度目標値訊號2 1上,並產生偏差訊號 2 3。爲了使鏡子1 1之角度依循於不產生常態偏差之角 度目標値,以積分補償電路2 4將偏差訊號2 3加以積分 並形成1型伺服系統。此外,爲了確保此伺服機構之安定 性,將角度檢測訊號2 2輸入於比例補償電路2 5及角速 度觀測電路3 2,並將這些電路之輸出訊號之和與來自於 扭轉振動安定化補償電路3 3之輸出訊號3 3 a ,從積分 補償電路2 4之輸出訊號中減算,並做爲控制輸入訊號 2 7。馬達驅動電路2 8將與控制輸入訊號2 7成比例之 馬達驅動電流2 9供給至光學掃描機1。馬達驅動電流 2 9流入移動線圏1 3,於移動線圏1 3中產生與電流値 成比例之驅動轉距。藉由如此,可以降低旋轉軸1 2之扭 轉振動。 在此,於馬達驅動電路2 8爲電流控制方式之情況下 ,一般而言,因爲移動線圈1 3之驅動轉距與馬達驅動電 流2 9成比例,因此可藉由測定馬達驅動電流2 9來得知 本紙張尺度適用中國國家標準(CNS ) A4規格(21〇><297公釐) —-------^ΙΙΓ 裝----:---訂-------I (請先閲讀背面之注意事項再填寫本頁) -20- 539933 經濟部智慧財產局員工消費合作社印製 A7 B7 五、發明説明(18) 移動線圈1 3之驅動轉距。而與馬達驅動電流2 9之値成 比例之電流檢測訊號3 1 ,例如將馬達驅動電流2 9流至 電阻値較小(0 · 1至數Ω以下)之電流檢測電阻中,藉 由將此電阻之端子間電壓輸入至差動輸入型減算電路中, 可以做爲差動輸入型減算電路之輸出來加以獲得。再將與 馬達驅動電流2 9之値成比例之電流檢測訊號3 1 ,輸入 於角速度觀測電路3 2與扭轉振動安定化補償電路3 3。 由角度感應器所檢測出之旋轉軸1 2之位置,係做爲 角度檢測訊號2 2從感應器角度檢測電路3 5中被輸出。 然後將角度檢測訊號2 2輸入於比例補償電路2 5及角速 度觀測電路3 2。 接下來,關於扭轉振動安定化補償電路3 3之說明, 可參照已說明之第1圖之扭轉振動一次補償電路3 3之說 明。 接下來基於光學掃描機之具體例,說明可動部分之扭 轉振動特性與伺服機構之安定性。 第7圖A及第7圖B係顯示相對於從馬達電流2 9至 角度檢測訊號2 2爲止之頻率數應答之增益及相位之關係 之柏德(B 〇 d e )線圖之例子,上段爲增益,下段爲相 位。此外,第8圖A及第8圖B係顯示相對於從馬達電流 2 9至鏡子角度檢測訊號1 7 e爲止之頻率數應答之增益 及相位之關係之柏德線圖之例子,上段爲增益,下段爲相 位。 將第7圖A與第8圖A加以比較的話,兩者於3 . 8 本紙張尺度適用中國國家標準(CNS ) A4規格(210X 297公釐) —1^------#^1----,——1T------0 (請先閲讀背面之注意事項再填寫本頁) -21 - 經濟部智慧財產局員工消費合作社印製 539933 A7 ___ B7_ 五、發明説明(19) k Η z之扭轉一次共振,1 〇 k Η z之扭轉二次共振, 1 1 k Η ζ之扭轉三次共振之頻率數一致。此外,相對於 第7圖Α中於3 kH ζ具有反共振,於第8圖Α中於其附 近並不具有反共振。 做爲構造系統之振動學之知識,從柏德線圖中之共陣 與反共振之排列方式可以得知特模式之同相位性·。於第7 圖A之情況下,於剛體模式、1次共振、2次共振之間各 存在著反共振,於2次共振及3次共振之間無反共振。因 此,於光學掃描機之情況下,於移動線圏1 3與內藏角度 感應器1 6之間,1次模式與2次模式爲同相,3次模式 爲異相。 相對於此,於第8圖A之情況下,於剛體模式與1次 共振之間無反共振,於1次共振與2次共振之間存在著1 個反共振,於2次共振及3次共振之間無反共振。因此, 於光學掃描機之情況下,於移動線圈1 3與鏡子1 1之間 ,1次模式與2次模式均爲異相,3次模式爲同相。 而將第6圖所示之伺服機構適用於具有如此特性之光 學掃描機1 ,亦即,於比例補償電路2 5及角速度觀測電 路2 6不採用鏡子角度檢測値1 7 e ,而藉由採用於低次 模式(1次模式與2次模式)中同相之角度檢測訊號2 2 以進行比例補償及微分補償,可以確保伺服機構之安定性 〇 因爲於此情況下3次模式亦爲異相,爲了使伺服頻寬 變寬廣,有必要對此模式施以安定化補償。此外,即使同 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) I 裝 „ 訂 (請先閲讀背面之注意事項再填寫本頁) -22 - 539933 A7 B7 五、發明説明(20) 相模式不至於導致伺服機構不安定,但是可能會成爲導致 殘留振動使位置決定精密度降低之因素,因此有必要快速 的進行使振動衰減之補償,而可以以將電流檢測訊號3 1 做爲輸入之扭轉振動安定化補償電路3 3,來進行此補償 〇 第9圖A及第9圖B係顯不從鏡子之動作開始至停止 爲止之經過時間與位置偏差之關係,爲將位置偏差二0之 附近加以擴大之圖示。第9圖A爲顯示將本發明之扭轉振 動安定化補償電路3 3設置於1次模式〜3次模式之情況 ,第9圖B爲顯示僅進行以往的積分補償、比例補償、微 分補償(I 一 P D補償)之情況。 藉由設置扭轉振動安定化補償電路3 3,於本發明之 情況下,變爲安定的過渡應答,並到達以雷射照射位置換 算之目標位置之10#m前面約0·8ms處。另一方面 ,於以往之情況下,因爲3次模式(1 1 k Η z )爲逆相 爲不安定,因此於此共振頻率數中產生振動。. 此外本發明中,因爲是將鏡子角度回饋至角度目標値 訊號2 1並進行偏差訊號2 3之積分補償,因此可以以高 精密度之方式使鏡子停止時之雷射照射位置與目標位置一 致。 接下來針對第6圖之伺服機構中之一次傳達函數’以 乃奎斯特(N y q u i s t )之安定判定法來評估安定性之大小。 第1 0圖係爲完全無固有振動數之誤差之情況下設計 扭轉振動安定化補償電路3 3之情況之,包含1次模式之 本紙張尺度適用中國國家標準(CNS ) A4規格(2丨〇><297公釐) (請先閲讀背面之注意事項再填寫本頁)• S bucket) (Eq. 11) Therefore, once the angle target signal 2 1 is input to the feedback control system shown in Fig. 1, it is possible to suppress the mirror vibration accompanying the position-determining action. Printed by the Consumer Cooperative of the Intellectual Property Bureau of the Ministry of Economic Affairs In addition, although the notch filter has a phase delay determined by the coefficient of the denominator polynomial, the output of the target orbit 4 1 1 and the differential factor 4 1 2 and the second-order differential factor The output of 4 1 3 is added so that the denominator polynomial of the notch filter is cancelled. As a result, the phase delay from the target track 4 11 to the angle target signal 2 1 can be eliminated, and the delay in determining the position of the target track 4 11 can be reduced. As mentioned above, the bending vibration that has occurred can be controlled by feedback to reduce the paper size. Chinese paper standard (CNS) A4 (210X297 mm) -17 539933 A7 B7 V. Description of invention (15) (please first Read the notes on the back and fill in this page) Subtraction is extremely difficult, but in the present invention, 'because it is input through the feedback control system, that is, the angle