JPS6315180A - Infrared source detector for flight body - Google Patents

Infrared source detector for flight body

Info

Publication number
JPS6315180A
JPS6315180A JP61158541A JP15854186A JPS6315180A JP S6315180 A JPS6315180 A JP S6315180A JP 61158541 A JP61158541 A JP 61158541A JP 15854186 A JP15854186 A JP 15854186A JP S6315180 A JPS6315180 A JP S6315180A
Authority
JP
Japan
Prior art keywords
target
image
target object
infrared rays
infrared
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.)
Pending
Application number
JP61158541A
Other languages
Japanese (ja)
Inventor
Takeshi Kuroda
健 黒田
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 JP61158541A priority Critical patent/JPS6315180A/en
Publication of JPS6315180A publication Critical patent/JPS6315180A/en
Pending legal-status Critical Current

Links

Landscapes

  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Image Analysis (AREA)

Abstract

PURPOSE:To obtain the motion information of a target, by adding a second operation apparatus for calculating the time required before a flight body and the target are associated from the image signal of the target. CONSTITUTION:Infrared rays emitted from a target transmit through a dome 1 and formed into an image on a CCD image sensor 3 by a lens group 2. The infrared image of the target is converted to a detection signal and this signal is processed by a first operation apparatus 4 to obtain information relating to a visual angle. Further, the detection is applied to a second operation apparatus 5 and the time required before a flight body and the target are associated using the size of the target obtained from both image signals and the change ratio thereof. Therefore, an induction rule having a high hit ratio can be used without requiring a separate apparatus for obtaining information relating to a distance by an electromagnetic wave other than infrared rays.

Description

【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、目標体の発する赤外線を検知することによ
り、目標体の運動情報を得る、飛翔体用の目標体検出装
置に関するものである。
DETAILED DESCRIPTION OF THE INVENTION [Industrial Application Field] The present invention relates to a target object detection device for a flying object, which obtains movement information of a target object by detecting infrared rays emitted by the target object.

〔従来の技術〕[Conventional technology]

第2図は従来の飛翔体用赤外線源検出装置を示すブロッ
ク図であり、図において、1はドーム、2は目標体から
の赤外線を電荷結合デバイス(9CD)に結像させるレ
ンズ群、3はCODイメージセンサ、4は検出信号を処
理する演算装置である。
FIG. 2 is a block diagram showing a conventional infrared source detection device for flying objects. In the figure, 1 is a dome, 2 is a lens group that focuses infrared rays from a target object onto a charge-coupled device (9CD), and 3 is a block diagram showing a conventional infrared source detection device for a flying object. The COD image sensor 4 is an arithmetic unit that processes a detection signal.

次に動作について説明する。目標体の発した赤外線は、
ドーム1を透過し、レンズ群2によってCCDイメージ
センサ3に結像される。CCDに結像した目標体からの
赤外線像は検出信号に変換され、この検出信号は演算装
置4によって処理され、飛翔体に固定された座標軸と飛
翔体と目標体とを結ぶ線分のなす角(目視線角)に関す
る情報が算出される。
Next, the operation will be explained. The infrared rays emitted by the target object are
The light passes through the dome 1 and is imaged on the CCD image sensor 3 by the lens group 2. The infrared image from the target object focused on the CCD is converted into a detection signal, and this detection signal is processed by the arithmetic unit 4 to determine the angle formed by the coordinate axis fixed to the flying object and the line segment connecting the flying object and the target object. Information regarding (eye angle) is calculated.

〔発明が解決しようとする問題点〕[Problem that the invention seeks to solve]

従来の飛翔体用赤外′!FA源検出装置は以上のように
構成されているので、飛翔体の誘導には目視線角に関す
る情報した用いることができず、命中精度の低い誘導則
した用いることができなかった。
Conventional infrared for flying objects! Since the FA source detection device is configured as described above, information regarding the eye angle cannot be used to guide the flying object, and a guidance rule with low accuracy cannot be used.

また、目標体との会合迄の時間、所謂timeto  
goを用いる命中精度の高いm1則を用いようとすると
、赤外線以外の電磁波を用いて目標との距離、又は接近
速度を検出するドソプラーレーf’等別の検出装置を必
要とするなどの問題点があった。
In addition, the time until the meeting with the target body, so-called timeto
If you try to use the m1 law with high accuracy using go, there are problems such as the need for a separate detection device such as a dosoplar array f' that uses electromagnetic waves other than infrared rays to detect the distance to the target or the approaching speed. there were.

