JPH0718674B2 - Proximity fuze - Google Patents
Proximity fuzeInfo
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- JPH0718674B2 JPH0718674B2 JP1282025A JP28202589A JPH0718674B2 JP H0718674 B2 JPH0718674 B2 JP H0718674B2 JP 1282025 A JP1282025 A JP 1282025A JP 28202589 A JP28202589 A JP 28202589A JP H0718674 B2 JPH0718674 B2 JP H0718674B2
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Description
【発明の詳細な説明】 〔産業上の利用分野〕 本発明は電波・光波複合形の近接信管装置に関する。DETAILED DESCRIPTION OF THE INVENTION [Industrial field of use] The present invention relates to a radio wave / light wave composite type proximity fuze device.
本発明による近接信管装置は飛翔体に搭載されるもの
で、目標存在方向を検出するための電波及び光波の検出
象限を45゜回転させる手段を有し、侵入して来る目標存
在象限の検出を電波および光波の2方式を用いて象限内
の目標物体の存在方向を限定することを可能ならしめた
ものである。The proximity fuze device according to the present invention is mounted on a flying object, and has means for rotating the detection quadrant of the electric wave and the light wave for detecting the target existence direction by 45 ° to detect the incoming target existence quadrant. It is possible to limit the existence direction of the target object in the quadrant by using two methods of radio waves and light waves.
また本発明装置によれば、電波及び光波の2方式を用い
て目標存在方向の検出を行い、検出分解能を向上させる
と共に、妨害電波、妨害光、反射波等の影響を減少さ
せ、誤動作を軽減させた近接信管装置を得ることができ
る。Further, according to the device of the present invention, the target existence direction is detected by using the two methods of radio wave and light wave, and the detection resolution is improved, and the influences of jamming radio waves, jamming light, reflected waves, etc. are reduced, and malfunctions are reduced. It is possible to obtain the close fuze device.
一般に、この種の飛翔体用アクティブ近接信管は、電波
又は光波の投射ビームに目標物体が通過すると目標物体
からの反射波を受信し、侵入目標物体を検出している。Generally, an active proximity fuze of this type receives a reflected wave from a target object when the target object passes through a projection beam of radio waves or light waves, and detects an intruding target object.
従来、アクティブ光波近接信管に於いては、光学系レン
ズを介してファンビームを形成し、そのファン・ビーム
により4象限、又はそれ以上の象限として全周囲の検知
範囲を構成し、投射ビーム光と同一波長の反射光を受光
器に入力させて所定の強さ以上に検出された場合に、そ
の検出信号を弾頭に点火信号として送出している。Conventionally, in an active light wave proximity fuze, a fan beam is formed through an optical system lens, and the fan beam configures a four-quadrant or four or more quadrants as a detection range of the entire circumference and When the reflected light of the same wavelength is input to the light receiver and detected with a predetermined intensity or more, the detection signal is sent to the warhead as an ignition signal.
この場合、目標検出象限範囲はファンビームを形成する
投射器の特性により決められ、検出象限の隣りの検出象
限との境界近辺に検知範囲の不明確な領域が発生する不
都合がある。In this case, the target detection quadrant range is determined by the characteristics of the projector that forms the fan beam, and there is the inconvenience that an unclear region of the detection range occurs near the boundary between the detection quadrant and the adjacent detection quadrant.
上記ファン・ビーム構成により全周囲方向に投射させる
ために投射器の特性上、象限範囲の境界近辺で切れ込み
が発生し、このため切れ込み部分は検知有効距離が小さ
くなる不都合がある。Due to the characteristics of the projector for projecting in the all-circumferential direction by the above fan beam configuration, a notch occurs near the boundary of the quadrant range, so that the notch portion has a disadvantage that the effective detection distance becomes small.