target signal is generated by the mirror vibration suppression factor 4 1 2 1 'To prevent bending vibration of the rotating shaft 12' Therefore, it is possible to reduce the error of the laser light position determination of the mirror vibration. The Laplace transform of the target velocity which is the first-order derivative of the time function of the target orbit is set to V (s), and the Laplace transform of the target acceleration which is the second-order derivative of the time function of the target orbit is set to If A (s), then Equation 1 1 can be transformed into Equation 12. Κ {ή = X (s) + sX (s) + ^ rs2X (s) ^ X (s) + ^ V (s) + ^ A (s), J \ cob cob ①b • · * (Eq. 12) Economy The 5th figure printed by the Ministry of Intellectual Property Bureau's Consumer Cooperatives is a block diagram of the vibration control factor of the present invention, and is the figure implementing the 12th formula. In the figure, the gain factors 4 1 7 and 4 1 8 are the coefficients of the weights determined by the constants of the notch filter 4 1 4. If it has such a structure, it can be added by assigning weights to the target trajectory (Formula 10), the target speed (Formula 9), and the target acceleration (Formula 8), even if the notch filter cannot be realized 4 1 4 , Can also generate the mirror vibration suppression factor shown in Figure 4 and the equivalent angle target 値 signal 21. Here, the vibration suppression factors shown in Figs. 4 and 5 can be easily realized by a microprocessor. In this case, in the case where the feedback control system of FIG. 1 is analog control, the digital angle target signal is converted to an analog signal by a DA converter, and the present invention is applicable. Except for calculating the target trajectory, target speed and target acceleration, this paper size applies the Chinese National Standard (CNS) A4 specification (210X297 mm) — -18- 539933 A7 B7 V. Description of the invention (16) (Please read the back first Note: Please fill in this page again.) In addition to the calculation, you can also calculate these time series 値 in advance and store them in memory, and read out the stored data in order when the position is determined. In this case, if each target is normalized by the stroke L and memorized in the memory, the memory capacity can be reduced. In addition, it is also possible to set several kinds of action time T μ by the size of the stroke L. Furthermore, the target track is not limited to that represented by Formula 10 '. The target track can also be set to be equal to or greater than Notch filter 4 1 4 is a time waveform differentiated by the power of the denominator polynomial. In addition, if the angular vibration number ω b of the notch filter 4 1 4 is set to be equal to the natural angular vibration number of the torsional vibration of the movable part of the scanner, it is possible to reduce the torsion with a structure different from that of the torsional vibration compensation circuit described above. vibration. In this case, the servo mechanism is not limited to the servo mechanism shown in Fig. 1, but the conventional servo mechanism shown in Fig. 13 may also be used. Printed by the Intellectual Property Bureau's Consumer Cooperatives, Ministry of Economic Affairs. Figure 6 shows another embodiment of the control device of the optical scanner. In Fig. 6, in addition to the elements shown in Fig. 1, a mirror 11 and elements attached to the mirror 11 and a sensor angle detection circuit 3 5 are added. Through this, the angle detection signal 2 2 It is only supplied to the angular velocity observation circuit 32 and the proportional compensation circuit 25, and is different from the first figure in this point. The other structures are the same as those in FIG. 1, and detailed descriptions thereof are omitted