JPS58178645A - Circuit for alarming fault of antenna - Google Patents
Circuit for alarming fault of antennaInfo
- Publication number
- JPS58178645A JPS58178645A JP57062144A JP6214482A JPS58178645A JP S58178645 A JPS58178645 A JP S58178645A JP 57062144 A JP57062144 A JP 57062144A JP 6214482 A JP6214482 A JP 6214482A JP S58178645 A JPS58178645 A JP S58178645A
- Authority
- JP
- Japan
- Prior art keywords
- antenna
- limiter
- transmission
- circuit
- pilot signal
- 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
- 230000005540 biological transmission Effects 0.000 claims abstract description 17
- 230000005856 abnormality Effects 0.000 claims description 25
- 229920006395 saturated elastomer Polymers 0.000 claims description 8
- 230000002159 abnormal effect Effects 0.000 claims description 4
- 238000011084 recovery Methods 0.000 abstract description 6
- 230000003111 delayed effect Effects 0.000 abstract 1
- 238000001514 detection method Methods 0.000 description 8
- 238000010586 diagram Methods 0.000 description 2
- 230000002457 bidirectional effect Effects 0.000 description 1
- 239000003795 chemical substances by application Substances 0.000 description 1
- 239000003814 drug Substances 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 230000007274 generation of a signal involved in cell-cell signaling Effects 0.000 description 1
- 230000007257 malfunction Effects 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Classifications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04B—TRANSMISSION
- H04B17/00—Monitoring; Testing
- H04B17/10—Monitoring; Testing of transmitters
- H04B17/15—Performance testing
- H04B17/17—Detection of non-compliance or faulty performance, e.g. response deviations
Landscapes
- Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Engineering & Computer Science (AREA)
- Computer Networks & Wireless Communication (AREA)
- Signal Processing (AREA)
- Emergency Alarm Devices (AREA)
- Details Of Aerials (AREA)
- Transceivers (AREA)
- Monitoring And Testing Of Transmission In General (AREA)
Abstract
Description
【発明の詳細な説明】
この発明は、空中線の異常から送受信機を保護するため
の空中線異常警報回路に関するものである。DETAILED DESCRIPTION OF THE INVENTION The present invention relates to an antenna abnormality warning circuit for protecting a transmitter/receiver from abnormalities in the antenna.
従来のこの種の装置として第1図に示すものがめった。As a conventional device of this type, the one shown in FIG. 1 is rare.
図において、(1)は空中線、(2)は方向性結合器、
(3)は送受切換器で、これはサーキュレータでもよい
。(4)は送信機、(5)は^周波増幅器、(6)およ
び(9)は切換回路、(7)は検波器、(8)は受信機
、(1■はパイロット信号発生器、01)は空中線(1
)の異常を判定する制御回路である。In the figure, (1) is an antenna, (2) is a directional coupler,
(3) is a transmitter/receiver switch, which may also be a circulator. (4) is a transmitter, (5) is a frequency amplifier, (6) and (9) are switching circuits, (7) is a detector, (8) is a receiver, (1■ is a pilot signal generator, 01 ) is the antenna (1
) is a control circuit that determines an abnormality.
次に動作について説明する。Next, the operation will be explained.
空中線(1)の異常を検出する場合は、切換回路(9)
および(61により、パイロット信号発生器aυおよび
検波器(7)を接続する。すると、パイロット信号発生
器(1Gから出力された信号は、切換回路(9)および
方向性結合器(2)を介して空中線(1)に送られ、空
中線は)で反射された信号は方向性結合器(2)、送受
切換器(3)、高周波増幅器(5)、切換回路(6)を
経て検波器(7)および制御回路αDに出力される。従
ってこの制御回路(Illにおいて検波器(7)の検波
レベルの大小により空中線[11の反射電力の大小を知
り、空中線il+の異常を検出することができる。When detecting an abnormality in the antenna (1), switch the switching circuit (9).
and (61) connect the pilot signal generator aυ and the detector (7).Then, the signal output from the pilot signal generator (1G) passes through the switching circuit (9) and the directional coupler (2). The signal reflected by the antenna (2) passes through a directional coupler (2), a transmitter/receiver switch (3), a high frequency amplifier (5), and a switching circuit (6) before being sent to a detector (7). ) and the control circuit αD.Therefore, in this control circuit (Ill), it is possible to know the magnitude of the reflected power of the antenna [11] based on the magnitude of the detection level of the detector (7), and to detect an abnormality in the antenna I1+.
