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JPS5933234B2 - Digital image tracking device - Google Patents
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JPS5933234B2 - Digital image tracking device - Google Patents

Digital image tracking device

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Publication number
JPS5933234B2
JPS5933234B2 JP53070559A JP7055978A JPS5933234B2 JP S5933234 B2 JPS5933234 B2 JP S5933234B2 JP 53070559 A JP53070559 A JP 53070559A JP 7055978 A JP7055978 A JP 7055978A JP S5933234 B2 JPS5933234 B2 JP S5933234B2
Authority
JP
Japan
Prior art keywords
tables
formulas
image
chemical formulas
coordinate
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.)
Expired
Application number
JP53070559A
Other languages
Japanese (ja)
Other versions
JPS54161819A (en
Inventor
久美雄 笠原
尚 伊東
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Mitsubishi Electric Corp
Original Assignee
Mitsubishi Electric Corp
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Mitsubishi Electric Corp filed Critical Mitsubishi Electric Corp
Priority to JP53070559A priority Critical patent/JPS5933234B2/en
Publication of JPS54161819A publication Critical patent/JPS54161819A/en
Publication of JPS5933234B2 publication Critical patent/JPS5933234B2/en
Expired legal-status Critical Current

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  • Closed-Circuit Television Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)

Description

【発明の詳細な説明】 この発明は、目標物のディジタル画像を用いて重心を追
尾するデイジタル画像追尾装置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION The present invention relates to a digital image tracking device that tracks the center of gravity of a target using a digital image.

通常、撮像装置を用いて撮像した画像をA/D変換し、
そのデイジタル画像内にある目標物の像、以下目標像と
略す、の重心を計算しての目標物を自動的に追尾するデ
イジタル画像追尾装置では、実時間性が最も重要視され
る。
Usually, an image captured using an imaging device is A/D converted,
In a digital image tracking device that automatically tracks a target by calculating the center of gravity of an image of the target in the digital image (hereinafter abbreviated as target image), real-time performance is most important.

この要求を満足するように画像データを高速処理するた
めには大型コンピユータと大容量メモリとが心要である
。ところで、この種のデイジタル画像追尾装置をミサイ
ルの誘導装置として搭載しようとすると、寸法、重量お
よび電源容量の点で制約があり当然大型コンピユータを
搭載することはできない。そのため、従来は小型のバイ
ポーラ型マイクロコンピユータを専用コンピユータとし
て開発し実時間処理させていたがその処理時間の制約か
ら最大100画素×100画素程度の画像しか処理でき
なかつた。また、専用マイクロコンピユータといえども
大きさにして300×200×100mm程度、重量に
して5kg程度であり小型のミサイルには搭載できない
欠点があつた。この発明は、これらの欠点を除去するた
め、目標像のX軸およびY軸方向の重み係数乗算演算部
、面積演算部および重心座標演算部を並列デイジタル・
コンパレータ、並列加算回路およびカウンタ回路で構成
し、画像データの処理時間の高速化と装置の小形・軽量
化、低消費電力化を図つたものである。
In order to process image data at high speed to meet this requirement, a large computer and a large capacity memory are essential. By the way, if this type of digital image tracking device is to be installed as a missile guidance device, there are restrictions in terms of size, weight, and power supply capacity, and naturally a large computer cannot be installed. Therefore, in the past, a small bipolar microcomputer was developed as a dedicated computer and processed in real time, but due to processing time constraints, it could only process images of about 100 pixels x 100 pixels at most. Furthermore, even though it was a dedicated microcomputer, it had the disadvantage of being about 300 x 200 x 100 mm in size and about 5 kg in weight, making it impossible to mount it on a small missile. In order to eliminate these drawbacks, the present invention constructs a weighting factor multiplication calculation unit in the X-axis and Y-axis directions of the target image, an area calculation unit, and a barycenter coordinate calculation unit in parallel digitally.
It consists of a comparator, a parallel adder circuit, and a counter circuit, and aims to speed up image data processing time, make the device smaller and lighter, and reduce power consumption.