here. Referring to Fig. 6, an angle sensor 16 for detecting an angle is arranged on the rotation axis 12 of the optical scanner 1. The mirror 11 includes a mirror surface that reflects laser light for processing, and a mirror surface 17a that is disposed on the surface of the mirror surface. With the mirror surface 1 7 This paper size is applicable to the Chinese National Standard (CNS) A4 specifications (2 Shu 297 mm) -19-539933 Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs A7 B7 V. Description of the invention (17) a, glowing The element 17 b and the light-receiving element 17 c are arranged. As the light-emitting element 17 b, for example, a semiconductor laser element, and as the light-receiving element 1 7 c, for example, a P S D (Position Sensitive Device) element can be used. Ο The following describes the signal flow and servo mechanism. The mirror angle detection signal 17e (voltage signal proportional to the angle of the mirror 11) output from the light receiving element 17C is amplified by the amplifier 17d, and is negatively fed back to the mirror angle The angle target 値 signal 21 output from the command circuit 20 is generated, and the deviation signal 23 is generated. In order to make the angle of the mirror 1 1 follow the angular target 値 that does not produce a normal deviation, the deviation signal 2 3 is integrated by an integral compensation circuit 24 to form a type 1 servo system. In addition, in order to ensure the stability of this servo mechanism, the angle detection signal 22 is input to the proportional compensation circuit 25 and the angular velocity observation circuit 32, and the sum of the output signals of these circuits and the torsional vibration stabilization compensation circuit 3 is input. The output signal 3 3 a of 3 is subtracted from the output signal of the integral compensation circuit 24 and used as the control input signal 27. The motor drive circuit 28 supplies a motor drive current 2 9 proportional to the control input signal 27 to the optical scanner 1. The motor driving current 2 9 flows into the moving line 圏 1 3, and a driving torque proportional to the current 产生 is generated in the moving line 圏 1 3. By doing so, the torsional vibration of the rotating shaft 12 can be reduced. Here, in the case where the motor driving circuit 28 is a current control mode, generally, because the driving torque of the moving coil 13 is proportional to the motor driving current 29, it can be obtained by measuring the motor driving current 29. It is known that the paper size is applicable to the Chinese National Standard (CNS) A4 specification (21〇 > < 297 mm) --------- ^ ΙΙΓ Packing ----: --- Order ------ -I (Please read the notes on the back before filling out this page) -20- 539933 Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs A7 B7 V. Description of the invention (18) The driving torque of the moving coil 13. The current detection signal 3 1 which is proportional to 値 of the motor drive current 2 9, for example, the motor drive current 2 9 flows to a current detection resistor with a small resistance 値 (0 · 1 to several Ω or less). The voltage between the terminals of the resistor is input to the differential input type subtraction circuit, which can be obtained as the output of the differential input type subtraction circuit. Then, a current detection signal 3 1 proportional to the magnitude of the motor drive current 29 is input to the angular velocity observation circuit 32 and the torsional vibration stabilization compensation circuit 33. The position of the rotating shaft 12 detected by the angle sensor is output as an angle detection signal 22 from the sensor angle detection circuit 35. Then, the angle detection signal 2 2 is input to the proportional compensation circuit 25 and the angular velocity