従来の空中線異常警報回路は以上のように構成されてい
るので、レーダ運行前に空中線のチェックをしなければ
ならず、運行中のチェックは不可能でめった。また検波
器(7)の異常時にもその異常を検出できなくてシステ
ムとしてフェイルセイフとはなっておらず、高周波増幅
器(5)の安定度によっては誤動作することがあり、さ
らに受信系に切換回路が入っているため雑音指数が悪化
する等の欠点かあった。Since the conventional antenna abnormality warning circuit is constructed as described above, the antenna must be checked before radar operation, and checking during operation is rarely possible. In addition, even if the detector (7) has an abnormality, it cannot be detected and the system is not fail-safe. Depending on the stability of the high-frequency amplifier (5), it may malfunction, and there is also a switching circuit in the receiving system. There were drawbacks such as a worsening of the noise figure due to the inclusion of
この発明は上記のような従来のものの欠点を除去するた
めになされたもので、送信信号の反射電力を利用し、受
信系によって空中線の異常検出をすることにより、レー
ダ連用中に異常検出ができ、かつフェイルセイフな空中
線異常警報回路を提供することを目的としている。This invention was made in order to eliminate the drawbacks of the conventional systems as described above. By using the reflected power of the transmitted signal and detecting abnormalities in the antenna by the receiving system, abnormalities can be detected during continuous radar operation. The purpose of the present invention is to provide a fail-safe antenna abnormality warning circuit.
以下、この発明の一実施例を図について説明する。An embodiment of the present invention will be described below with reference to the drawings.
第2図は本発明の一実施例による空中線異常警報回路を
示す。図において、(1)は空中線、(2)は方向性結
合器、(3)はサーキュレータ又は送受切換器。FIG. 2 shows an antenna abnormality alarm circuit according to an embodiment of the present invention. In the figure, (1) is an antenna, (2) is a directional coupler, and (3) is a circulator or transmitter/receiver switch.
(4)はサーキュレータ又は送受切換器(3)、方向性
結合器(2)を介して空中線(1)に送信信号を供給す
る送信機、aυは方向性結合器(2)を介して空中線(
1)にパイロット信号を供給するパイロット信号発生器
、031は送信信号の送信直後に上記パイロット信号を
発生させるパイロット信号制御回路、0zは送受切換器
(3)と受信系α4との間に接続され送信時該受信系I
を保護するためのリミッタである。また受信糸Iにおい
て151は高周波増幅器、(7)は検波器、(11&)
はパイロット信号の発生直後からリミ、ツタ02か飽和
状態から回復するまでの時間を測定しこれを設定値と比
較して空中線(1)の異常を判定する異常判定回路、(
8)は受信信号を処理する受信機である。(4) is a transmitter that supplies transmission signals to the antenna (1) via a circulator or transmitter/receiver switch (3) and a directional coupler (2), and aυ is a transmitter that supplies a transmission signal to the antenna (1) via a directional coupler (2).
1) a pilot signal generator that supplies a pilot signal to When transmitting, the receiving system I
It is a limiter to protect the Also, in the receiving thread I, 151 is a high frequency amplifier, (7) is a detector, (11 &)
is an abnormality determination circuit that measures the time from immediately after the pilot signal is generated until the limit and ivy 02 recover from the saturated state, and compares this with a set value to determine whether there is an abnormality in the antenna (1).
8) is a receiver that processes the received signal.
第3図は上記回路のタイミングチャートを示し、図にお
いて、2は送信タイミング、bはパイロット信号発生タ
イミング、Cは空中線正常時・における検波器(7)の
検波出力、dは空中線異常時における検波器(7)の検
波出力であり、τ0は送信パルス幅、τ1はパイロット
信号パルス幅、τ2.τ4は空中線正常、異常時におけ
るリミッタ02の回復時間、τ8は異常判定回路(11
11)に設定されている判定時間である。Figure 3 shows a timing chart of the above circuit, in which 2 is the transmission timing, b is the pilot signal generation timing, C is the detection output of the detector (7) when the antenna is normal, and d is the detection output when the antenna is abnormal. is the detection output of the detector (7), τ0 is the transmission pulse width, τ1 is the pilot signal pulse width, τ2. τ4 is the recovery time of limiter 02 when the antenna is normal or abnormal, and τ8 is the abnormality judgment circuit (11
This is the determination time set in 11).
次に動作について説明する。Next, the operation will be explained.
送信時送信機(4)から出力された送信電力はサーキュ
レータ又は送受切換器(3)、方向性結合器(2)を経
て空中線(1)に至る。そしてこの空中線(1)からの
反射電力は方向性結合器(2)、サーキュレータ(3)
を経てリミッタ(12に印加され、その結果送信中リミ
ッタ(1カは飽和状態になっている。これは該リミッタ
(121には一定以上の電力か入力すると、飽和状態に
なってその出力を制限するという保a機能があるからで
あるか、このような飽和状態にある状態から上記−足以
上の電力入力かなくなったときの該リミッタt13の回
復時間は上記入力電力に比例する。At the time of transmission, the transmission power output from the transmitter (4) reaches the antenna (1) via a circulator or transmitter/receiver switch (3), and a directional coupler (2). The reflected power from this antenna (1) is transmitted to a directional coupler (2) and a circulator (3).