アクティブ電波近接信管に於いて送受信アンテナ・パタ
ーンは、送信電波の波長と装着する飛翔体の形状(例え
ば、直径等)との関係により、投射ファンビームの形成
が影響されるため送受信合成パターンによる検知ビーム
は隣接する象限検出範囲の不明瞭な部分が大きく発生す
る。又、波長の短いミリ波帯などと用いる場合には、飛
翔体の径に対して非常に短い波長になるため、切れ込み
の大きいファンビームとなり、均一な全周囲の検知有効
距離を得にくい不都合がある。In the active radio wave proximity fuze, the transmission / reception antenna pattern is detected by the transmission / reception combined pattern because the formation of the projection fan beam is affected by the relationship between the wavelength of the transmission radio wave and the shape (eg diameter) of the mounted flying object. The beam has a large unclear portion in the adjacent quadrant detection range. Further, when used in a millimeter wave band having a short wavelength, the wavelength becomes extremely short with respect to the diameter of the flying object, resulting in a fan beam with a large notch, which makes it difficult to obtain a uniform effective detection distance around the entire circumference. is there.
また、上記電波又は光波方式の近接信管は、各々別個に
使用されているために、それぞれの妨害電波、妨害光、
太陽光、反射光等不要な電波、光波により影響されやす
いという不都合がある。Further, since the above-mentioned radio wave or light wave type proximity fuze is used separately, each of the jamming radio wave, jamming light,
There is an inconvenience that it is easily affected by unnecessary electric waves and light waves such as sunlight and reflected light.
本発明の目的は、侵入して来る目標の存在方向を検出す
るための電波及び光波の検出象限を45゜回転させて、侵
入して来る目標の検出が行われ、目標存在象限が判定さ
れ、象限内の目標物体の存在方向を限定して検出分解能
を向上させた電波・光波複合形の近接信管装置を提供す
るものである。The object of the present invention is to rotate the detection quadrant of the radio wave and the light wave for detecting the presence direction of the invading target by 45 °, detect the invading target, and determine the target existence quadrant. An object of the present invention is to provide a radio wave / light wave composite type proximity fuze device in which the detection direction is improved by limiting the direction of existence of a target object in a quadrant.
本発明の他の目的は、電波・光波の2方式を用いて妨害
電波、妨害光、太陽光、反射光等の影響を減少させるこ
との可能な電波・光波複合形の近接信管装置を提供する
ことにある。Another object of the present invention is to provide a radio / light wave composite type proximity fuze device capable of reducing the effects of radio wave / interference light, sunlight, reflected light, etc. by using two methods of radio wave / light wave. Especially.
本発明によれば、4象限対応させて、第1〜第4の電波
によるファン・ビームの目標物体からの反射波を受信す
る電波目標検出部、該第1〜第4の電波によるファン・
ビームの投射配置を所定の回転方向に45゜回転させた配
置において、光波ビームを投射し、目標物体からの反射
光波ビームを受信する光波目標検出部、上記電波目標検
出部の出力信号をそれぞれ隣り合った象限の出力信号と
の比較を行う電波信号比較部、上記光波目標検出部の出
力信号をそれぞれ隣り合った象限の出力信号との比較を
行う光波信号比較部、上記電波信号比較部の出力信号お
よび上記電波目標検出部からのラッチ信号を受け電波に
よる目標存在象限の判定を行う電波存在象限判定部、上
記光波信号比較部の出力信号および上記光波目標検出部
からのラッチ信号を受け、光波による目標存在象限の判
定を行う光波存在象限判定部、および上記電波存在象限
判定部および該光波存在象限判定部の出力信号を受け、
該出力信号の合成を行うことにより目標物体の存在方向
の判定を行う象限信号発出部、を具備することを特徴と
する電波・光波複合形の近接信管装置が提供される。According to the present invention, a radio wave target detection unit that receives reflected waves from a target object of a fan beam by the first to fourth radio waves corresponding to four quadrants, a fan by the first to fourth radio waves,
In the arrangement in which the beam projection arrangement is rotated by 45 ° in a predetermined rotation direction, the lightwave target detection unit that projects the lightwave beam and receives the reflected lightwave beam from the target object, and the output signals of the radiowave target detection unit are adjacent to each other. Output of the radio wave signal comparison unit that compares the output signal of the matched quadrant, the output signal of the light wave target detection unit with the output signal of the adjacent quadrant, and the output of the radio wave signal comparison unit A signal and a latch signal from the radio wave target detection unit are used to determine a target existence quadrant by radio waves. A radio wave existence quadrant determination unit, an output signal from the light wave signal comparison unit and a latch signal from the light wave target detection unit are received, and a light wave is received. Receiving the output signal of the light wave existence quadrant judgment unit and the light wave existence quadrant judgment unit, which determines the target existence quadrant by
There is provided a radio wave / light wave composite type near fuze device characterized by comprising a quadrant signal emitting section for judging the existence direction of a target object by synthesizing the output signals.