observation circuit 32. Next, for the description of the torsional vibration stabilization compensation circuit 33, reference may be made to the description of the torsional vibration primary compensation circuit 33 of FIG. 1 already described. Next, based on a specific example of an optical scanner, the torsional vibration characteristics of the movable part and the stability of the servo mechanism will be described. Figure 7A and Figure 7B are examples of Bode line diagrams showing the relationship between the gain and phase of the frequency response from the motor current 29 to the angle detection signal 22. The upper paragraph is Gain, the lower stage is phase. In addition, Fig. 8A and Fig. 8B are examples of Bird's-line diagrams showing the relationship between the gain and phase with respect to the frequency response from the motor current 29 to the mirror angle detection signal 17e. The upper section is the gain. , The lower section is phase. Comparing Figure 7A and Figure 8A, the two papers are applicable to the Chinese paper standard (CNS) A4 (210X 297 mm) at 3.8 paper size. —1 ^ ------ # ^ 1 ----, ---- 1T ------ 0 (Please read the notes on the back before filling this page) -21-Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs 539933 A7 ___ B7_ V. Description of the invention ( 19) The frequency of k Η z torsional primary resonance, 10 k Η z torsional second resonance, and the frequency of 1 k Η ζ torsional third resonance are the same. In addition, in FIG. 7A, there is an antiresonance at 3 kH ζ, and in FIG. 8A, there is no antiresonance. As a knowledge of the vibrational system of the construction system, the same phase of the special mode can be obtained from the arrangement of the co-matrix and antiresonance in the Bird diagram. In the case of FIG. 7A, there is an antiresonance between the rigid body mode, the first resonance, and the second resonance, and there is no antiresonance between the second resonance and the third resonance. Therefore, in the case of an optical scanner, between the moving line 13 and the built-in angle sensor 16, the primary mode and secondary mode are in phase, and the tertiary mode is out of phase. On the other hand, in the case of FIG. 8A, there is no antiresonance between the rigid body mode and the first resonance, there is one antiresonance between the first resonance and the second resonance, and the second resonance and the third resonance exist. There is no antiresonance between the resonances. Therefore, in the case of an optical scanner, between the moving coil 13 and the mirror 11, the primary mode and secondary mode are out of phase, and the tertiary mode is in phase. And the servo mechanism shown in FIG. 6 is applied to the optical scanner 1 having such characteristics, that is, the proportional compensation circuit 25 and the angular velocity observation circuit 2 6 do not use the mirror angle detection 値 1 7 e, but by using In the low-order mode (1st mode and 2nd mode), the same phase angle detection signal 2 2 is used for proportional compensation and differential compensation, which can ensure the stability of the servo mechanism. In this case, the 3rd mode is also out of phase. To widen the servo bandwidth, it is necessary to apply stabilization compensation to this mode. In addition, even if the Chinese paper standard (CNS) A4 size (210X297 mm) is applied to the same paper size, I order (please read the precautions on the back before filling this page) -22-539933 A7 B7 V. Description of the invention (20 ) The phase mode does not cause the servo mechanism to be unstable, but it may become a factor that causes the residual vibration to reduce the precision of the position determination. Therefore, it is necessary to quickly compensate the attenuation of the vibration, and the current detection signal 3 