この発明は上記のような問題点を解消するためになされ
たもので、赤外線以外の電磁波を用いることなく目視線
角に関する情報とともに、飛翔体と目標体との会合迄の
時間をも得られる飛翔体用赤外線源検出装置を得ること
を目的とする。
This invention was made in order to solve the above-mentioned problems, and it is a flying object that can obtain information about the viewing angle as well as the time until the meeting of the flying object and the target object without using electromagnetic waves other than infrared rays. The purpose of this invention is to obtain an infrared source detection device for the body.

〔問題点を解決するための手段〕[Means for solving problems]

この発明に係る飛翔体用赤外線源検出装置は、目標体検
出装置で得られた検出信号(画像信号)の中の、目標体
の大きさ及びその変化率を用いることによって、飛翔体
と目標体の会合迄の時間を算出する第2の演算装置を付
加したものである。
The infrared source detection device for a flying object according to the present invention uses the size of the target object and its rate of change in the detection signal (image signal) obtained by the target object detection device to detect the distance between the flying object and the target object. A second arithmetic unit is added to calculate the time until the meeting.

〔作用〕 この発明においては、付加された第2の演算装置が、C
CDイメージセンサによって得られた目標体の画像信号
から目標体の大きさおよびその変化率を算出し、飛翔体
と目標との会合迄の時間を算出するから、赤外線以外の
電磁波により目標体との距離、又は接近速度を検出する
別の装置を要することなく命中精度の高いMm則を用い
ることができる。
[Operation] In this invention, the added second arithmetic unit is C
The size of the target object and its rate of change are calculated from the image signal of the target object obtained by the CD image sensor, and the time until the flying object meets the target is calculated. The Mm law with high accuracy can be used without requiring a separate device to detect distance or approach speed.

〔実施例〕〔Example〕

以下、この発明の一実施例を図について説明する。第1
図は本発明の一実施例による飛翔体用赤外線源検出装置
を示し、図において、lはドーム、2は目標体からの赤
外線をCCDに結像させるレンズ群、3はCCDイメー
ジセンサ、4は検出信号を処理する第1の演算装置、5
は新たに付加された第2の演算装置である。
An embodiment of the present invention will be described below with reference to the drawings. 1st
The figure shows an infrared source detection device for a flying object according to an embodiment of the present invention. In the figure, l is a dome, 2 is a lens group that images infrared rays from a target object on a CCD, 3 is a CCD image sensor, and 4 is a a first arithmetic device that processes the detection signal; 5;
is a newly added second arithmetic unit.

次に動作について説明する。Next, the operation will be explained.

目標体の発した赤外線はドーム1を透過し、レンズ群2
によってCCDイメージセンサ3に結像される。COD
に結像した目標体の赤外線像は検出信号に変換され、第
1の演算装置4によって目視線角に関する情報へと処理
される。また、検出48号は第2の演算装置5によって
、画像信壮から得られた目標体の大きさく長さ)及びそ
の変化率を用いて飛翔体と目標体との会合迄の時間が算
出される。第3図に示した目標体の長さl、飛翔体と目
標体との距離R、レンズ群とCCDイメージセンサの距
離f、CCDに結像した目標体の長さdの間には角度θ
を介して以下の関係が成立する。
The infrared rays emitted by the target object pass through the dome 1, and are transmitted through the lens group 2.
An image is formed on the CCD image sensor 3 by. COD
The infrared image of the target object focused on is converted into a detection signal and processed by the first arithmetic unit 4 into information regarding the eye angle. In addition, in detection No. 48, the second arithmetic unit 5 calculates the time until the flying object meets the target object using the size and length of the target object obtained from the image belief and the rate of change thereof. Ru. There is an angle θ between the length l of the target object shown in Fig. 3, the distance R between the flying object and the target object, the distance f between the lens group and the CCD image sensor, and the length d of the target object imaged on the CCD.
The following relationship is established through .