以下図面に従つて詳細に説明する。ここではA/D変換
として、1ビツト処理すなわち2値化の場合を例にとり
説明する。第1図に、この発明における重心座標演算動
作,を説明するための2値化画像を模式的に示す。
A detailed explanation will be given below with reference to the drawings. Here, the case of 1-bit processing, that is, binarization, will be explained as an example of A/D conversion. FIG. 1 schematically shows a binarized image for explaining the barycenter coordinate calculation operation in this invention.

第1図において、2値化画像1内の目標像2の重心座標
XO,YOは、座標i司画素の出力をPij,,l″ま
たは,0″、と表わすと第(1)式で与えられる。第(
1)式中で、分子は目標像2のX軸およびY軸軸方向の
重み係数乗算演算部出力であり、分母は面積演算部出力
である。
In FIG. 1, the barycentric coordinates XO, YO of the target image 2 in the binarized image 1 are given by equation (1), where the output of the pixel with coordinates i is expressed as Pij,,l''or,0''. It will be done. No. (
In formula 1), the numerator is the output of the weighting coefficient multiplication unit in the X-axis and Y-axis directions of the target image 2, and the denominator is the output of the area calculation unit.

第2図は、第(1)式中の重み係数乗算演算および千→
Jrijと面積演算’並びに重心座標演算 および を実現するための回路の一実施例の構 成図である。
Figure 2 shows the weighting coefficient multiplication operation in equation (1) and
FIG. 2 is a configuration diagram of an embodiment of a circuit for realizing Jrij, area calculation', and barycenter coordinate calculation.

第2図において、X軸およびY軸座標信号発生回路3a
および3bを用いて第1図に示した2値化画像1の走査
時間に同期させて座標信号を発生させる。
In FIG. 2, the X-axis and Y-axis coordinate signal generation circuit 3a
and 3b to generate coordinate signals in synchronization with the scanning time of the binarized image 1 shown in FIG.

各座標信号は2値化画像信号4に応じてゲート回路5a
および5bを通り、並列加算回路6aおよび6bに入力
され、X軸方向およびY軸方向の重み係数乗算演算部出
力2’→゛IPijおよびが得られる。一方、2値化画
像信号4をカウンタ回路Tへ入力し、目標像の大きさに
対応する画素数を計数することにより目標像の面積演算
部出力→→“Pijが得られる。
Each coordinate signal is sent to the gate circuit 5a according to the binarized image signal 4.
and 5b, and is input to parallel adder circuits 6a and 6b, and weighting coefficient multiplication calculation unit outputs 2'→'IPij and in the X-axis direction and Y-axis direction are obtained. On the other hand, by inputting the binarized image signal 4 to the counter circuit T and counting the number of pixels corresponding to the size of the target image, the area calculation unit output of the target image →→“Pij” is obtained.

上記の゛および→ヰPijの演算が終つてからこ』 l の面積演算部出力→’2’PIJを並列加算回路8へ入
Jl力LjJn算命令によりクロツク発生回路9からの
クロロツク信号により→“→“Pijの整数倍の値を順
々にJl発生させ並列デイジタル・コンパレータ10a
および10bに入力する。
After the above calculations of ゛ and →ヰPij are completed, the output of the area calculation section of l → '2' PIJ is input to the parallel adder circuit 8, and the clock signal from the clock generation circuit 9 is input by the Jl input LjJn calculation command →" →“The parallel digital comparator 10a generates Jl values that are integral multiples of Pij in sequence.
and 10b.

