JPH0794960B2 - Control device - Google Patents
Control deviceInfo
- Publication number
- JPH0794960B2 JPH0794960B2 JP63319984A JP31998488A JPH0794960B2 JP H0794960 B2 JPH0794960 B2 JP H0794960B2 JP 63319984 A JP63319984 A JP 63319984A JP 31998488 A JP31998488 A JP 31998488A JP H0794960 B2 JPH0794960 B2 JP H0794960B2
- Authority
- JP
- Japan
- Prior art keywords
- signal
- target
- control device
- outputs
- transmission
- 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 - Fee Related
Links
- 230000005540 biological transmission Effects 0.000 claims description 27
- 238000005474 detonation Methods 0.000 claims description 13
- 238000001514 detection method Methods 0.000 claims description 12
- 238000003079 width control Methods 0.000 claims description 8
- 230000007274 generation of a signal involved in cell-cell signaling Effects 0.000 claims description 3
- 230000001678 irradiating effect Effects 0.000 claims description 3
- 230000000977 initiatory effect Effects 0.000 claims description 2
- 238000010586 diagram Methods 0.000 description 3
- 230000001133 acceleration Effects 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000005516 engineering process Methods 0.000 description 1
- 230000002452 interceptive effect Effects 0.000 description 1
- 238000000926 separation method Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Description
【発明の詳細な説明】 〔産業上の利用分野〕 この発明は、目標から生ずる赤外線あるいは反射波を検
出し、目標を捕捉、追尾する制御装置に関するもので、
特に目標に送信波を照射し、目標からの反射波を検知
し、目標が制御装置の近傍を通過又は、目標に直撃した
時起爆し、目標に対し大きな損害を与える制御装置の目
標撃墜性能を向上させようとするものである。DETAILED DESCRIPTION OF THE INVENTION [Industrial application] The present invention relates to a control device for detecting an infrared ray or a reflected wave generated from a target, and capturing and tracking the target.
In particular, irradiate the target with the transmitted wave, detect the reflected wave from the target, detonate when the target passes near the control device or directly hits the target, and the target shooting performance of the control device which causes great damage to the target It is an attempt to improve.
まず、従来のこの種制御装置について簡単に説明する。 First, a conventional control device of this type will be briefly described.
第２図において、Ｍは制御装置、（１）は制御装置Ｍが
捕捉・追尾する目標、（２）は目標（１）に照射する送
信波、（３）は目標（１）からの反射波、（４）は目標
（１）に照射する送信波（２）の送信信号を、信号処理
部（９）の出力の送信指令信号により発生する送信源
部、（５）は送信波（２）の送信方向を制御する移相器
（６）に送信信号を供給し、受信機部（８）に供給せ
ず、また、アンテナ（７）で受信した受信信号は受信機
部（８）に供給し、送信源部（４）には供給しないサー
キユレータ、（６）は、送信波（２）の送信方向で受信
波（３）の受信方向であるビーム指向方向をビーム制御
部（10）の出力のビーム制御信号により制御する移相
器、（７）は送信波（２）を目標（１）に照射し、目標
（１）からの反射波（３）を受信するアンテナ、（70）
はアンテナを外界より保護するドーム、（８）はアンテ
ナ（７）で受信した受信信号より目標信号を発生する受
信機部、（９）は受信機部（８）の出力の目標信号より
目標方向指令信号、誘導信号及び送信指令信号を出力す
る信号処理部、（10）は信号処理部（９）の出力の目標
方向指令信号より送信波（２）の制御方向を制御するた
めのビーム制御信号を移相器（６）に出力するビーム制
御部、（11）は信号処理部（９）の出力の誘導信号より
制御装置Ｍの飛しょう経路を目標（１）との会合点方向
に操舵する操舵指令信号を出力するオートパイロツト、
（12）はオートパイロツト（11）の出力の操舵指令信号
により制御装置Ｍの飛しょう経路を目標（１）との会合
点方向に操舵する操舵装置、（13）は目標（１）近傍通
過時に近接起爆パルスを発生し、又、目標（１）に直撃
したとき着発起爆パルスを発生し、近接起爆パルス、又
は、着発起爆パルスにより弾頭を起爆する起爆信号を発
生する信管、（14）は目標（１）との会合時、信管（1
3）の出力の起爆信号により爆発し、目標（１）に対し
て大きなダメージを与える弾頭、（15）は制御装置Ｍの
構成品に必要な電力を供給する電源、（16）は制御装置
Ｍに推力を与える推進装置である。In FIG. 2, M is the control device, (1) is the target captured and tracked by the control device M, (2) is the transmitted wave irradiating the target (1), and (3) is the reflected wave from the target (1). , (4) generate a transmission signal of the transmission wave (2) for irradiating the target (1) with a transmission command signal output from the signal processing unit (9), and (5) a transmission wave (2). The transmission signal is supplied to the phase shifter (6) that controls the transmission direction of the signal and is not supplied to the receiver unit (8), and