本発明の一実施例としての近接信管装置が第1図に示さ
れる。A proximity fuze device as an embodiment of the present invention is shown in FIG.
第1図装置における飛翔体における電波方式送受信アン
テナおよび光波方式投射器、受光器の取付状況が第2〜
4図に示される。Fig. 1 shows the mounting conditions of the radio wave transmitting / receiving antenna, the light wave projector, and the light receiver in the flying object in the device.
It is shown in FIG.
第1図装置はアクティブ方式による電波および光波の目
標検出部(1と2)を有し、飛翔体の機軸を中心に全周
囲方向の4象限内目標存在方向を検知するための装置で
ある。FIG. 1 is a device having target detection units (1 and 2) for radio waves and light waves of an active system, and for detecting a target existence direction within four quadrants in the omnidirectional direction around the axis of a flying object.
電波目標検出部1は夫々一対の送受信アンテナ11〜14、
電波目標検出器10とを含む。送受信アンテナ(11〜14)
は例えば上、下の送信アンテナ(11,12)により送信波
を投射し、目標物体からの反射波を、左、右の受信アン
テナ(13,14)により受信し、電波目標検出器(10)を
介して4象限のファン・ビーム信号として電波信号比較
部(3)に送出する。(本件出願人による特願昭63−15
4967、平1−95353を参照)この場合、4象限のファン
・ビームを構成可能なアンテナであれば、いずれの方式
を用いても差支えない。The radio wave target detection unit 1 includes a pair of transmission / reception antennas 11 to 14,
The radio wave target detector 10 is included. Transmit and receive antennas (11-14)
For example, the transmission waves are projected by the upper and lower transmission antennas (11, 12), the reflected waves from the target object are received by the left and right reception antennas (13, 14), and the radio wave target detector (10) is received. Is transmitted to the radio wave signal comparison unit (3) as a four-quadrant fan beam signal via. (Japanese Patent Application No. 63-15 by the applicant
In this case, any method can be used as long as it is an antenna capable of forming a 4-quadrant fan beam.
光波目標検出器2も同様に夫々一対の投射器(211〜21
4)及び受光器(221〜224)を介して光波信号を目標に
対して送り、その反射光を受光して受光器を経由して検
出器201〜204に信号を送り、その出力SL(1)〜SL
(4)に夫々各象限I〜IVの情報を光波信号比較部4に
送信する。この場合光波目標検出部2は、赤外線または
半導体レーザ発振光源等を用いた4象限の象限検知可能
ないずれの目標検出器201〜204を使用しても差支えな
い。Similarly, the light wave target detectors 2 each have a pair of projectors (211 to 211).
4) and sends a lightwave signal with respect to the target through a light receiver (221 to 224), sends a signal to the detector 201 to 204 via the optical receiver receives the reflected light, the output S L ( 1) ~S L
In (4), the information of each quadrant I to IV is transmitted to the lightwave signal comparison unit 4. In this case, the light wave target detection unit 2 may use any of the target detectors 201 to 204 capable of detecting four quadrants using infrared rays or a semiconductor laser oscillation light source.