1 can be used as The input torsional vibration stabilization compensation circuit 3 3 performs this compensation. Figures 9A and 9B show the relationship between the elapsed time from the start of the mirror to the stop and the position deviation. The diagram is enlarged in the vicinity of 0. Fig. 9A shows the case where the torsional vibration stabilization compensation circuit 33 of the present invention is set in the primary mode to the third mode, and Fig. 9B shows only the conventional integration. Compensation, proportional compensation, differential compensation (I-PD compensation). By setting the torsional vibration stabilization compensation circuit 3 3, in the case of the present invention, it becomes a stable transition. Answer, and reach about 0.8ms before 10 # m of the target position converted by laser irradiation position. On the other hand, in the past, because the 3rd mode (1 1 k Η z) is inverse phase, it is not The vibration is stable in this resonance frequency. In addition, in the present invention, because the mirror angle is fed back to the angle target 値 signal 2 1 and the integral compensation of the deviation signal 2 3 is performed, it can be made with high precision The laser irradiation position when the mirror is stopped is consistent with the target position. Next, the stability function of Nyquist is used to evaluate the stability function of the first-time transfer function in the servo mechanism of Fig. 6. Part 1 Figure 0 shows the design of a torsional vibration stabilization compensation circuit without any error in the natural vibration number. In the case of 3 3, the paper size including the primary mode is applicable to the Chinese National Standard (CNS) A4 specification (2 丨 〇 > < 297 mm) (Please read the notes on the back before filling out this page)
、T d 經濟部智慧財產局員工消費合作社印製 -23- 539933 A7 B7 _ 五、發明説明(21) (請先閲讀背面之注意事項再填寫本頁) 固有振動數(3 · 8kHz)之頻率數範圍(1kHz〜 7 k Η z )之乃奎斯特(Nyguist )軌跡。實線爲適用對於 1次模式之安定化補償之情況,虛線爲以往之對於1次模 式未進行安定化補償之情況。 無安定化補償之情況之軌跡從(1)進行至(2), 之後離開此圖之外框並描繪了順時針之圓形軌跡,然後再 返回框內到達(3 )。此圓形軌跡意味著於1次共振附近 ,增益逐漸變高之意思。此外,此軌跡接近於座標( - 1 ,0 )之安定判別點,其相位寬裕度非常小。另一方 面,適用安定化補償之情況下,從原點至軌跡之距離變小 ,相對於安定判別點之相位寬裕度及增益寬裕度均變大。 因此,無固有振動數之誤差之補償電路具有藉由抑制共振 .峰値使伺服系統之安定性增加之效果。 經濟部智慧財產局員工消費合作社印製 於設計扭轉振動安定化補償電路3 3之情況,有必要 測定欲進行補償之振動模式之固有振動數。欲進行補償之 振動模式之固有振動數,可藉由測定第7圖A所示之頻率 數應答來得知。然而此測定精密度是取決於所採用之測定 器(例如伺服分析器)之性能與分解功能,必定會包含誤 差。此外,光學掃描機之固有振動數本身並不經常維持固 定’亦須考慮馬達之熱量產生等之影響所造成之變動。即 使具有如此之誤差與變動亦可保持控制之安定性者,爲較 具實用性。 以下,針對扭轉振動之頻率數之誤差,具有安定性之 伺服機構之構成加以說明。 本紙張尺度適用中國國家標準(CNS ) A4規格(210 X 297公釐) 539933 A7 _ B7 五、發明説明(22) (請先閲讀背面之注意事項再填寫本頁) 第1 1圖係爲將扭轉振動安定化補償電路3 3之固有 振動數,移至低於實際之1次模式之固有振動數3 . 8 kHz 之 5% (190kHz)之 3 . 61kHz 之扭轉 振動安定化補償電路3 3之情況下之,包含1次模式之固 有振動數(3 . 8 k Η z )之乃奎斯特(Nyquist )軌跡, 實線爲適用對於1次模式之安定化補償之情況,虛線爲以 往之對於1次模式未進行安定化補償(與第1 0圖之虛線 相同軌跡)之情況。 適用安定化補償之情況之軌跡從(1 )進行至(4 ) ’之後離開此圖之外框並描繪了順時針之圓形軌跡,然後 再返回框內到達(5 )。從原點至軌跡之距離並不如第 1 0圖般那麼大,但與無安定化補償之情況互相比較更接 近1次共振之附近之相位,因此相對於安定判別點之相位 寬裕度變大。其結果爲,可以增大伺服系統之安定性。 經濟部智慧財產局員工消費合作社印製 可以增大伺服系統之安定性之理由如下。於固有振動 數中,此補償電路於比固有振動數還低之頻率區域中,使 相位產生最大約9 0度爲止之延遲,於高頻率區域中,使 相位產生最大約9 0度爲止之前進。因此,於實際之模式 之固有振動數比補償電路之固有振動數相對較高之情況下 ,於此模式之共振點附近當中,乃奎斯特(Nyquist)軌跡 之相位產生前進。 如此,扭轉振動安定化補償電路3 3可以做爲相對於 共振之相位補償器來加以利用。此外,藉由將補償電路之 固有振動數挪至實際測得之値來設計,可以實現針對振動 本紙張尺度適用中國國家標準(CNS ) A4規格(21〇Χ297公釐) - 25- 經濟部智慧財產局員工消費合作社印製 539933 A7 B7 五、發明説明(二) 數之誤差與變動之安定的伺服機構。 於此例中,因爲1次模式爲同相,因此設定爲將補償 電路之固有振動數挪至低頻率區域並形成相位前進’而於 使逆向模式(例如3次模式)加以安定化之情況下則設定 爲將電路之固有振動數挪至高頻率區域並形成相位延遲。 此外,振動數之差距値之正負,係使相位寬裕度變大 之方式因應模式之同相、異相來決定。而差距値之大小則 有必要以,即使產生所假定之最大誤差及變動,亦能夠使 實際之固有振動數與補償電路之固有振動數不產生反轉之 方式來決定。 【圖面之簡單說明】: 第1圖係爲本發明之光學掃描機之控制磚塊圖。 第2圖係爲本發明之扭轉r次補償電路之接續圖。 第3圖係爲本發明之角速度觀測電路之接續圖。 第4圖係爲本發明之振動控制因子之碍塊圖。 第5圖係爲本發明之振動控制因子之其他磚塊圖。 第6圖係爲本發明之光學掃描機之其他控制磚塊圖。 第7圖A及第7圖B係顯示相對於從馬達電流至角度 檢測訊號爲止之頻率數應答之增益及相位之關係之柏德( B 〇 d e )線圖之例子。 第8圖A及第8圖B係顯示相對於從馬達電流至鏡子 角度檢測訊號爲止之頻率數應答之增益及相位之關係之柏 德線圖之例子。 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) I--------^-裝----Ί.