JPH03195900A - Laser apparatus - Google Patents
Laser apparatusInfo
- Publication number
- JPH03195900A JPH03195900A JP1337467A JP33746789A JPH03195900A JP H03195900 A JPH03195900 A JP H03195900A JP 1337467 A JP1337467 A JP 1337467A JP 33746789 A JP33746789 A JP 33746789A JP H03195900 A JPH03195900 A JP H03195900A
- Authority
- JP
- Japan
- Prior art keywords
- distance
- target
- projectile
- laser
- laser beam
- 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
- 230000001678 irradiating effect Effects 0.000 claims 1
- 230000010354 integration Effects 0.000 abstract 1
- 238000010586 diagram Methods 0.000 description 3
- 238000001514 detection method Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000007796 conventional method Methods 0.000 description 1
Landscapes
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Optical Radar Systems And Details Thereof (AREA)
Abstract
Description
【発明の詳細な説明】
〔産業上の利用分野〕
本発明はレーザ装置に関し、特に標的からのレーザ反射
光を自ら検知して標的の方向に飛翔体を誘導するレーザ
装置に関する。DETAILED DESCRIPTION OF THE INVENTION [Field of Industrial Application] The present invention relates to a laser device, and more particularly to a laser device that detects laser reflected light from a target and guides a projectile toward the target.
標的に飛翔体を誘導するレーザ装置はJ:<知られてい
る。Laser devices for guiding projectiles to targets are known.
この種のレーザ装置は、第2図に示す如く、標的2の形
状よりも狭いレーザビーム11をレーザ装置1から標的
2に照射する。飛翔体3の頭部に搭載されたレーザシー
カ(laser 5eeker)31は、標的2からの
レーザ反射光21を検知してその角度情報を出力する。This type of laser device irradiates a target 2 with a laser beam 11 narrower than the shape of the target 2 from the laser device 1, as shown in FIG. A laser seeker 31 mounted on the head of the flying object 3 detects the laser reflected light 21 from the target 2 and outputs its angle information.
サーボ装置32は、レーザシーカ31の角度情報をもと
に飛翔体を標的に命中するよう操舵する。The servo device 32 steers the flying object to hit the target based on the angle information of the laser seeker 31.
上述した従来のレーザ装置は、飛翔体誘導に常時レーザ
ビームを標的2に照射するため、敵から発見される確率
が高いという欠点がある。またレーザ照射を手動で行な
おうとする場合、照射手はレーザ照射開始のタイミング
がつかめず、照射開始が遅れてしまい飛翔体を標的に命
中できない場合も生じるという欠点がある。The above-mentioned conventional laser device constantly irradiates the target 2 with a laser beam to guide the flying object, so it has a drawback that it has a high probability of being discovered by an enemy. Furthermore, when laser irradiation is attempted to be performed manually, the irradiator cannot grasp the timing to start laser irradiation, resulting in a delay in the start of irradiation and the disadvantage that the projectile may not be able to hit the target.
本発明のレーザ装置は、レーザビームを照射して標的か
らの反射光を受け飛翔体を目標に追尾させるレーザ装置
において、レーザビームを発生するパルスレーザ発生器
と、前記レーザビームによる標的の反射光を受光する受
光器と、前記レーザビーム照射後標的からの反射光を受
光するまでの時間を計数することにより標的までの距離
RLを求める計数回路と、飛翔体の既知の速度■。と器
体発射後の時間tとの積■otを前記距1iRLから減
算して得られる信号(RL−Vot〉が所定の値になっ
たときに前記パルスレーザ発生器に前記レーザビームの
照射を開始させる制御回路と、クロック発生回路とを備
えて構成される。The laser device of the present invention is a laser device that irradiates a laser beam, receives reflected light from a target, and tracks a flying object to a target, and includes a pulsed laser generator that generates a laser beam, and a laser beam that is reflected from a target by the laser beam. a counting circuit that calculates the distance RL to the target by counting the time from irradiation of the laser beam until receiving the reflected light from the target; and a known speed of the flying object. When the signal (RL-Vot) obtained by subtracting the product of the time t and the time t after launching the vehicle from the distance 1iRL reaches a predetermined value, the pulse laser generator is irradiated with the laser beam. It is configured to include a control circuit for starting and a clock generation circuit.
次に本発明について図面を参照して説明する。 Next, the present invention will be explained with reference to the drawings.
第1図は本発明によるレーザ装置の一実施例の構成図で
ある。第1図に示す実施例は、パルスレーザ発生器12
と、標的2からのレーザ反射光を検知するための受光器
13と、標的2までの距離を計数する計数回路14と、
計数回路14による検知距離の情報と飛翔体発射のタイ
ミング情報をもとに飛翔体3から標的2までの距離を求
め、この距離が所定値に達したときにパルスレーザ発生
器12を駆動する制御信号を発生する制御回路15とク
ロック発生回路16とを備えて成る。FIG. 1 is a block diagram of an embodiment of a laser device according to the present invention. The embodiment shown in FIG.