近接信管を搭載した飛翔体には電波系アンテナ11〜14と
投射器(211〜214)・受光器(221〜224)が第2図に示
されるように装着されている。第2図の装置が斜視図と
して第3図に示される。第2図の装置における電波方式
アンテナの配置と光波方式の投射器・受光器の配置が第
4図(A)、(B)に示される。As shown in FIG. 2, radio wave antennas 11 to 14, a projector (211 to 214), and a light receiver (221 to 224) are mounted on a flying body equipped with a proximity fuze. The device of FIG. 2 is shown in perspective in FIG. The arrangement of the radio wave type antenna and the arrangement of the light wave type projector / light receiver in the apparatus of FIG. 2 are shown in FIGS. 4 (A) and 4 (B).
電波系は送信アンテナおよび受信アンテナの各ビームの
組合せにより第5図(A)に示される目標検出ビームが
発生させられる。光波系は、投射器・受光器の位置にし
たがって、第5図(B)に示される目標検出ビームが得
られる。このように光波系の4個のビームは電波系の4
個のビームに対して45゜回転している。In the radio wave system, a target detection beam shown in FIG. 5 (A) is generated by combining the beams of the transmitting antenna and the receiving antenna. In the light wave system, the target detection beam shown in FIG. 5 (B) is obtained according to the positions of the projector and the light receiver. In this way, the four beams of the lightwave system are
It is rotated 45 ° with respect to each beam.
第5図に示されるように、電波方式の検知象限に対して
光波方式の検知象限を所定の回転方向に45゜回転させた
状態で侵入して来る目標物体を2方式により検知する。
この所定の回転方向としては、時計方向、反時計方向い
ずれも可能であるが、以下においては、反時計方向を選
んだ場合について説明する。As shown in FIG. 5, a target object coming in is detected by the two methods in a state where the light wave type detection quadrant is rotated by 45 ° in a predetermined rotation direction with respect to the radio wave type detection quadrant.
The predetermined rotation direction can be either clockwise or counterclockwise, but in the following, a case where counterclockwise is selected will be described.
2方式の目標検出器の投射ビームに侵入した目標物体の
反射波は検出信号として各々の目標検出器内のスレッシ
ョルドレベル設定値と比較されて検知ビーム信号(電
波:SEM(1)〜SEM(4)、光波:SL(1)〜S
L(4))を電圧値としてそれぞれの信号比較部に送出
すると、ともに目標を検知した一瞬の検知信号をトリガ
・パルスとして存在象限判定部に送出する。The reflected wave of the target object that has entered the projection beam of the two-type target detector is compared as the detection signal with the threshold level setting value in each target detector, and the detection beam signal (radio waves: S EM (1) to S EM (4), the light wave: S L (1) ~S
When L (4)) is sent as a voltage value to each of the signal comparison units, the detection signal of the moment when the target is detected is sent as a trigger pulse to the existing quadrant determination unit.
電波信号比較部3は、各象限の検知ビーム信号S
EM(1),SEM(2),SEM(3),SEM(4)を用いて、第
6図に示すように通常用いられているコンパレータ回路
により、それぞれ隣り合った象限を対とした信号を例え
ば象限IとIIの場合SEM(1)とSEM(2)の信号を比
較し、その検出象限範囲を明確にして、2値信号により
象限信号(Sa(1)〜Sa(4))を電波存在象限判
定部5に送出する。The radio signal comparison unit 3 detects the detection beam signal S of each quadrant.
Using EM (1), S EM (2), S EM (3) and S EM (4), a pair of adjacent quadrants are paired by a normally used comparator circuit as shown in FIG. For example, in the case of quadrants I and II, the signals of S EM (1) and S EM (2) are compared, the detected quadrant range is clarified, and the quadrant signals (S a (1) to S S a (4)) is sent to the radio wave existence quadrant determination unit 5.