the reception signal received by the antenna (7) is supplied to the receiver unit (8). However, the circulator that does not supply the transmission source unit (4), (6) outputs the beam pointing direction, which is the reception direction of the reception wave (3) in the transmission direction of the transmission wave (2), to the output of the beam control unit (10). The phase shifter controlled by the beam control signal of (7) irradiates the target (1) with the transmitted wave (2) and reflects the reflected wave (3) from the target (1). Antenna for receiving, (70)
Is a dome that protects the antenna from the outside, (8) is a receiver unit that generates a target signal from the received signal received by the antenna (7), and (9) is a target direction from the target signal output from the receiver unit (8) A signal processing unit for outputting a command signal, a guidance signal and a transmission command signal, (10) is a beam control signal for controlling the control direction of the transmission wave (2) from the target direction command signal output from the signal processing unit (9) A beam control unit for outputting the signal to the phase shifter (6), and (11) steers the flight path of the control device M in the direction of the meeting point with the target (1) from the guidance signal output from the signal processing unit (9). An auto pilot that outputs a steering command signal,
(12) is a steering device that steers the flight path of the control device M toward the meeting point with the target (1) by a steering command signal output from the autopilot (11), and (13) is when passing near the target (1). A fuze that generates a proximity detonation pulse, and also generates an initiation detonation pulse when the target (1) is directly hit, and a detonation signal that detonates a warhead by a proximity detonation pulse or an arrival detonation pulse, (14) Is a fuze (1
A warhead that explodes due to the detonation signal of the output of 3) and causes great damage to the target (1), (15) is a power supply that supplies power necessary for the components of the control device M, and (16) is the control device M. It is a propulsion device that gives thrust to.
従来の、制御装置Ｍは以上の様に構成され、目標（１）
との会合点方向へと誘導し、最終的に制御装置Ｍ、目標
（１）に直撃するか又は、目標（１）の近傍通過時に起
爆信号を発生し弾頭（14）を起爆させ目標（１）に対し
大きなダメージを与え、目標（１）を撃墜する。The conventional controller M is configured as described above, and the target (1)
And then directly hit the control device M, the target (1), or generate a detonation signal when passing near the target (1) to detonate the warhead (14) and detonate the target (1). ), And shoot down the target (1).
ただし、目標（１）が大きな加速度で旋回した場合、あ
るいは高速度で飛行してきた目標（１）に対して、その
速度を見越して制御装置Ｍが飛しようする場合には、ビ
ーム指向方向と、制御装置Ｍの機軸方向は大きくずれ
る。いま、制御装置Ｍの機軸方向と、ビーム指向方向と
角度をビーム走査角と呼ぶ。目標（１）が大きな加速度
で旋回するほど、あるいは目標（１）が高速になるほ
ど、ビーム走査角は広い範囲まで制御する必要がある。
ビーム走査角が狭いままであると、ビーム走査角範囲外
に目標（１）が出てしまい、制御装置Ｍは、目標を見失
い、ロツクオフする。However, when the target (1) turns with a large acceleration, or when the control device M attempts to fly in anticipation of the speed with respect to the target (1) flying at a high speed, the beam pointing direction, The axial direction of the control device M is largely deviated. Now, the axis direction of the control device M and the angle between the beam pointing direction and the angle are called the beam scanning angle. The beam scanning angle needs to be controlled to a wider range as the target (1) turns with a larger acceleration or the target (1) becomes faster.
If the beam scanning angle remains narrow, the target (1) will be out of the beam scanning angle range, and the control device M will lose sight of the target and lock off.