, a light receiver 13 for detecting laser reflected light from the target 2, and a counting circuit 14 for counting the distance to the target 2.
Control that calculates the distance from the flying object 3 to the target 2 based on the information on the detection distance by the counting circuit 14 and the timing information of the projectile launch, and drives the pulse laser generator 12 when this distance reaches a predetermined value. It comprises a control circuit 15 that generates a signal and a clock generation circuit 16.
パルスレーザ発生器12から発生したレーザビーム11
による標的からのレーザ反射光21は、受光器13によ
り検知される。Laser beam 11 generated from pulsed laser generator 12
The laser reflected light 21 from the target is detected by the light receiver 13.
パルスレーザ発生器12から得られるレーザビームのト
リガパルスと、受光器13から得られる検知パルスとは
、距離に比例した時間差を有するので、レーザビームの
トリガパルスをスタートパルスとして受光器13で得ら
れるレーザ反射光パルスをストップパルスとしてクロッ
ク発生回路15で発生するクロックパルスの数を計数回
路14で計数することにより距lll1RLが求められ
る3以上の距離計数は飛翔体発射前に単一パルスレーザ
で行う。Since the trigger pulse of the laser beam obtained from the pulse laser generator 12 and the detection pulse obtained from the photoreceiver 13 have a time difference proportional to the distance, the trigger pulse of the laser beam is used as a start pulse to be obtained by the photoreceiver 13. The distance lll1RL is determined by counting the number of clock pulses generated by the clock generation circuit 15 using the counting circuit 14 using the laser reflected light pulse as a stop pulse. Distance counting of 3 or more is performed using a single pulse laser before launching the projectile. .
次に、上述した距離情報と飛翔体発射のタイミング情報
を制御回路16に供給する。飛翔体の飛翔遠度voは既
知であるので、制御回路〕、6で飛翔体の発射と同時に
■oなる値の積分を開始し秒後の飛翔距離Votを得て
、先に検知した距離RLとの差を計算することにより、
発射から秒後の飛翔体3から標的2までの距離RMを(
RL−VQt)として時間的に連続して得ることができ
る9次にこの距離RMが所定値に達したときパルスレー
ザ発生器12を駆動し、パルスレーザの照射を開始する
。なお本実施例では、パルスレーザの照射を開始する距
離RMの所定値とは飛翔体が標的に命中するのに必要な
最小の誘導時間を確保するための距離を限度として設定
している。Next, the above-mentioned distance information and projectile launch timing information are supplied to the control circuit 16. Since the flight distance vo of the projectile is known, the control circuit starts integrating the value o at the same time as the projectile is launched in step 6, obtains the flight distance Vot seconds later, and calculates the previously detected distance RL. By calculating the difference between
Distance RM from projectile 3 to target 2 seconds after launch (
When this distance RM, which can be obtained continuously in time as RL-VQt), reaches a predetermined value, the pulsed laser generator 12 is driven to start pulsed laser irradiation. In this embodiment, the predetermined value of the distance RM at which pulse laser irradiation is started is set to a distance that ensures the minimum guidance time necessary for the flying object to hit the target.
以上説明したように本発明は、あらかじめレーザ装置か
ら標的までの距離を検知し、飛翔体発射後この距離情報
をもとに飛翔体から標的までの距離を計算し、この距離
が所定値に達したとき飛翔体誘導のためのレーザパルス
の照射を開始することにより、敵に発見される確率を著
しく低減できる効果がある。また、従来よりも照射時間
が短かくてすむため、レーザ装置の電池の消耗が少なく
できる効果もある。As explained above, the present invention detects the distance from the laser device to the target in advance, calculates the distance from the projectile to the target based on this distance information after launching the projectile, and when this distance reaches a predetermined value. By starting the irradiation of laser pulses to guide the projectile at that time, the probability of being discovered by the enemy can be significantly reduced. Furthermore, since the irradiation time is shorter than that of the conventional method, there is also the effect that the battery consumption of the laser device can be reduced.