この並列デイジタル・コンパレータ10aおよび10b
を用いて、上記のの整数倍値、およびと””RiJの整
数倍値とをそれぞれ同 』 l じ桁のビツト同志を並列的に比較し、X軸およびY軸ご
とに両者が等しいかまたは→゛→”ゞIjの整数倍値が
大きくなつた場合にストツプパルス信号を発生させ、加
算命令クロツク信号をカウンタ回路11aおよび11b
で計数するのを停止させると、その時点までの計数値が
目標像2の重心座標Xc,Ycを与える。
The parallel digital comparators 10a and 10b
Using , compare the integer multiples of the above and the integer multiples of RiJ in parallel, and check whether they are equal or not for each X-axis and Y-axis. →゛→”ゞWhen the integer multiple of Ij becomes large, a stop pulse signal is generated, and the addition instruction clock signal is sent to the counter circuits 11a and 11b.
When counting is stopped at , the counted values up to that point give the center of gravity coordinates Xc, Yc of the target image 2.

第3図は上記の重心座標演算動作を説明するためのタイ
ムチヤートである。
FIG. 3 is a time chart for explaining the above barycentric coordinate calculation operation.

第3図において重み係数乗算演算および面積演算が完了
すると同時に加算命令クロツク信号(第3図a)が発生
する。この加算命令クロツク信号(第3図a)をX軸お
よびY軸方向のストツプパルス信号(第3図b)および
(第3図c)の発生時まで計数すると計数信号Nx(第
3図d)およびN,(第3図e)が得られる。このよう
にして得られたNx,n,の値は、第1図に示したよう
に座標原点を設定したときの重心座標Xc,Ycに等し
くなる。以上述べた重み係数乗算演算部、面積演算部お
よび重心座標演算部を総称して重心追尾演算部と呼ぶこ
とにすると、この重心追尾演算部の演算時間を制限する
のは並列デジタル・コンパレータの比較処理時間のみで
あり、バイポーラ・デイジタルICを用いれば、1回当
りの比較処理時間Tcは数+Nsであり、また上記の如
く並列ビツト比較方式を採用しているので、全体の演算
時間は最大NxXTcnsまたはNyXTcnsとなる
0一例としてデイジタルコンパレータとしてテキサス・
インステルメント社製のSN74LS85を用いる場合
Tcは36nsであり、またNx及びN,の最大値を2
56に設定した場合、処理時間は最大でTcXnx(又
はNy)=36ns×256=9216nsでありこの
値はTV走査方式の撮像装置の1フレーム時間33ms
の約0.03%に相当する。
In FIG. 3, the addition command clock signal (FIG. 3a) is generated at the same time as the weighting factor multiplication operation and the area operation are completed. When this addition command clock signal (Figure 3a) is counted until the generation of the stop pulse signals (Figure 3b) and (Figure 3c) in the X- and Y-axis directions, the count signal Nx (Figure 3d) and N, (Fig. 3e) is obtained. The values of Nx, n, obtained in this way are equal to the center of gravity coordinates Xc, Yc when the coordinate origin is set as shown in FIG. The weighting factor multiplication calculation unit, area calculation unit, and center of gravity coordinate calculation unit described above are collectively referred to as the center of gravity tracking calculation unit.The computation time of this center of gravity tracking calculation unit is limited by the comparison of parallel digital comparators. If a bipolar digital IC is used, the processing time Tc per comparison is several + Ns, and since the parallel bit comparison method is adopted as described above, the total calculation time is at most NxXTcns. Or NyXTcns 0 As an example, Texas
When using SN74LS85 manufactured by Instrument Co., Ltd., Tc is 36 ns, and the maximum value of Nx and N, is 2
When set to 56, the maximum processing time is TcXnx (or Ny) = 36ns x 256 = 9216ns, and this value is 33ms for one frame of a TV scanning type imaging device.
This corresponds to approximately 0.03% of