ビーム走査角範囲を広くするためには、アンテナ（７）
に対しては、アンテナ特性を広い角度範囲で維持するこ
とが要求され、また、アンテナ（７）を制御装置Ｍが飛
しようしている間、外界より保護するためのドーム（7
0）に対しても、広い角度範囲で送信・受信時の電波透
過特性を、維持することが要求される。To widen the beam scanning angle range, the antenna (7)
, It is required to maintain the antenna characteristics in a wide angle range, and the dome (7) for protecting the antenna (7) from the outside while the controller M is about to fly.
For 0), it is required to maintain the radio wave transmission characteristics during transmission and reception in a wide angle range.
しかしながら、アンテナ特性を維持できる角度範囲には
限界があり、ドーム（70）についても、空力特性及び機
械的強度上、電波透過特性を維持できる角度範囲には限
界がある。However, there is a limit in the angle range in which the antenna characteristics can be maintained, and also in the dome (70), there is a limit in the angle range in which the radio wave transmission characteristics can be maintained due to aerodynamic characteristics and mechanical strength.
特に近年は、目標（１）の高速化、旋回能力の向上によ
り、上記限界を克服することが重要な課題となつてい
る。In particular, in recent years, it has become an important subject to overcome the above-mentioned limit by increasing the speed of the target (1) and improving the turning ability.
この発明は、制御装置Ｍのビーム走査角範囲に限界があ
る場合でも、アンテナ（７）のビーム走査角内にかつ、
ドーム（70）の送信・受信範囲内に常時、目標（１）が
入るように、制御装置Ｍの姿勢角及び飛しよう経路を制
御することにより、高旋回目標（１）に対するロツクオ
フを防止し、又、ロツクオフしたとしても目標との相対
距離及び目標変化に応じてアンテナビーム幅を必要最低
限に制御し（相対距離が短かくなる程目標旋回による制
御装置の目視線角の変化分が大きくなるため目標をビー
ム幅の中に入れておくためにはビーム幅を広くする必要
があるが広くすること妨害波の影響を受けやすくなるた
め必要最低限のビーム幅に設定する必要がある。）短時
間のうちに再ロツクできるようにすることにより目標
（１）撃墜能力を向上させる制御装置Ｍを得ることを目
的とする。また、この発明によりドームを改善できるた
め制御装置Ｍの高速化が可能となる。Even if the beam scanning angle range of the controller M is limited, the present invention is within the beam scanning angle of the antenna (7) and
By controlling the attitude angle and the flight path of the control device M so that the target (1) is always within the transmission / reception range of the dome (70), the lock-off to the high turning target (1) is prevented, Further, even if it is locked off, the antenna beam width is controlled to a necessary minimum according to the relative distance to the target and the target change (the shorter the relative distance, the larger the change in the visual line angle of the control device due to the target turning. Therefore, in order to keep the target within the beam width, it is necessary to widen the beam width, but it is necessary to set the beam width to the minimum necessary because widening makes it easier to be affected by interfering waves.) An object of the present invention is to obtain a control device M that improves target (1) shooting down ability by enabling re-locking in time. Further, since the dome can be improved by the present invention, the speed of the control device M can be increased.
この発明に係わる制御装置Ｍは、目標方向指令信号が所
定のレベルを越えない場合ローレベル信号を出力し、所
定のレベルを越えた場合ハイレベル信号を出力する手段
と、前記手段の出力がローレベルの場合ゼロ信号を出力
し、ハイレベル信号の場合目標方向指令信号の大きさに
応じた操舵指令補償信号を出力する手段と、前記手段の
出力とオートパイロツト（11）の出力の操舵指令信号を
たし算し補償操舵指令信号を操舵装置（12）に出力する
手段と目標方向信号より目標を制御装置がロツクオフし
たことを検知しロツクオフ信号を出力する手段と、目標
信号より目標と制御装置の相対距離を検知し相対距離信
号を出力する手段と、目標方向指令信号より目標の動き
の変化分を検知し目標変化信号を出力する手段と、ロツ
クオフ信号と相対距離信号と目標変化信号よりロツクオ
フ信号が入力した時のみ相対距離及び目標変化に応じて
必要最小限のビーム幅を設定するビーム幅制御信号を出
力する手段と、ビーム幅制御信号によりアンテナビーム
幅を制御する手段とを具備したものである。The control device M according to the present invention outputs a low level signal when the target direction command signal does not exceed the predetermined level and outputs a high level signal when the target direction command signal exceeds the predetermined level, and the output of the means is low. A means for outputting a zero signal in the case of a level signal, and a steering command compensation signal in the case of a high level signal, and a steering command signal of the output of said means and the output of the auto-pilot (11) Means for outputting a compensation steering command signal to the steering device (12), means for detecting that the control device has locked off the target from the target direction signal, and outputting a lock-off signal, and target and control device for the target signal. Means for detecting the relative distance of the target and outputting a relative distance signal, a means for detecting a change in the target movement from the target direction command signal and outputting a target change signal, a lock-off signal and a relative distance A means for outputting the beam width control signal that sets the minimum required beam width according to the relative distance and target change only when the lock-off signal is input from the separation signal and the target change signal, and the antenna beam width is controlled by the beam width control signal. And means for controlling.