光波信号比較部も上記と同様に、各象限の検知ビーム信
号SL(1),SL(2),SL(3),SL(4)を用い
て、コンパレータ回路により、それぞれの隣り合った象
限を対とした信号を比較し、その検出象限範囲を明確に
して、2値信号により象限信号(Sb(1)〜S
b(4))を光波存在象限判定部に送出する。Similarly to the above, the light wave signal comparison unit also uses the detection beam signals S L (1), S L (2), S L (3), and S L (4) of each quadrant, and uses the detection beam signals S L (1), S L (2), S L (3), and S L (4), The signals in which the matched quadrants are paired are compared to clarify the detection quadrant range, and the quadrant signals (S b (1) to S
b (4)) is sent to the light wave existing quadrant determination unit.
電波及び光波の存在象限判定部5,6は、各々の信号比較
部3,4から入力した2値信号を目標検出部1からのトリ
ガ・パルスをラッチ信号として第7図第1番目に示す例
のように信号保持し、その信号保持状態による目標の存
在象限信号として象限信号発生部7に送出する。The radio wave and light wave existence quadrant determination units 5 and 6 use the binary signal input from the respective signal comparison units 3 and 4 as a trigger pulse from the target detection unit 1 as a latch signal and are shown in the first example in FIG. The signal is held as described above, and the signal is sent to the quadrant signal generator 7 as a target existing quadrant signal according to the signal holding state.
ここで光波方式は、象限検出範囲が45゜回転しずれてい
るために、電波方式の各象限の中央に対して+45゜方向
と−45゜方向に於いて異った象限の検出信号が第7図第
2、第3番目に示すように出力されることになる。In the light wave method, since the quadrant detection range is rotated by 45 ° and shifted, the detection signals of different quadrants in the + 45 ° direction and −45 ° direction with respect to the center of each quadrant of the radio wave method are the first. It is output as shown in FIG. 7 second and third.
象限信号発生部7は、第8図に示すように電波方式及び
光波方式の存在象限判定部5,6に於いて保持された2値
信号を合成し、目標物体の存在象限内の方向を判定す
る。The quadrant signal generation unit 7 synthesizes the binary signals held in the existence quadrant judgment units 5 and 6 of the radio wave system and the light wave system, as shown in FIG. 8, and judges the direction in the existence quadrant of the target object. To do.
例えば、象限I内の第5図矢印に示す方向に目標が侵入
した場合、電波方式のコンパレータ回路IIとIIIは
“0"、コンパレータ回路IとIVは“1"の2値信号が、
又、光波方式のコンパレータ回路は、象限Iの+45゜側
に目標が存在しているために投射ビーム1の検知出力で
コンパレータ回路はIIとIIIが“0"、コンパレータ回路
IとIVが“1"の2値信号となる。For example, when a target enters in the quadrant I in the direction shown by the arrow in FIG. 5, a binary signal of “0” is output to the radio wave type comparator circuits II and III, and a binary signal of “1” is output to the comparator circuits I and IV.
In the lightwave type comparator circuit, since the target exists on the + 45 ° side of the quadrant I, the detection output of the projection beam 1 causes the comparator circuits II and III to be “0”, and the comparator circuits I and IV to be “1”. It becomes a binary signal of ".
上記、2方式の出力信号を合成すると、この状態では第
8図に示すように存在象限Iの+45゜方向内に目標が存
在していることを判定して弾頭にその情報を送出する。When the output signals of the two systems are combined, in this state, as shown in FIG. 8, it is determined that the target exists within the + 45 ° direction of the existence quadrant I, and the information is sent to the warhead.
第1図装置においては、電波及び光波の目標検出器の象
限検出範囲を45゜回転させ、侵入して来る目標物体を2
方式で合成して検出することにより、象限内の目標の方
向を検出させることができ、2方式による検出分解能を
向上させることができる。In the apparatus shown in FIG. 1, the quadrant detection range of the target detector for radio waves and light waves is rotated by 45 °, and the target object coming in
By combining and detecting by the method, the direction of the target in the quadrant can be detected, and the detection resolution by the two methods can be improved.