これに対し、従来のマイクロコンピユータを用いて、上
記処理を実現しようとすると33ms程度を必要として
おり、この発明による重心座標演算部を用いることによ
り、従来の比較して約3580倍の高速処理ができる。
さらに上記の重心追尾演算部は通常のバイポーラ・デイ
ジタルICを基本として構成でき、その部品数も少くて
済むので小形・軽量化並びに低消費電力化が図られると
ともに、特殊な部品が必要でないためハイブリツドIC
化が容易にできる。以上では、ミサイル誘導装置として
搭載する場合について説明したがこの発明はこれに限ら
ず航空機、船舶、車両等に搭載し野外で使用する追尾装
置に適用できるばかりでなく、トランジスタ、ICなど
の半導体チツプの自動ポンデイング装置の位置合わせ用
検出装置などの計測装置にも応用できる。
On the other hand, when trying to realize the above processing using a conventional microcomputer, it takes about 33ms, but by using the barycentric coordinate calculation section of the present invention, processing speed is about 3580 times faster than that of the conventional one. can.
Furthermore, the center of gravity tracking calculation unit described above can be configured based on a normal bipolar digital IC, and the number of parts required is small, making it compact, lightweight, and low power consumption. IC
can be easily converted into Although the above description has been made regarding the case where the device is installed as a missile guidance device, the present invention is not limited to this, and can be applied not only to tracking devices installed in aircraft, ships, vehicles, etc. and used outdoors, but also to semiconductor chips such as transistors and ICs. It can also be applied to measurement devices such as detection devices for positioning of automatic ponding devices.

以上述べたように、この発明に係るデイジタル画像追尾
装置では、目標物の重心演算をコンピユττ− 1
!』 ττ −Jljータを用いて除算↓÷、
.一及び苦←1.−をする代わりに、並列デイジタル・
コンパレータ等ΣΣX−P・・で構成した専用プロセツ
サを用いて.. 11jJ1とギギPijの整数倍値及
びγギYjPijとΣΣP・・.. 1Jの整数倍値と
をデイジタル的に比較演算するだけで重心座標を演算で
きるので重心演算の高速化が図られ画像データの実時間
処理が容易に行なえるとともに、小形・軽量化並びに低
消費電力化が図られ小型ミサイルへの搭載が容易にでき
る利点がある。
As described above, in the digital image tracking device according to the present invention, the center of gravity of the target is calculated using the computer ττ−1.
! ” Divide using ττ −Jlj data ↓÷,
.. One and bitter←1. – instead of parallel digital
Using a dedicated processor consisting of comparators, etc. ΣΣX-P... .. 11jJ1, integral multiple of gigi Pij, γgi YjPij and ΣΣP... .. The coordinates of the center of gravity can be calculated simply by digitally comparing and calculating the integral multiples of 1J, which speeds up the calculation of the center of gravity and facilitates real-time processing of image data.It is also compact, lightweight, and has low power consumption. It has the advantage that it can be easily mounted on small missiles.

また、回路構成が単純であり部品数も少ないためハイブ
リツドIC化が容易にできる利点もある。
Further, since the circuit configuration is simple and the number of parts is small, it has the advantage that it can be easily converted into a hybrid IC.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図はこの発明における重心座標演算動作を説明する
ための2値化画像を示す図、第2図は重み係数乗算演算
部、面積演算部および重心座標演算部を実現するための
回路の一実施例の構成図、第3図は重心座標演算動作を
説明するためのタイムチヤート図である。 図中1は2値化画像、2は目標像、3aおよび3bはX
軸およびY軸座標信号発生回路、4は2値化画像信号、
5aおよび5bはゲート回路、6aおよび6bは並列加
算回路、7はカウンタ回路、8は並列加算回路、9は加
算命令クロツク発生回路、10aおよび10bは並列デ
ジタル・コンパレータ、11aおよび11bはカウンタ
回路である。
FIG. 1 is a diagram showing a binarized image for explaining the barycenter coordinate calculation operation in this invention, and FIG. 2 is a diagram showing a circuit for realizing the weighting coefficient multiplication calculation section, the area calculation section, and the barycenter coordinate calculation section. FIG. 3, which is a block diagram of the embodiment, is a time chart for explaining the barycentric coordinate calculation operation. In the figure, 1 is a binarized image, 2 is a target image, 3a and 3b are X
Axis and Y-axis coordinate signal generation circuit, 4 is a binary image signal,
5a and 5b are gate circuits, 6a and 6b are parallel adder circuits, 7 is a counter circuit, 8 is a parallel adder circuit, 9 is an addition instruction clock generation circuit, 10a and 10b are parallel digital comparators, and 11a and 11b are counter circuits. be.