この発明は、制御装置Ｍのアンテナ（７）のビーム走査
角範囲内に、また、ドーム（70）の送信・受信範囲内に
常時、目標（１）が入るように、制御装置Ｍの姿勢角及
び飛しよう経路を制御する。又ロツクオフしたとしても
目標との相対距離及び目標の変化に応じてアンテナビー
ム幅を制御し、短時間のうちに再ロツクできるように制
御装置を制御する。The present invention relates to the attitude angle of the control device M so that the target (1) is always within the beam scanning angle range of the antenna (7) of the control device M and within the transmission / reception range of the dome (70). And control the flight path. Even if the lock-off is performed, the antenna beam width is controlled according to the relative distance to the target and the change of the target, and the control device is controlled so that the antenna beam width can be re-locked within a short time.
第１図は、この発明の一実施例を示す図であり、（１）
〜（16）及び（70）は第２図と同じであり、（17）〜
（19）が第２図に対して新たに付加した装置である。FIG. 1 is a diagram showing an embodiment of the present invention.
~ (16) and (70) are the same as in Fig. 2, and (17) ~
(19) is a device newly added to FIG.
（17）は信号処理部（９）の出力の目標方向指令信号よ
り、目標方向指令信号が所定のレベルを越えない場合ロ
ーレベル信号を出力し、所定のレベルを越えた場合ハイ
レベル信号を出力するリミツタ回路、（18）はリミツタ
回路の出力がローレベル信号の場合ゼロ信号を出力しハ
イレベル信号の場合、信号処理部（９）の出力の目標方
向指令信号の大きさに応じた操舵指令補償信号を出力す
る操舵指令バイアス信号発生回路、（19）はオートパイ
ロツト（11）の出力の操舵指令信号と、操舵指令バイア
ス信号回路の操舵補償信号をたし算し補償操舵指令信号
を操舵装置（12）に出力する加算器、（20）は受信機部
（８）の出力の目標信号より目標（１）を制御装置Ｍが
ロツクオフしたことを検知しロツクオフ信号を出力する
ロツクオフ検知回路、（21）は受信機部（８）の出力の
目標信号より目標（１）と制御装置Ｍの相対距離を検知
し相対距離信号を出力する相対距離検知回路、（22）は
信号処理部（９）の出力の目標方向指令信号より目標
（１）の動きの変化分を検知し目標変化信号を出力する
目標方向変化分検知回路、（23）はロツクオフ検知回路
（20）の出力のロツクオフ信号と相対距離検知回路（2
1）の出力の相対距離信号と、目標方向変化分検知回路
（22）の出力の目標変化信号よりロツクオフ信号が入力
した時のみ相対距離及び目標変化に応じて必要最小限に
アンテナビーム幅を設定するビーム制御部信号を出力す
るビーム幅設定回路、（24）はビーム幅設定回路（23）
の出力のビーム幅制御信号よりアンテナビーム幅を制御
するビーム幅制御部とを有し目標（１）に会合する制御
装置Ｍである。(17) outputs a low level signal when the target direction command signal does not exceed a predetermined level from the target direction command signal output from the signal processing unit (9), and outputs a high level signal when the target direction command signal exceeds the predetermined level. The limiter circuit (18) outputs a zero signal when the output of the limiter circuit is a low level signal, and when the output of the limiter circuit is a high level signal, a steering command corresponding to the magnitude of the target direction command signal output from the signal processing unit (9). A steering command bias signal generation circuit that outputs a compensation signal, (19) is a steering device that adds the steering command signal of the output of the auto pilot (11) and the steering compensation signal of the steering command bias signal circuit to the steering device. An adder for outputting to (12), a lock-off detection circuit for outputting a lock-off signal by detecting that the control device M has locked off the target (1) from the target signal output from the receiver section (8), Reference numeral 21) is a relative distance detection circuit that detects the relative distance between the target (1) and the control device M from the target signal output from the receiver section (8) and outputs a relative distance signal, and (22) is the signal processing section (9). Target direction change detection circuit that detects the change in movement of target (1) from the target direction command signal of the output of and outputs the target change signal. (23) is relative to the lock-off signal of the output of lock-off detection circuit (20). Distance detection circuit (2