--訂-------J (請先閱讀背面之注意事項再填寫本頁) -26- 539933 A7 B7 五、發明説明(: 4) 第9圖A及第9圖B係顯示從鏡子之動作開始至停止 爲止之經過時間與位置偏差之關係。 第1 0圖係爲完全無固有振動數之誤差之情況下之乃 奎斯特(N y q u i s t )軌跡。 第1 1圖係爲將固有振動數挪至實際之1次模式之固 有振動數之情況下之乃奎斯特(Nyquist)軌跡。 第1 2圖係爲光學掃描機中之可動部分之構成圖。 第1 3圖係爲光學掃描機之控制磚塊圖。 主要元件對照表 1 經濟部智慧財產局員工消費合作社印製 1 4,1 5 1 6,3 5 17a,17b,17c,17d 1 7 e 2 0 2 1 2 2 2 3 2 4 2 5 光學掃描機 鏡子 旋轉軸 移動線圈 軸承 旋轉軸角度檢測手段 鏡子角度檢測手段 鏡子角度檢測値 鏡子角度指令電路 角度目標値訊號 角度檢測訊號 偏差訊號 積分補償電路 比例補償電路 裝 ^ 訂 . , (請先閱讀背面之注意事項再填寫本頁) 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) -27- 539933 A7 B7 五、發明説明(」 2 6 2 7 2 8 2 9 2 經濟部智慧財產局員工消費合作社印製 321,322,323,33 1,332 324 、 325 、 333 、 334 、 335 3 4 3 5 4 1 4 11 4 12 4 13 4 14 4 1 7,4 1 8 4 2 C 0 1 , C 0 2 , C 1 1 微分補償電路 控制輸入訊號 馬達驅動電路 馬達驅動電流 電流檢測訊號 角速度觀測電路 扭轉振動一次補償電路 輸出訊號 端子 運算放大器 扭轉振動二次補償電路 感應器角度檢測電路 鏡子振動抑制因子 目標軌道 微分因子 二階微分因子 陷波濾波器 增益因子 補正値 電容器 R〇l,R〇2,R〇3,R〇4,R〇5,R〇6,Rll,Rl2,Rl3,Rl4,Rl5,Rl 電阻 I-------^裝----:—訂—----- (請先閱讀背面之注意事項再填寫本頁) 本紙張尺度適用中國國家標準(CNS ) A4規格(210X297公釐) -28-, T d Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs -23- 539933 A7 B7 _ V. Description of the invention (21) (Please read the precautions on the back before filling this page) Frequency of natural vibration (3 · 8kHz) Nyguist trace in the range of numbers (1kHz ~ 7 k Η z). The solid line is the case where the stabilization compensation for the primary mode is applied, and the dashed line is the case where the stabilization compensation is not performed for the primary mode in the past. In the case of no stabilization compensation, the trajectory proceeds from (1) to (2), then leaves the frame outside the figure and traces the clockwise circular trajectory, and then returns to the frame to reach (3). This circular trajectory means that the gain gradually increases near the first resonance. In addition, this trajectory is close to the stability discrimination point of coordinates (-1, 0), and its phase margin is very small. On the other hand, when the stabilization compensation is applied, the distance from the origin to the trajectory becomes smaller, and the phase margin and gain margin relative to the stability discrimination point become larger. Therefore, the compensation circuit without the error of the natural vibration number has the effect of increasing the stability of the servo system by suppressing the resonance peaks. Printed by the Consumer Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs. When designing a torsional vibration stabilization compensation circuit 33, it is necessary to measure the natural vibration number of the vibration mode to be compensated. The natural vibration number of the vibration mode to be compensated can be obtained by measuring the frequency response shown in Fig. 7A. However, the accuracy of this measurement depends on the performance and resolution of the used analyzer (such as a servo analyzer), and it will necessarily include errors. In addition, the inherent vibration number of the optical scanner does not always remain fixed. It must also take into account changes caused by the heat generated by the motor. Those who can maintain the stability of control even with such errors and changes are more practical. In the following, the error of the frequency of torsional vibration and the structure of a stable servo mechanism will be described. This paper size applies Chinese National Standard (CNS) A4 specification (210 X 297 mm) 539933 A7 _ B7 V. Description of the invention (22) (Please read the precautions on the back before filling this page) Figure 1 1 The natural vibration number of the torsional vibration stabilization compensation circuit 3 3 is lower than the actual natural vibration number of the primary mode 3. 8 kHz to 5% (190 kHz) 3. 3. 