Claims (1)

【特許請求の範囲】[Claims] 1 撮像装置よりその視野内にある所要の目標像及びそ
の背景を撮像して得られる画像内で、画像の明るさのち
がいを利用して背景から所要の目標像を分離抽出すると
ともに、上記画像の水平及び垂直方向に設けたX軸−Y
軸直交座標系での目標像の重心座標を演算しその重心座
標と所定の座標との誤差信号を検出し、この誤差信号が
零となるように前記撮像装置の姿勢を制御することによ
り撮像装置の視野内の所定の位置に所要の目標像が静止
するように追尾するディジタル画像追尾装置において、
上記目標像の重心座標演算部を、前記撮像装置により得
られる画像をその最小単位である画素に分割するための
X軸及びY軸方向の座標信号X_i及びY_jを発生さ
せる座標信号発生回路、上記座標信号に基づいてX軸−
Y軸方向に順次走査して各画素の明るさを“1”又は“
0”に2値化した画像P_i_j(“1”の場合P_i
_j=1、“0”の場合P_i_j=0)に変換するA
/D変換回路、X軸及びY軸方向毎に前記座標信号を上
記2値化画像P_i_jが“1”の場合のみ加算して座
標の重み付け演算値▲数式、化学式、表等があります▼
P_i_j及び▲数式、化学式、表等があります▼P_
i_jを求める並列加算回路、上記2値化画像P_i_
jが“1”となる画素の面積演算値▲数式、化学式、表
等があります▼P_i_jを求めるカウンタ回路、重心
座標を計算するためのクロック信号を発生させる加算命
令クロック信号発生回路、上記クロック信号に基づいて
上記の面積演算値▲数式、化学式、表等があります▼P
_i_jの整数倍の値▲数式、化学式、表等があります
▼P_i_j(n=1、2、3・・・)を算出する並列
回加算回路、この面積演算値の整数倍した値▲数式、化
学式、表等があります▼P_i_jと前記座標の重み付
け演算値▲数式、化学式、表等があります▼P_i_j
及び▲数式、化学式、表等があります▼P_i_jと▲
数式、化学式、表等があります▼P_i_jとの大小関
係を比較し、次式を満足するときX軸方向及びY軸方向
毎にストップパルス信号を発生させるディジタル・コン
パレータ、▲数式、化学式、表等があります▼(1)▲
数式、化学式、表等があります▼(2)上記ストップ・
パルス信号が発生されるまでの間X軸方向及びY軸方向
毎に前記加算命令クロック信号発生回路から発生される
クロックパルス信号の個数n_x及びn_yを計数し次
式の重心座標(X_c、Y_c)▲数式、化学式、表等
があります▼(3)▲数式、化学式、表等があります▼
(4)を求めるカウンタ回路とを具備したことを特徴と
するディジタル画像追尾装置。
1. Separate and extract the desired target image from the background by utilizing the difference in brightness of the image within the image obtained by capturing the desired target image and its background within the field of view of the imaging device, and extract the desired target image from the background. X-axis - Y set in the horizontal and vertical directions of
The imaging device calculates the barycentric coordinates of the target image in an axis-orthogonal coordinate system, detects an error signal between the barycentric coordinates and a predetermined coordinate, and controls the attitude of the imaging device so that this error signal becomes zero. In a digital image tracking device that tracks a desired target image so that it remains stationary at a predetermined position within the field of view,
A coordinate signal generation circuit that causes the target image barycentric coordinate calculation unit to generate coordinate signals X_i and Y_j in the X-axis and Y-axis directions for dividing the image obtained by the imaging device into pixels, which are the minimum units thereof; X-axis based on coordinate signal
Scan sequentially in the Y-axis direction and set the brightness of each pixel to "1" or "
Image P_i_j binarized to “0” (in case of “1”, P_i
If _j=1, “0”, convert A to P_i_j=0)
/D conversion circuit, add the above coordinate signals for each X-axis and Y-axis direction only when the above binarized image P_i_j is "1" and calculate the coordinate weighting calculation value ▲ There are mathematical formulas, chemical formulas, tables, etc. ▼
There are P_i_j and ▲mathematical formulas, chemical formulas, tables, etc.▼P_
Parallel addition circuit for calculating i_j, the above binarized image P_i_