The antenna beam width is set to the minimum required according to the relative distance and target change only when the lock-off signal is input from the relative distance signal of the output of 1) and the target change signal of the target direction change detection circuit (22). Beam width setting circuit for outputting beam control signal, (24) is beam width setting circuit (23)
And a beam width control unit for controlling the antenna beam width based on the beam width control signal output by the control unit M for meeting the target (1).
上記の様に構成された制御装置Ｍにおいては、制御装置
Ｍが、アンテナ（７）のビーム走査範囲内に、また、ド
ームの送信・受信範囲内に常時、目標（１）が入るよう
に、制御装置Ｍの姿勢角及び、飛しよう経路を制御する
と同時に、ロツクオフしたとしても目標との相対距離及
び目標変化に応じてアンテナビーム幅を制御し短時間の
うちに再ロツクできるように制御することになる。In the control device M configured as described above, the control device M keeps the target (1) within the beam scanning range of the antenna (7) and the transmission / reception range of the dome, Controlling the attitude angle of the control device M and the flight path, and at the same time controlling the antenna beam width according to the relative distance to the target and the target change even if the lock-off is performed so that the lock can be performed again in a short time. become.
従つて高旋回Ｇ目標（１）に対してロツクオフが防止で
き又ロツクオフしたとしても短時間で再ロツクできるた
め目標撃墜能力の急激な低下が防止されることになる。Therefore, the lock-off can be prevented for the high turning G target (1), and even if the lock-off is performed, the lock-off can be re-locked in a short time, so that the sharp reduction of the target shooting ability can be prevented.
この発明は、以上説明したとおりの構成により、高旋回
目標、及び、高速度目標に対する、制御装置の目標撃墜
能力を向上させるという効果がある。The present invention has the effect of improving the target shooting ability of the control device for the high turning target and the high speed target by the configuration as described above.
第１図はこの発明の一実施例を示す構成ブロツク図、第
２図は、従来の制御装置を示す構成ブロツク図である。 図において、（１）は目標、（２）は送信波、（３）は
反射波、（４）は送信源部、（５）はサーキユレータ、
（６）は移相器、（７）はアンテナ、（70）はドーム、
（８）は受信機部、（９）は信号処理部、（10）はビー
ム制御部、（11）はオートパイロツト、（12）は操舵装
置、（13）は信管、（14）は弾頭、（15）は電源、（1
6）は推進装置、（17）はリミツタ回路、（18）は操舵
指令バイアス信号発生回路、（19）は加算器、（20）は
ロツクオフ検知回路、（21）は相対距離検知回路、（2
2）は目標方向変化分検知回路、（23）はビーム幅設定
回路、（24）はビーム幅制御部、Ｍは制御装置である。 なお、図中同一符号は同一又は相当部分を示す。FIG. 1 is a configuration block diagram showing an embodiment of the present invention, and FIG. 2 is a configuration block diagram showing a conventional control device. In the figure, (1) is a target, (2) is a transmitted wave, (3) is a reflected wave, (4) is a transmission source section, (5) is a circulator,
(6) is a phase shifter, (7) is an antenna, (70) is a dome,
(8) receiver unit, (9) signal processing unit, (10) beam control unit, (11) autopilot, (12) steering device, (13) fuze, (14) warhead, (15) is the power source, (1
6) a propulsion device, (17) a limiter circuit, (18) a steering command bias signal generation circuit, (19) an adder, (20) a lock-off detection circuit, (21) a relative distance detection circuit, (2
2) is a target direction change detection circuit, (23) is a beam width setting circuit, (24) is a beam width control unit, and M is a control device. The same reference numerals in the drawings indicate the same or corresponding parts.