第1図装置における信号比較部3,4、トリガ・パルス、
存在象限判定部5,6、象限信号発生器7については、本
件出願人による特願昭63−154967号、昭63−176484号の
明細書を参照することができる。Fig. 1 Signal comparison units 3 and 4 in the device, trigger pulse,
Regarding the existing quadrant determining units 5 and 6, and the quadrant signal generator 7, the specification of Japanese Patent Application Nos. 63-154967 and 63-176484 by the applicant of the present application can be referred to.
本発明によれば、目標存在方向を検出するための電波及
び光波の検出象限を45゜回転させて侵入して来る目標の
検出が行われ目標存在象限が判定され、象限内の目標物
体の存在方向を限定することができ、電波光波複合形の
近接信管装置の機能向上が実現する。According to the present invention, the intruding target is detected by rotating the radio wave and light wave detection quadrants for detecting the target existence direction by 45 °, the target existence quadrant is determined, and the existence of the target object in the quadrant is detected. The direction can be limited, and the function improvement of the radio wave combined wave type fuze device is realized.
また本発明によれば、電波、光波の2方式を用いて目標
存在方向の検出が行われ、検出分解能を向上させること
ができる。Further, according to the present invention, the target existing direction is detected using two methods of radio waves and light waves, and the detection resolution can be improved.
また本発明によれば、電波、光波の2方式が用いられ、
妨害電波、妨害光、反射波等の影響を減少させることが
できる。Further, according to the present invention, two methods of radio wave and light wave are used,
It is possible to reduce the influence of jamming radio waves, jamming lights, reflected waves, and the like.
第1図は本発明の一実施例としての近接信管装置の概略
ブロック図、 第2図は飛翔体に装着された電波方式のアンテナと光波
方式の投射器、受光器を説明する図、 第3図は第2図の後方斜視図、 第4図(A)、(B)はそれぞれ第2図の装置における
電波方式アンテナの配置と光波方式の投射器、受光器の
配置の断面図、 第5図(A)、(B)はそれぞれ電波方式(A)および
光波方式(B)における投射ファンビームの各象限にお
けるパターンを示す図、 第6図は第1図の電波信号比較部3における各象限比較
器を含むコンパレータ回路の接続図、 第7図は電波方式および±45゜回転させた場合の光波方
式のラッチ信号対対象存在象限判定信号波形図、 第8図は2方式の各象限対応コンパレータにおける2値
化目標存在象限信号を示す図、 を夫々表わしている。 1……電波目標検出部、2……光波目標検出部、 3……電波信号比較部、4……光波信号比較部、 5……電波存在象限判定部、 6……光波存在象限判定部、 7……象限信号発生部、10……電波目標検出器、 11〜14……送受信アンテナ、 201〜204……光波目標検出器、 211〜214……投射器、221〜224……受光器。FIG. 1 is a schematic block diagram of a proximity fuze device as an embodiment of the present invention, and FIG. 2 is a diagram for explaining a radio wave type antenna, a light wave type projector, and a light receiver mounted on a flying object. FIG. 4 is a rear perspective view of FIG. 2, and FIGS. 4 (A) and 4 (B) are cross-sectional views of the arrangement of the radio wave type antenna and the light wave type projector and the light receiver in the apparatus of FIG. 2, respectively. FIGS. 6A and 6B are diagrams showing a pattern in each quadrant of the projection fan beam in the radio wave system (A) and the light wave system (B), respectively. FIG. 6 is a quadrant in the radio wave signal comparison unit 3 of FIG. 7 is a connection diagram of a comparator circuit including a comparator, FIG. 7 is a waveform diagram of a latch signal of a radio wave method and a light wave method when rotated by ± 45 °, and a target existence quadrant determination signal waveform diagram. FIG. Shows the binary target existence quadrant signal in , Respectively represent. 1 ... Radio wave target detection unit, 2 ... Light wave target detection unit, 3 ... Radio wave signal comparison unit, 4 ... Light wave signal comparison unit, 5 ... Radio wave existence quadrant determination unit, 6 ... Light wave existence quadrant determination unit, 7 ... Quadrant signal generator, 10 ... Radio wave target detector, 11-14 ... Transmitting / receiving antenna, 201-204 ... Lightwave target detector, 211-214 ... Projector, 221-224 ... Photoreceiver.
