JPS63109960A - Optional angle profile system in profile control - Google Patents
Optional angle profile system in profile controlInfo
- Publication number
- JPS63109960A JPS63109960A JP25547286A JP25547286A JPS63109960A JP S63109960 A JPS63109960 A JP S63109960A JP 25547286 A JP25547286 A JP 25547286A JP 25547286 A JP25547286 A JP 25547286A JP S63109960 A JPS63109960 A JP S63109960A
- Authority
- JP
- Japan
- Prior art keywords
- axis
- operating part
- velocity
- angle
- velocity component
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
- 238000009825 accumulation Methods 0.000 claims abstract description 7
- 238000000034 method Methods 0.000 claims description 9
- 238000010586 diagram Methods 0.000 description 5
- 230000029777 axis specification Effects 0.000 description 4
- 239000000700 radioactive tracer Substances 0.000 description 4
- 241001422033 Thestylus Species 0.000 description 2
- 230000001186 cumulative effect Effects 0.000 description 2
- 238000001514 detection method Methods 0.000 description 2
- 238000006073 displacement reaction Methods 0.000 description 2
- 241001494479 Pecora Species 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
Abstract
Description
【発明の詳細な説明】
(発明の技術分野)
本発明は、倣い制御装置によって任意角度の表面倣いを
行なう場合の、累積誤差を生じないようにした倣い制御
における任意角度倣い方式(発明の技術的背景とその問
題点)
倣い制御装置によるモデルの表面倣いで任意角度倣いを
行なう場合、従来は第5図に示すようにある時点に求め
た目標位置(トレースフィード開始位置)poに対し、
次の目標位a P 1を所定の角度演算によって求める
ようにしているが、この演算を各目標位置毎に(P2.
P3.・・・)順次繰返して行なうと演算誤差Δθの累
積によって、目標進行方向0νに対して実際の進行方向
RVが誤差eのように累積されていた。これは、XY平
面上の速度成分VXYを第4図に示すような演算式で、
X軸速度成分vX及びYfIII速度成分瞥に分解する
と共に、点Pn(Xo、Y、)はで求めており、三角関
数等のディジタル計算に基づく数値の切捨ないしは四捨
五入等の演算誤差Δθが常に生じるのである。かかる演
算誤差Δθの各目標位置における累積によって、実際の
進行方向nvが、目標進行方向DVに対して次第に大き
くずれてしまうことが問題となっていた。Detailed Description of the Invention (Technical Field of the Invention) The present invention relates to an arbitrary angle scanning method (technology of the invention) in scanning control that prevents cumulative errors from occurring when a scanning control device performs surface scanning at an arbitrary angle. Background and problems) When performing arbitrary angle scanning by scanning the surface of a model using a scanning control device, conventionally, as shown in Fig. 5, for the target position (trace feed start position) po obtained at a certain point,
The next target position a P 1 is determined by a predetermined angle calculation, but this calculation is performed for each target position (P2.
P3. ...) If the calculations were repeated in sequence, the actual traveling direction RV would be accumulated as an error e with respect to the target traveling direction 0v due to the accumulation of calculation errors Δθ. This is the calculation formula for the velocity component VXY on the XY plane as shown in Figure 4.
In addition to decomposing the X-axis velocity component vX and the YfIII velocity component, the point Pn (Xo, Y,) is determined by It happens. A problem has been that the actual traveling direction nv gradually deviates greatly from the target traveling direction DV due to the accumulation of such calculation errors Δθ at each target position.
(発明の目的)
本発明は上述のような事情よりなされたものであり、本
発明の目的は、累積誤差が生じないように常に基準点に
基づいて演算を行ない、任意角度の倣いを誤差が生じる
ことなく行ない得るようにした任意角度倣い方式を提供
することにある。(Object of the Invention) The present invention was made in view of the above-mentioned circumstances, and an object of the present invention is to always perform calculations based on a reference point so as to avoid cumulative errors, and to perform scanning at arbitrary angles without errors. It is an object of the present invention to provide an arbitrary angle scanning method that can be scanned without any occurrence of curvature.
(発明の概要)
本発明は倣い制御における任意角度倣い方式に関するも
ので、倣い制御装置によって任意角度の表面倣いを行な
う場合、常にトレースフィード開始位置を起点として、
従方向軸に誤差補正項を入れることにより、演算誤差の
累積をなくして二定誤差内の角度で倣い制御を行ない得
るようにしたものである。(Summary of the Invention) The present invention relates to an arbitrary-angle scanning method in scanning control, and when a scanning control device performs surface scanning at an arbitrary angle, the trace feed start position is always used as the starting point.