第1図は本発明のレーザ装置の一実施例を示す構成図、
第2図は本発明のレーザ装置を使用するシステムの説明
図である。
1・・・レーザ装置、2・・・標的、3・・・飛翔体、
12・・・パルスレーザ発生器、13・・・受光器、1
4・・・計数回路、15・・・制御回路、16・・・ク
ロック発生回路、
3
1・・・レーザシーカ、
2・・・サーボ装置。FIG. 1 is a configuration diagram showing an embodiment of the laser device of the present invention,
FIG. 2 is an explanatory diagram of a system using the laser device of the present invention. 1... Laser device, 2... Target, 3... Flying object,
12... Pulse laser generator, 13... Light receiver, 1
4... Counting circuit, 15... Control circuit, 16... Clock generation circuit, 3 1... Laser seeker, 2... Servo device.
Claims (2)
飛翔体を目標に追尾させるレーザ装置において、レーザ
ビームを発生するパルスレーザ発生器と、前記レーザビ
ームによる標的の反射光を受光する受光器と、前記レー
ザビーム照射後標的からの反射光を受光するまでの時間
を計数することにより標的までの距離RLを求める計数
回路と、飛翔体の既知の速度V_oと飛翔体発射後の時
間tとの積V_otを前記距離RLから減算して得られ
る信号(RL−V_ot)が所定の値になったときに前
記パルスレーザ発生器に前記レーザビームの照射を開始
させる制御回路と、クロック発生回路とを備えて成るこ
とを特徴とするレーザ装置。(1) A laser device that irradiates a laser beam, receives reflected light from a target, and tracks a flying object to a target, including a pulsed laser generator that generates a laser beam, and a light receiver that receives the reflected light from the target by the laser beam. a counting circuit that calculates the distance RL to the target by counting the time from irradiation of the laser beam until receiving the reflected light from the target, the known velocity V_o of the projectile, and the time t after the projectile is launched. a control circuit that causes the pulse laser generator to start irradiating the laser beam when a signal (RL-V_ot) obtained by subtracting the product V_ot from the distance RL reaches a predetermined value; and a clock generation circuit. A laser device comprising:
ot)の所定の値を、飛翔体を標的に命中させるに必要
な最小の誘導時間が確保できる距離としたことを特徴と
する請求項(1)記載のレーザ装置。(2) Signal obtained in the control circuit (RL-V_
2. The laser device according to claim 1, wherein the predetermined value of ot) is set to a distance that ensures a minimum guidance time necessary for the projectile to hit the target.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1337467A JP2864599B2 (en) | 1989-12-25 | 1989-12-25 | Laser device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP1337467A JP2864599B2 (en) | 1989-12-25 | 1989-12-25 | Laser device |
Publications (2)
Publication Number | Publication Date |
---|---|
JPH03195900A true JPH03195900A (en) | 1991-08-27 |
JP2864599B2 JP2864599B2 (en) | 1999-03-03 |
Family
ID=18308917
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP1337467A Expired - Lifetime JP2864599B2 (en) | 1989-12-25 | 1989-12-25 | Laser device |
Country Status (1)
Country | Link |
---|---|
JP (1) | JP2864599B2 (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004257724A (en) * | 2003-02-07 | 2004-09-16 | Komatsu Ltd | Bullet guidance device and method |
JP2009162632A (en) * | 2008-01-08 | 2009-07-23 | Ihi Aerospace Co Ltd | Laser semiactive guidance method |
JP2010270947A (en) * | 2009-05-20 | 2010-12-02 | Mitsubishi Electric Corp | Guidance device and target determining device |
JP2010281564A (en) * | 2003-02-07 | 2010-12-16 | Komatsu Ltd | Device and method of guiding ammunition |
JP2013156011A (en) * | 2013-02-28 | 2013-08-15 | Ihi Aerospace Co Ltd | Laser semi-active guidance method |
JP2017101870A (en) * | 2015-12-01 | 2017-06-08 | 株式会社Ihiエアロスペース | Laser semi-active guiding method and device |
-
1989
- 1989-12-25 JP JP1337467A patent/JP2864599B2/en not_active Expired - Lifetime
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP2004257724A (en) * | 2003-02-07 | 2004-09-16 | Komatsu Ltd | Bullet guidance device and method |
JP2010281564A (en) * | 2003-02-07 | 2010-12-16 | Komatsu Ltd | Device and method of guiding ammunition |
JP2009162632A (en) * | 2008-01-08 | 2009-07-23 | Ihi Aerospace Co Ltd | Laser semiactive guidance method |
JP2010270947A (en) * | 2009-05-20 | 2010-12-02 | Mitsubishi Electric Corp | Guidance device and target determining device |
JP2013156011A (en) * | 2013-02-28 | 2013-08-15 | Ihi Aerospace Co Ltd | Laser semi-active guidance method |
JP2017101870A (en) * | 2015-12-01 | 2017-06-08 | 株式会社Ihiエアロスペース | Laser semi-active guiding method and device |
Also Published As
Publication number | Publication date |
---|---|
JP2864599B2 (en) | 1999-03-03 |
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