Claims (1)
よるファン・ビームの目標物体からの反射波を受信する
電波目標検出部、 該第1〜第4の電波によるファン・ビームの投射配置を
所定の回転方向に45゜回転させた配置において、光波ビ
ームを投射し、目標物体からの反射光波ビームを受信す
る光波目標検出部、 上記電波目標検出部の出力信号をそれぞれ隣り合った象
限の出力信号との比較を行う電波信号比較部、 上記光波目標検出部の出力信号をそれぞれ隣り合った象
限の出力信号との比較を行う光波信号比較部、 上記電波信号比較部の出力信号および上記電波目標検出
部からのラッチ信号を受け電波による目標存在象限の判
定を行う電波存在象限判定部、 上記光波信号比較部の出力信号および上記光波目標検出
部からのラッチ信号を受け、光波による目標存在象限の
判定を行う光波存在象限判定部、および 上記電波存在象限判定部および該光波存在象限判定部の
出力信号を受け、該出力信号の合成を行うことにより目
標物体の存在方向の判定を行う象限信号発生部、 を具備することを特徴とする電波・光波複合形の近接信
管装置。1. A radio wave target detecting unit for receiving a reflected wave of a fan beam of first to fourth radio waves from a target object corresponding to four quadrants, and a fan beam of the first to fourth radio waves. In the arrangement in which the projection arrangement of is rotated by 45 ° in the predetermined rotation direction, the light wave target detection unit that projects the light wave beam and receives the reflected light wave beam from the target object, and the output signals of the above-mentioned radio wave target detection units are adjacent to each other. Radio wave signal comparison unit for comparing with the output signal of the quadrant, the light wave signal comparison unit for comparing the output signal of the light wave target detection unit with the output signal of the adjacent quadrant, the output signal of the radio wave signal comparison unit And a radio wave existence quadrant determining unit that receives a latch signal from the radio wave target detecting unit and determines a target existence quadrant by a radio wave, an output signal of the light wave signal comparing unit and a latch signal from the light wave target detecting unit Receiving the output signal of the light wave existence quadrant judging unit and the light wave existence quadrant judging unit and judging the target existence quadrant by the light wave, and by synthesizing the output signals A radio wave / light wave composite type close fuze device, comprising: a quadrant signal generator that determines the direction of existence.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1282025A JPH0718674B2 (en) | 1989-10-31 | 1989-10-31 | Proximity fuze |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP1282025A JPH0718674B2 (en) | 1989-10-31 | 1989-10-31 | Proximity fuze |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH03144300A JPH03144300A (en) | 1991-06-19 |
| JPH0718674B2 true JPH0718674B2 (en) | 1995-03-06 |
Family
ID=17647188
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP1282025A Expired - Fee Related JPH0718674B2 (en) | 1989-10-31 | 1989-10-31 | Proximity fuze |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0718674B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3030952U (en) * | 1996-04-09 | 1996-11-12 | 株式会社白興商会 | Paper hanger with collar holder |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP5044794B2 (en) * | 2009-06-08 | 2012-10-10 | 防衛省技術研究本部長 | Active defense methods against flying objects |
-
1989
- 1989-10-31 JP JP1282025A patent/JPH0718674B2/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP3030952U (en) * | 1996-04-09 | 1996-11-12 | 株式会社白興商会 | Paper hanger with collar holder |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH03144300A (en) | 1991-06-19 |
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