By inserting an error correction term in the slave direction axis, the accumulation of calculation errors is eliminated and scanning control can be performed at an angle within a two-dimensional error.
(発明の実施例)
第1図は本発明方式を実現する装置の構成例を示してお
り、モデル1をトレーサヘッド2がスタイラス2八を介
して倣い、そのXYZ軸の変位量EX、E、、a、はそ
れぞれ倣い演算部10に人力され、倣い演算部lOで演
算されたXY各軸の各速度指令り八X及びDAYがドラ
イブユニット5に人力され、ドライブユニット5がモー
タ3を駆動することによって、モータ3に連結されたト
レーサヘッド2がモデル1の表面を倣うようになってい
る。又、モータ3には位置検出器4が連結されて倣い位
置を検出するようになっており、位置検出器4の位置検
出信号psは倣い演算部10内の指令演算部14に人力
されている。さらに、倣い演算部10は後述する演算部
11及び12を有し、更に第2図にその詳細を示す角度
演算部13と、速度指令DAX、DAYを演算する指令
演算部14とを有している。すなわち、角度演算部13
は第2図に示すように主方向軸判定部131 と、X@
が主方向軸と判定された場合(この場合、Y釉が従方向
軸となる)の目標値演算部132と、Y軸が主方向軸と
判定された場合(この場合、X軸が従方向軸となる)の
目標値演算部133と、X軸の速度v×及びY軸の速度
vYを演算する速度演算部134 とで構成されている
。(Embodiment of the Invention) FIG. 1 shows an example of the configuration of an apparatus for realizing the method of the present invention, in which a tracer head 2 traces a model 1 via a stylus 28, and the displacement EX, E, , a, are manually inputted to the copying calculation unit 10, and the respective speed commands for each of the X and Y axes calculated by the copying calculation unit IO are inputted to the drive unit 5. , a tracer head 2 connected to a motor 3 traces the surface of the model 1. Further, a position detector 4 is connected to the motor 3 to detect the scanning position, and the position detection signal ps of the position detector 4 is manually inputted to the command calculation section 14 in the scanning calculation section 10. . Further, the tracing calculation unit 10 has calculation units 11 and 12, which will be described later, and further includes an angle calculation unit 13, the details of which are shown in FIG. 2, and a command calculation unit 14, which calculates speed commands DAX and DAY. There is. That is, the angle calculation section 13
As shown in FIG. 2, the main direction axis determination unit 131 and
is determined to be the main direction axis (in this case, the Y glaze is the subordinate direction axis), and when the Y axis is determined to be the main direction axis (in this case, the X axis is the subordinate direction axis). The target value calculation section 133 is configured to calculate the speed vX of the X axis and the speed vY of the Y axis.
このような構成において、トレーサヘッド2かスタイラ
ス2Aを介してモデルlの表面を倣って得られるXYZ
@ノ変位量EX、EY、EZより、モデル1の形状やス
タイラス2Aとモデル1の接触状況を識別することがで
きる。このため、倣い速度指令V。を基準にしてモデル
1の接線方向速度VT及び法線方向速度vNを、倣い演
算部lO内の7可算部11で求める。これら速度VT、
VNは演算部12てXY平面上の速度成分VXYとZ!
N1方向の速度成分v2とに分解され、Z軸速度成分v
2は指令演算部14に人力され、XY平面上の速度成分
VXYは角度演算部13に人力されて、主方向軸判定部
131て主方向軸の判定が行なわれる。この場合、移動
量の多い方の軸が主方向軸と判定され、移動ユの少ない
方の軸が従方向軸とされる。例えば、任意角度倣いにお
けるX@から反時計方向の指定角度をθとすれば、
の時にX軸が主方向軸となり、Y・袖が従方向軸とされ
る。又、
45°〈θ≦135°、225°くθ≦315゜・・・
・・・・・・(2)
の時にY軸が主方向軸となり、X軸が従方向軸とされる
。このような上記(1)及び(2)式になる主方向軸の
判定を、主方向・釉判定部131が行なうことになる。In such a configuration, the XYZ data obtained by tracing the surface of the model l using the tracer head 2 or the stylus 2A
The shape of the model 1 and the contact situation between the stylus 2A and the model 1 can be identified from the displacement amounts EX, EY, and EZ. Therefore, the copying speed command V. The tangential direction velocity VT and normal direction velocity vN of the model 1 are determined by the 7-countable unit 11 in the tracing calculation unit 1O using as a reference. These speeds VT,
VN is the velocity component VXY and Z! on the XY plane calculated by the calculation unit 12.