───────────────────────────────────────────────────── フロントページの続き (51)Int.Cl.6 識別記号 庁内整理番号 ＦＩ 技術表示箇所 Ｇ０１Ｓ 13/88 Ｆ Ｍ Ｇ０５Ｄ 1/12 Ｄ ─────────────────────────────────────────────────── ─── Continuation of the front page (51) Int.Cl. 6 Identification code Internal reference number FI technical display location G01S 13/88 FM G05D 1/12 D
Claims (1)
る送信源部と、送信波の送信方向を制御する移相器に送
信信号を供給し、受信機部には供給せず、また、アンテ
ナ受信した受信信号を受信機部に供給し、送信源部には
供給しないサーキュレータと、送信波の信号方向を制御
する移相器と、送信波を目標に照射し、目標からの反射
波を受信するアンテナと、このアンテナを外界より保護
するドームと、上記アンテナで受信した受信信号より目
標信号を発生する受信機部と、目標信号より目標方向指
令信号、誘導信号及び送信指令信号を出力する信号処理
部と、目標方向指令信号より送信波の送信方向を制御す
るためのビーム制御信号を出力するビーム制御部と、誘
導信号より制御装置の飛しょう経路を目標との会合点方
向に操舵する操舵指令信号を発生するオートパイロット
と、操舵指令信号により制御装置の飛しょう経路を目標
との会合点方向に操舵する操舵装置と、目標近傍通過時
に近接起爆パルスを発生し、又、目標に直撃したとき着
発起爆パルスを発生し、近接起爆パルス、又は、着発起
爆パルスにより弾頭を起爆する起爆信号を発生する信管
と、目標との会合時、起爆信号により爆発し、目標に対
して大きなダメージを与える弾頭と、構成品に必要な電
力を供給する電源と、推力を与える推進装置を備えた制
御装置において、目標方向指令信号が所定のレベルを越
えない場合ローレベル信号を出力し、所定のレベルを越
えた場合ハイレベル信号を出力するリミッタ回路とリミ
ッタ回路の出力がローレベル信号の場合ゼロ信号を出力
し、ハイレベル信号の場合目標方向指令信号の大きさに
応じた操舵指令補償信号を出力する操舵指令バイアス信
号発生回路、操舵指令信号と操舵指令補償信号をたし算
し補償操舵指令信号を操舵装置に出力する加算器と、目
標信号より目標を制御装置がロックオフしたことを検知
し、ロックオフ信号を出力するロックオフ検知回路と、
目標信号より目標と制御装置の相対距離を検知し相対距
離信号を出力する相対距離検知回路と、目標方向指令信
号より目標の動きの変化分を検知し、目標変化信号を出
力する目標方向変化分検知回路と、ロックオフ信号と相
対距離信号と目標変化信号よりロックオフ信号が入力し
た時のみ相対距離及び目標変化に応じて必要最小限にア
ンテナビーム幅を設定するビーム幅制御信号を出力する
ビーム幅設定回路と、ビーム幅制御信号によりアンテナ
ビーム幅を制御するビーム幅制御部とで構成されたこと
を特徴とする制御装置。1. A transmission source unit for generating a transmission signal of a transmission wave for irradiating a target and a phase shifter for controlling a transmission direction of the transmission wave, the transmission signal is not supplied to a receiver unit, and , A circulator that supplies the received signal received by the antenna to the receiver section, but not to the transmission source section, a phase shifter that controls the signal direction of the transmitted wave, and a reflected wave from the target that irradiates the target with the transmitted wave. An antenna for receiving the signal, a dome that protects this antenna from the outside world, a receiver unit that generates a target signal from the received signal received by the antenna, and a target direction command signal, a guidance signal, and a transmission command signal that are output from the target signal. Signal processing unit, a beam control unit that outputs a beam control signal for controlling the transmission direction of the transmitted wave from the target direction command signal, and a guidance signal that steers the flight path of the control device toward the meeting point with the target. Steering Command signal to generate an autopilot, a steering device to steer the flight path of the control device toward the meeting point with the target by a steering command signal, a proximity detonation pulse when passing near the target, and a direct hit to the target. At the time of meeting with a target and a fuse that generates an initiation detonation pulse and generates a detonation signal to detonate a warhead by a proximity detonation pulse or an arrival detonation pulse, it explodes due to the detonation signal and causes large damage to the target. In a control device equipped with a warhead that gives a power, a power supply that supplies necessary power to the components, and a propulsion device that gives thrust, a low level signal is output if the target direction command signal does not exceed a predetermined level, and When the level exceeds the level, the limiter circuit that outputs a high level signal and the limiter circuit output a zero signal when the output is a low level signal, and a target direction when the output is a high level signal Steering command bias signal generation circuit that outputs a steering command compensation signal according to the magnitude of the command signal, an adder that adds the steering command signal and the steering command compensation signal, and outputs a compensation steering command signal to the steering device, and a target A lock-off detection circuit that detects that the control device has locked off the target from the signal and outputs a lock-off signal,