As a result, the limiter (12) is applied to the limiter (12) during transmission, and as a result, the limiter (121) is in a saturated state.This means that if more than a certain amount of power is input to the limiter (121), it becomes saturated and limits its output. This may be because the limiter t13 has a protection function that allows the limiter t13 to recover from such a saturated state when the power input is no more than the above-mentioned amount, and is proportional to the above-mentioned input power.
一方送他が完了すると同時にパイロット信号をパイロッ
ト信号発生器tlljから発生すると、パイロット信号
は方向性結合器(2)を経てリミッタ叩に至るが、この
時リミッタ021は飽和状態にあるため、アッテネータ
として機能する。そのためパイロット信号はリミッタ(
社)の回復時間の間リミッタ02に阻止されることとな
るが、このリミッタ(2)の回復時間は空中線(1)か
らの反射電力の小さい該空中線(1)の正常時は’2+
上記反射電力の大きい空中線は)の異常時はτ4である
。従って高周波増幅器(5)を経て検波器(7)の出力
として現われる波形は正常時、異常時それぞれ第3図c
、dの様になり、異常判だ回路(11λ)でτ8を判定
レベルとして設定しておけば、リミッタ(12が回復す
るまで、卸もリミッタレベルV6を出力するまでの時間
τ2又はτ4を該τ8と比較することにより空中線(1
)の正常、異常を検出できる。なお同図中の信号Cにお
いてリミッタO2か飽和状態から回復したあと出力する
上記リミッタレベルViはリミッタO2の飽和状態(送
信中)における出力レベル■sより多少小さい値となっ
ている。また回申の信号dにおける破線はパイロット信
号かflより長く続いたとしたときのりミッタ02の出
力波形を示す。On the other hand, when a pilot signal is generated from the pilot signal generator tllj at the same time as the transmission is completed, the pilot signal passes through the directional coupler (2) and hits the limiter, but since the limiter 021 is in a saturated state at this time, it is used as an attenuator. Function. Therefore, the pilot signal is limited by a limiter (
During the recovery time of the antenna (1), the recovery time of the limiter (2) is '2+' when the antenna (1) has a small reflected power and is normal.
The above-mentioned antenna with a large reflected power is τ4 at the time of abnormality. Therefore, the waveforms that appear as the output of the detector (7) after passing through the high frequency amplifier (5) are shown in Figure 3c in normal and abnormal conditions.
, d. If τ8 is set as the judgment level in the abnormality detection circuit (11λ), the time τ2 or τ4 until the limiter (12) is recovered and the wholesaler outputs the limiter level V6 can be set as the determination level. By comparing with τ8, the antenna (1
) can detect normality and abnormality. In addition, in the signal C in the figure, the limiter level Vi outputted after the limiter O2 recovers from the saturated state is a value somewhat smaller than the output level ■s of the limiter O2 in the saturated state (during transmission). Furthermore, the broken line in the circular signal d indicates the output waveform of the limiter 02 when the pilot signal continues longer than the pilot signal fl.
以上のように、この発明によれば、受信糸を保護するリ
ミッタを用い、送信信号の反射信号を利用して空中線の
異常検出を行なうように構成したので、送イg概の運用
中にも異常検出を行なうことができる。また受信系その
ものを利用し、パイロット信号が検出できなくなる状態
で異常を検出するため、尚周波回路から検波回路までの
いずれの回路の異常に対してもフェイルセイフに動作す
る。As described above, according to the present invention, a limiter is used to protect the receiving line, and the reflected signal of the transmitted signal is used to detect an abnormality in the antenna. Abnormality detection can be performed. Furthermore, since the reception system itself is used to detect an abnormality in a state where the pilot signal cannot be detected, it operates fail-safely even in the event of an abnormality in any circuit from the frequency circuit to the detection circuit.
さらに、試験信号回路をすでに装備しているシステムで
あれば、高価なマイクロ波部品を何一つ追加することな
く、制御系の変更と低い周波数帯1こおける安価な検波
回路の追加のみで実施できるので、装置が安価にでき、
信頼性を向上できる効果がめる。Furthermore, if the system is already equipped with a test signal circuit, it can be implemented by simply changing the control system and adding an inexpensive detection circuit in one low frequency band, without adding any expensive microwave components. , equipment can be made at low cost,
The effect of improving reliability can be seen.