It is decomposed into a velocity component v2 in the N1 direction, and a velocity component v2 in the Z-axis direction.
2 is manually inputted to the command calculation unit 14, the velocity component VXY on the XY plane is inputted manually to the angle calculation unit 13, and the main direction axis determination unit 131 determines the main direction axis. In this case, the axis with the larger amount of movement is determined to be the main direction axis, and the axis with the smaller amount of movement is determined to be the subordinate direction axis. For example, if the specified angle in the counterclockwise direction from X@ in arbitrary angle scanning is θ, then the X axis becomes the main direction axis and the Y/sleeve becomes the subordinate direction axis. Also, 45°〈θ≦135°, 225°〈θ≦315°...
......(2) At the time of (2), the Y-axis becomes the main direction axis and the X-axis becomes the subordinate direction axis. The main direction/glaze determination unit 131 determines the main direction axes according to equations (1) and (2) above.
そして、例えば主方向軸がX・袖の時、XY座標の目標
値×。、Ynを
に従って目標値演算部132で計算する。又この時のX
Y各軸の速度Vx、V、は、
と速度演算部134で計算される。これは、第3図のト
レースフィード開始位置P。(Xo、Yo)は目標位置
P。(Xn、Yn)に対して
Yn −(Xn −Xo)tanθ ・・・・
・・・・・(5)の関係を有していることに基づく。For example, when the main direction axis is X/sleeve, the target value of the XY coordinates is ×. , Yn are calculated by the target value calculating section 132 according to the following. X again at this time
The speeds Vx, V, of each Y axis are calculated by the speed calculation unit 134 as follows. This is the trace feed start position P in FIG. (Xo, Yo) is the target position P. Yn - (Xn - Xo) tanθ for (Xn, Yn)...
...Based on having the relationship (5).
このようにして求められた速度指令VX及びvYは指令
演算部14に入力され、XY各軸を駆動するドライブユ
ニット5に速度指令DAX及びI)AYとして与えられ
る。XY各軸の移動に応じて、モータ3に連結された位
置検出器4から位置検出信号PSが指令演算部14にフ
ィードバックされ、目標値xrl及びyI、と比較され
、もし誤差が有ればこの誤差を打消す成分が指令演算部
14で計算され、速度指令り八X及び〇AYとして出力
するような位置制御が行なわれる。このようにして任意
方向倣いにおいても指定方向に対し、常にトレースフィ
ード開始位置P0を基準にして目標値を定めているので
、誤差の累積しない倣い制御を実現することができる。The speed commands VX and vY thus obtained are input to the command calculation section 14, and are given as speed commands DAX and I)AY to the drive unit 5 that drives each of the X and Y axes. In accordance with the movement of each of the X and Y axes, the position detection signal PS from the position detector 4 connected to the motor 3 is fed back to the command calculation unit 14, and is compared with the target values xrl and yI, and if there is an error, this signal is A component for canceling the error is calculated by the command calculation unit 14, and position control is performed such that the speed command is output as 8X and 0AY. In this way, even when scanning in any direction, the target value is always determined for the designated direction based on the trace feed start position P0, so that scanning control without accumulation of errors can be realized.
また、上述の角度演算部13の主方向軸判定部131に
おいて、主方向軸がYitI[hと判定され、X軸が従
方向軸とされた場合には、目標値演算部133は
の演算をすることになる。Furthermore, when the main direction axis determination section 131 of the angle calculation section 13 described above determines that the main direction axis is YitI[h and the X axis is set as the subordinate direction axis, the target value calculation section 133 performs the calculation of I will do it.
尚、第3図における直j−JDRが目標進行方向を示し
ており、トレースフィード開始位置P0に対して目標点
Pnを上記(3)式又は(6)式で計算することにより
、誤差は累積することがない。Note that the straight j-JDR in Fig. 3 indicates the target traveling direction, and by calculating the target point Pn with respect to the trace feed start position P0 using the above equation (3) or (6), the error can be accumulated. There's nothing to do.