61 kHz torsional vibration stabilization compensation circuit 3 3 to In this case, the Nyquist trajectory that includes the natural vibration number (3.8 k Η z) of the primary mode. The solid line is the case where the stabilization compensation is applied to the primary mode. When the stabilization mode is not performed in the primary mode (the same trajectory as the dotted line in Fig. 10). When the stabilization compensation is applied, the trajectory goes from (1) to (4) ', then leaves the frame outside the figure and traces the clockwise circular trajectory, and then returns to the frame to reach (5). The distance from the origin to the trajectory is not as large as in Figure 10, but compared with the case without stabilization compensation, it is closer to the phase near the first resonance, so the phase margin relative to the stability discrimination point becomes larger. As a result, the stability of the servo system can be increased. Printed by the Employees' Cooperatives of the Intellectual Property Bureau of the Ministry of Economic Affairs The reasons for increasing the stability of the servo system are as follows. In the natural vibration number, this compensation circuit advances the phase to a maximum of approximately 90 degrees in a frequency region lower than the natural vibration number, and advances in a high-frequency region to a phase of approximately 90 degrees. . Therefore, when the natural vibration number of the actual mode is relatively higher than the natural vibration number of the compensation circuit, the phase of the Nyquist trajectory progresses in the vicinity of the resonance point of this mode. Thus, the torsional vibration stabilization compensation circuit 33 can be used as a phase compensator with respect to resonance. In addition, by designing the natural vibration number of the compensation circuit to the actual measured value, the Chinese National Standard (CNS) A4 specification (21〇 × 297 mm) can be applied to the paper size of the paper. Printed by the Consumer Cooperative of the Property Bureau 539933 A7 B7 V. Description of the invention (2) The stable servo mechanism of the error and change of the number. In this example, since the primary mode is in phase, it is set to move the natural frequency of the compensation circuit to a low-frequency region and form a phase advance. When the reverse mode (such as the third mode) is stabilized, It is set to move the natural vibration number of the circuit to a high frequency region and form a phase delay. In addition, the difference between the number of vibrations and the positive and negative values is determined by the method of increasing the phase margin in accordance with the in-phase and out-of-phase modes. The magnitude of the gap 値 must be determined in such a way that the actual natural vibration number and the natural circuit vibration number of the compensation circuit do not reverse even if the assumed maximum error and variation occur. [Brief description of the drawing]: Figure 1 is a control block diagram of the optical scanner of the present invention. Fig. 2 is a continuation diagram of the torsion r-time compensation circuit of the present invention. FIG. 3 is a continuation diagram of the angular velocity observation circuit of the present invention. Figure 4 is a block diagram of the vibration control factor of the present invention. Figure 5 is another block diagram of the vibration control factor of the present invention. Fig. 6 is another control block diagram of the optical scanner of the present invention. FIG. 7A and FIG. 7B are examples of a Bode (B o d e) diagram showing the relationship between the gain and the phase of the frequency response from the motor current to the angle detection signal. Fig. 8A and Fig. 8B are examples of Bird diagrams showing the relationship between the gain and the phase of the frequency response from the motor current to the detection signal at the angle of the mirror. This paper size applies to Chinese National Standard (CNS) A4 specification (210X297 mm) I -------- ^-Packing ---- Ί .