但し、lの時間変化は無視し、角度θは微小と仮定した
。また(6)は時間微分を表す。
However, the time change of l was ignored, and the angle θ was assumed to be small. Also, (6) represents time differentiation.

以上のように第1.第2の演算装置4.5によって目視
線角(方位)及び会合迄の時間(距離)に関する情報が
得られるから、赤外線以外の電磁波によって距離に関す
る情報を得る別の装置を要することなく命中精度の高い
誘導側を用いることができる効果がある。
As mentioned above, the first. Since the second arithmetic unit 4.5 can obtain information regarding the line of sight angle (azimuth) and the time until meeting (distance), accuracy can be improved without the need for a separate device that obtains information regarding distance using electromagnetic waves other than infrared rays. This has the effect of being able to use a high induction side.

なお、上記実施例では、第2の演算装置5は検出信号を
入力としていたが、第1の演算装置4の中間データを入
力としても良い。
In the above embodiment, the second arithmetic device 5 receives the detection signal as an input, but it may also receive intermediate data from the first arithmetic device 4 as an input.

また、上記実施例では目標体の像の長さを用いて演算を
行ったが、像の面積を用いて演算しても良い。
Further, in the above embodiment, the calculation was performed using the length of the image of the target object, but the calculation may be performed using the area of the image.

〔発明の効果〕〔Effect of the invention〕

以上のように、この発明に係る飛翔体用赤外線源検出装
置によれば、目標体の画像信号から、飛翔体と目標体と
の会合迄の時間を算出する第2の演算装置を付加したの
で、従来の目視線角に関する情報とともに利用すること
により、命中精度の高い誘導側を用いることができる効
果がある。
As described above, according to the infrared source detection device for a flying object according to the present invention, the second arithmetic unit that calculates the time until the meeting of the flying object and the target object from the image signal of the target object is added. By using this information together with the conventional information regarding the eye sight angle, it is possible to use the guidance side with high accuracy.

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

第1図はこの発明の一実施例による飛翔体用赤外線源検
出装置を示すブロック図、第2図は従来例を示すブロッ
ク図、第3図は目視線角と飛翔体との位置関係を示す図
である。 図において、1はドーム、2はレンズ群、3はCCDイ
メージセンサ、4は第1の演算装置、5は第2の演算装
置である。
Fig. 1 is a block diagram showing an infrared source detection device for a flying object according to an embodiment of the present invention, Fig. 2 is a block diagram showing a conventional example, and Fig. 3 shows the positional relationship between the viewing angle and the flying object. It is a diagram. In the figure, 1 is a dome, 2 is a lens group, 3 is a CCD image sensor, 4 is a first computing device, and 5 is a second computing device.

Claims (1)

【特許請求の範囲】[Claims] (1)目標体の発する赤外線を電荷結合デバイスを用い
て検知する目標体検出装置と、 上記目標体検出装置によって得られる検出画像を受け、
該検出画像から飛翔体と目標体とがなす目視線角に関す
る情報を得る第1の演算装置と、同じく上記検出画像を
受け、該検出画像の変化から現時点から飛翔体と目標体
が会合する迄の時間を算出する第2の演算装置とを有し
、上記目標体までの距離及び角度を検出する演算装置と
を備えたことを特徴とする飛翔体用赤外線源検出装置。
(1) a target detection device that detects infrared rays emitted by the target using a charge-coupled device; and receiving a detection image obtained by the target detection device;
a first arithmetic unit that obtains information regarding the line of sight angle between the flying object and the target object from the detected image; an infrared source detection device for a flying object, comprising: a second arithmetic device that calculates the time of the second arithmetic operation; and a arithmetic device that detects the distance and angle to the target object.
JP61158541A 1986-07-04 1986-07-04 Infrared source detector for flight body Pending JPS6315180A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP61158541A JPS6315180A (en) 1986-07-04 1986-07-04 Infrared source detector for flight body

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP61158541A JPS6315180A (en) 1986-07-04 1986-07-04 Infrared source detector for flight body

Publications (1)

Publication Number Publication Date
JPS6315180A true JPS6315180A (en) 1988-01-22

Family

ID=15673962

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61158541A Pending JPS6315180A (en) 1986-07-04 1986-07-04 Infrared source detector for flight body

Country Status (1)

Country Link
JP (1) JPS6315180A (en)

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