(発明の効果)
以上のように本発明の任意角度倣い方式によれば、従方
向軸に誤差補正項を入れているので演算誤差の累積が無
くなり、一定額差内の角度で倣い制御を行なうことが可
能となる。(Effects of the Invention) As described above, according to the arbitrary angle scanning method of the present invention, since the error correction term is included in the slave direction axis, there is no accumulation of calculation errors, and scanning control is performed at an angle within a certain amount difference. becomes possible.
第1図はこの発明方式を実現する装置の一例を示すブロ
ック構成図、第2図はその角度演算部の詳細を示すブロ
ック図、第3図はこの発明方式の原理を説明するための
図、第4図は従来の角度演算の式を示す図、第5図は従
来における任意角度倣い方式を説明するための図である
。
1・・・モデル、2・・・トレーサヘッド、3・・・モ
ータ、4・・・位置検出器、5・・・ドライブユニット
、lO・・・倣い演算部、11.12・・・演算部、1
3・・・角度演算部、14・・・指令演算部、131・
・・主方向軸判定部、132.133・・・目標値演算
部、134・・・速度演算部。
出願人代理人 安 形 雄 三
tj
茶2図
羊3面FIG. 1 is a block diagram showing an example of a device for realizing the method of this invention, FIG. 2 is a block diagram showing details of the angle calculation section, and FIG. 3 is a diagram for explaining the principle of the method of this invention. FIG. 4 is a diagram showing a conventional angle calculation formula, and FIG. 5 is a diagram for explaining a conventional arbitrary angle scanning method. DESCRIPTION OF SYMBOLS 1...Model, 2...Tracer head, 3...Motor, 4...Position detector, 5...Drive unit, lO...Copy calculation section, 11.12...Calculation section, 1
3... Angle calculation section, 14... Command calculation section, 131.
...Main direction axis determination section, 132.133...Target value calculation section, 134...Speed calculation section. Applicant's representative Yasugata Yu 3tj brown 2 figures sheep 3 pages
Claims (1)
、常にトレースフィード開始位置を起点として、従方向
軸に誤差補正項を入れることにより、演算誤差の累積を
なくして一定誤差内の角度で倣い制御を行ない得るよう
にしたことを特徴とする倣い制御における任意角度倣い
方式。When performing surface scanning at an arbitrary angle using a scanning control device, by always using the trace feed start position as the starting point and inserting an error correction term in the slave direction axis, it is possible to eliminate the accumulation of calculation errors and control scanning at an angle within a certain error. An arbitrary angle scanning method in scanning control, which is characterized in that it can perform
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP61255472A JP2515518B2 (en) | 1986-10-27 | 1986-10-27 | Arbitrary angle scanning method in scanning control |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP61255472A JP2515518B2 (en) | 1986-10-27 | 1986-10-27 | Arbitrary angle scanning method in scanning control |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS63109960A true JPS63109960A (en) | 1988-05-14 |
JP2515518B2 JP2515518B2 (en) | 1996-07-10 |
Family
ID=17279240
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP61255472A Expired - Lifetime JP2515518B2 (en) | 1986-10-27 | 1986-10-27 | Arbitrary angle scanning method in scanning control |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2515518B2 (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007334138A (en) * | 2006-06-16 | 2007-12-27 | Ricoh Co Ltd | Process cartridge and image forming apparatus |
JP2009053311A (en) * | 2007-08-24 | 2009-03-12 | Konica Minolta Business Technologies Inc | Process cartridge interval measuring method using optical path altering member and process cartridge measured using measuring method |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59209741A (en) * | 1983-05-16 | 1984-11-28 | Fanuc Ltd | Arbitrary direction copying controlling method |
-
1986
- 1986-10-27 JP JP61255472A patent/JP2515518B2/en not_active Expired - Lifetime
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPS59209741A (en) * | 1983-05-16 | 1984-11-28 | Fanuc Ltd | Arbitrary direction copying controlling method |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2007334138A (en) * | 2006-06-16 | 2007-12-27 | Ricoh Co Ltd | Process cartridge and image forming apparatus |
JP2009053311A (en) * | 2007-08-24 | 2009-03-12 | Konica Minolta Business Technologies Inc | Process cartridge interval measuring method using optical path altering member and process cartridge measured using measuring method |
Also Published As
Publication number | Publication date |
---|---|
JP2515518B2 (en) | 1996-07-10 |
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