-- Order ------- J (Please read first Note on the back, please fill out this page) -26- 539933 A7 B7 V. Description of the invention (: 4) Figure 9A and 9B show the relationship between the elapsed time and position deviation from the start of the mirror to the stop. . Fig. 10 is a quiz (N y q u i s t) locus in the case where there is no error in the natural vibration number at all. Fig. 11 is the Nyquist trajectory when the natural vibration number is shifted to the actual vibration number of the primary mode. Fig. 12 is a structural diagram of a movable part in the optical scanner. Figure 13 is a control block diagram of the optical scanner. Comparison table of main components 1 Printed by the Consumer Cooperative of Intellectual Property Bureau of the Ministry of Economic Affairs 1 4, 1 5 1 6, 3 5 17a, 17b, 17c, 17d 1 7 e 2 0 2 1 2 2 2 3 2 4 2 5 Optical scanner Mirror rotation axis, moving coil bearing, rotation axis angle detection means, mirror angle detection means, mirror angle detection, mirror angle command circuit, angle target, signal angle detection, signal deviation, signal integral compensation circuit, proportional compensation circuit assembly, (Please read the note on the back first Please fill in this page again for this matter) This paper size applies Chinese National Standard (CNS) A4 specification (210X297mm) -27- 539933 A7 B7 V. Description of invention ("2 6 2 7 2 8 2 9 2 Employees of Intellectual Property Bureau, Ministry of Economic Affairs Printed by Consumer Cooperatives 321, 322, 323, 33 1, 332 324, 325, 333, 334, 335 3 4 3 5 4 1 4 11 4 12 4 13 4 14 4 1 7, 4 1 8 4 2 C 0 1, C 0 2, C 1 1 differential compensation circuit control input signal motor drive circuit motor drive current detection signal angular velocity observation circuit primary torsional vibration compensation circuit output signal terminal operational amplifier torsional vibration secondary compensation circuit Reactor angle detection circuit, mirror vibration suppression factor, target orbit differential factor, second-order differential factor, notch filter, gain factor correction, capacitors R01, R02, R03, R04, R05, R06, R11 , Rl2, Rl3, Rl4, Rl5, Rl resistance I ------- ^ install ----:-order ------- (Please read the precautions on the back before filling this page) The paper size Applicable to China National Standard (CNS) A4 specification (210X297 mm) -28-
Claims (1)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
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JP2000231769A JP4233202B2 (en) | 2000-07-31 | 2000-07-31 | Control device for optical scanner device |
JP2000231760A JP3986241B2 (en) | 2000-07-31 | 2000-07-31 | Control device for optical scanner device |
Publications (1)
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TW539933B true TW539933B (en) | 2003-07-01 |
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TW90129323A TW539933B (en) | 2000-07-31 | 2001-11-27 | Controller for optical scanner |
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Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN117806026A (en) * | 2024-02-28 | 2024-04-02 | 安徽瑞控信光电技术股份有限公司 | High-precision light beam switching device and quick reflection mirror |
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Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN117806026A (en) * | 2024-02-28 | 2024-04-02 | 安徽瑞控信光电技术股份有限公司 | High-precision light beam switching device and quick reflection mirror |
CN117806026B (en) * | 2024-02-28 | 2024-05-03 | 安徽瑞控信光电技术股份有限公司 | High-precision light beam switching device and quick reflection mirror |
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