第1図は従来の空中w異常警報回路のブロック図、第2
図はこの発明の一実施例による空中線異゛冨警報回路の
ブロック図、第3図はこの発明の動作説明のためのタイ
ムナヤート図である。
(1)・・・空中線、(4)・・・送信機、(3)・・
・送受切換器、(2)・・・方間性結合器、fiG・・
・パイロット信号発生器、03・・・パイロット信号制
御回路、O2・・・リミッタ、(8j・・・受信機、(
llj)・・・異常判定回路。
なお図中同一符号は同−又は相当部分を示す。
代 理 人 葛 野 信 −第1図
第2図
第3図
!11許庁12官殿
1.・11円の人手 特願昭 57−6214
4 号2、発明の名称 空中IMi4常−報囚
籍3、 ?11i +1:、をする者
’JGf’lとの関係 特許出願人5、補正の対象
明細書の発明の詳細な説明の蜂
6、補止の内科
明細書をつき゛のとおり訂市する、
明細−FをつぎのとおりJ1圧する。Figure 1 is a block diagram of a conventional aerial w abnormality alarm circuit;
The figure is a block diagram of an antenna overload alarm circuit according to an embodiment of the present invention, and FIG. 3 is a time chart for explaining the operation of the present invention. (1)...Antenna, (4)...Transmitter, (3)...
・Transmission/reception switch, (2)...bidirectional coupler, fiG...
・Pilot signal generator, 03...Pilot signal control circuit, O2...Limiter, (8j...Receiver, (
llj)...Abnormality determination circuit. Note that the same reference numerals in the figures indicate the same or equivalent parts. Agent Makoto Kuzuno - Figure 1, Figure 2, Figure 3! 11 Government offices 12 Government buildings 1.・11 yen labor special request Sho 57-6214
4 No. 2, Name of the invention Aerial IMi4 Regular Report 3, ? 11i +1: Relationship with the person 'JGf'l Patent applicant 5, Detailed explanation of the invention in the specification subject to amendment 6, Revise the supplementary internal medicine specification as per ゛, Specification - Apply F to J1 pressure as follows.
Claims (1)
結合器を介して送信信号を供給する送信機と、上記方向
性結合器を介して上記空中線にパイロット信号を送出す
るパイロット信号発生器と、上記送信信号の送信直後に
上記パイロット信号を発生せしめるパイロット信号制御
回路と、上記送受切換器と受信系との間に接続され送信
時該受信系を保°護するためのリミッタと、上記パイロ
ット信号の発生直後から上記リミッタが飽和状態から回
復するまでの時間を測足し上記空中線の異常を判定する
異常判定回路とを備えたことを特徴とする空中線異常V
軸回路。(1) An antenna, a transmitter that supplies a transmission signal to the antenna via a transmission/reception switch and a directional coupler, and a pilot signal generator that sends a pilot signal to the antenna via the directional coupler. , a pilot signal control circuit that generates the pilot signal immediately after transmitting the transmission signal, a limiter connected between the transmission/reception switch and the reception system to protect the reception system during transmission, and the pilot. An antenna abnormality V characterized by comprising: an abnormality determination circuit that measures the time from immediately after a signal is generated until the limiter recovers from a saturated state and determines whether the antenna is abnormal.
axis circuit.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57062144A JPS58178645A (en) | 1982-04-12 | 1982-04-12 | Circuit for alarming fault of antenna |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
JP57062144A JPS58178645A (en) | 1982-04-12 | 1982-04-12 | Circuit for alarming fault of antenna |
Publications (2)
Publication Number | Publication Date |
---|---|
JPS58178645A true JPS58178645A (en) | 1983-10-19 |
JPH0376055B2 JPH0376055B2 (en) | 1991-12-04 |
Family
ID=13191602
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
JP57062144A Granted JPS58178645A (en) | 1982-04-12 | 1982-04-12 | Circuit for alarming fault of antenna |
Country Status (1)
Country | Link |
---|---|
JP (1) | JPS58178645A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1995024059A3 (en) * | 1994-02-23 | 1995-10-12 | Allgon Ab | System for antenna supervising |
WO2008023097A1 (en) * | 2006-08-24 | 2008-02-28 | Idesco Oy | Component mismatch identification in rfid reader |
-
1982
- 1982-04-12 JP JP57062144A patent/JPS58178645A/en active Granted
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO1995024059A3 (en) * | 1994-02-23 | 1995-10-12 | Allgon Ab | System for antenna supervising |
WO2008023097A1 (en) * | 2006-08-24 | 2008-02-28 | Idesco Oy | Component mismatch identification in rfid reader |
Also Published As
Publication number | Publication date |
---|---|
JPH0376055B2 (en) | 1991-12-04 |
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