The area calculation value of the pixel where j is "1" ▲ There are mathematical formulas, chemical formulas, tables, etc. ▼ Counter circuit to calculate P_i_j, addition instruction clock signal generation circuit to generate the clock signal to calculate the center of gravity coordinates, the above clock signal Based on the above area calculation value ▲ There are mathematical formulas, chemical formulas, tables, etc. ▼ P
A value that is an integer multiple of _i_j ▲ There are mathematical formulas, chemical formulas, tables, etc. ▼ Parallel addition circuit that calculates P_i_j (n = 1, 2, 3...), a value that is an integer multiple of this area calculation value ▲ Mathematical formula, chemical formula , tables, etc. ▼ Weighted calculation value of P_i_j and the above coordinates ▲ Numerical formulas, chemical formulas, tables, etc. ▼ P_i_j
and ▲ There are mathematical formulas, chemical formulas, tables, etc. ▼ P_i_j and ▲
There are mathematical formulas, chemical formulas, tables, etc. ▼Digital comparator that compares the magnitude relationship with P_i_j and generates a stop pulse signal in each X-axis direction and Y-axis direction when the following formula is satisfied, ▲Mathematical formulas, chemical formulas, tables, etc. There is ▼(1)▲
There are mathematical formulas, chemical formulas, tables, etc. ▼ (2) The above stop/
Until the pulse signal is generated, the numbers n_x and n_y of the clock pulse signals generated from the addition instruction clock signal generation circuit are counted in each of the X-axis direction and the Y-axis direction, and the barycenter coordinates (X_c, Y_c) of the following formula are calculated. ▲There are mathematical formulas, chemical formulas, tables, etc.▼(3)▲There are mathematical formulas, chemical formulas, tables, etc.▼
(4) A digital image tracking device characterized by comprising: a counter circuit for determining (4).
JP53070559A 1978-06-12 1978-06-12 Digital image tracking device Expired JPS5933234B2 (en)

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Application Number Priority Date Filing Date Title
JP53070559A JPS5933234B2 (en) 1978-06-12 1978-06-12 Digital image tracking device

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JP53070559A JPS5933234B2 (en) 1978-06-12 1978-06-12 Digital image tracking device

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JPS54161819A JPS54161819A (en) 1979-12-21
JPS5933234B2 true JPS5933234B2 (en) 1984-08-14

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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6150325A (en) * 1984-08-20 1986-03-12 松下電器産業株式会社 electronic components

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5748111A (en) * 1980-09-04 1982-03-19 Toshiba Corp Flying object induction device
JPS5849277U (en) * 1981-09-30 1983-04-02 日本電気株式会社 Target setting device
US4847688A (en) * 1987-04-17 1989-07-11 Matsushita Electric Industrial Co., Ltd. Moving body recognition circuit using luminance signal and moving body tracking apparatus using the moving body recognition circuit

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS6150325A (en) * 1984-08-20 1986-03-12 松下電器産業株式会社 electronic components

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JPS54161819A (en) 1979-12-21

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