A relative distance detection circuit that detects the relative distance between the target and the control device from the target signal and outputs a relative distance signal, and a target distance change circuit that detects the change in target movement from the target direction command signal and outputs the target change signal A beam that outputs a beam width control signal that sets the antenna beam width to the minimum required according to the relative distance and target change only when the lock-off signal is input from the detection circuit, lock-off signal, relative distance signal, and target change signal A control device comprising a width setting circuit and a beam width control unit for controlling an antenna beam width by a beam width control signal.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63319984A JPH0794960B2 (en) | 1988-12-19 | 1988-12-19 | Control device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP63319984A JPH0794960B2 (en) | 1988-12-19 | 1988-12-19 | Control device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH02166398A JPH02166398A (en) | 1990-06-27 |
| JPH0794960B2 true JPH0794960B2 (en) | 1995-10-11 |
Family
ID=18116446
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP63319984A Expired - Fee Related JPH0794960B2 (en) | 1988-12-19 | 1988-12-19 | Control device |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH0794960B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021237481A1 (en) * | 2020-05-26 | 2021-12-02 | 深圳市大疆创新科技有限公司 | Control method and device for unmanned aerial vehicle |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2777026B2 (en) * | 1992-08-10 | 1998-07-16 | 三菱電機株式会社 | Phased array antenna device |
| CN113437518B (en) * | 2021-06-29 | 2022-08-05 | 中国西安卫星测控中心 | Scanning capture method based on paraboloid unified measurement and control antenna |
-
1988
- 1988-12-19 JP JP63319984A patent/JPH0794960B2/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2021237481A1 (en) * | 2020-05-26 | 2021-12-02 | 深圳市大疆创新科技有限公司 | Control method and device for unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH02166398A (en) | 1990-06-27 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JPH0794960B2 (en) | Control device | |
| JPH0331699A (en) | Control device | |
| JPH07117357B2 (en) | Control device | |
| JPH02103400A (en) | Missile | |
| JPH04140684A (en) | Controller | |
| JPH0781800B2 (en) | Control device | |
| JP2518086B2 (en) | Tracking device | |
| JP2650793B2 (en) | Guided flying object | |
| RU2253824C1 (en) | Method for guided missile guidance on air target (modifications) and radar set for its realization | |
| JP2536667B2 (en) | Tracking device | |
| JPH07190692A (en) | Guided missile | |
| JPH0771897A (en) | Guided missile | |
| JPH0289999A (en) | Controller | |
| JPS58195800A (en) | Induction missile | |
| JP2999065B2 (en) | Proximity fuse control device | |
| JP3231078B2 (en) | Proximity fuse control device | |
| JP2001201296A (en) | Missile system | |
| JP2738465B2 (en) | Proximity fuse control device | |
| JPH04263798A (en) | Controller | |
| JPH0571782U (en) | Control device | |
| JPH0718677B2 (en) | Proximity fuze | |
| JPH07280499A (en) | Guided missile | |
| JPH0711400B2 (en) | Flying body | |
| JPS6053797A (en) | Guided missile | |
| JPH07103696A (en) | Guided missile |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| LAPS | Cancellation because of no payment of annual fees |