JPH0348709B2 - - Google Patents
Info
- Publication number
- JPH0348709B2 JPH0348709B2 JP56208159A JP20815981A JPH0348709B2 JP H0348709 B2 JPH0348709 B2 JP H0348709B2 JP 56208159 A JP56208159 A JP 56208159A JP 20815981 A JP20815981 A JP 20815981A JP H0348709 B2 JPH0348709 B2 JP H0348709B2
- Authority
- JP
- Japan
- Prior art keywords
- output
- signal
- pilot
- circuit
- video 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.)
- Expired - Lifetime
Links
Classifications
-
- H—ELECTRICITY
- H04—ELECTRIC COMMUNICATION TECHNIQUE
- H04N—PICTORIAL COMMUNICATION, e.g. TELEVISION
- H04N7/00—Television systems
- H04N7/10—Adaptations for transmission by electrical cable
Landscapes
- Engineering & Computer Science (AREA)
- Multimedia (AREA)
- Signal Processing (AREA)
- Television Receiver Circuits (AREA)
Description
【発明の詳細な説明】
(技術分野)
本発明は、映像信号とパイロツト・キヤリアの
混変調歪の影響を受けない映像信号伝送用のパイ
ロツトAGC方式に関するものである。DETAILED DESCRIPTION OF THE INVENTION (Technical Field) The present invention relates to a pilot AGC method for video signal transmission that is not affected by cross-modulation distortion between a video signal and a pilot carrier.
(背景技術)
従来のパイロツトAGC方式のブロツク図を第
1図に示す。第1図において、VIDEO INは映
像信号入力、BA1は映像入力増幅回路、OSCは
パイロツト・キヤリア発生回路、MIXは映像信
号とパイロツト・キヤリアを混合する混合回路、
DRは送信出力回路、Lは伝送路、AMPは受信
側入力増幅器、AGCは利得制御回路、LPF1は
パイロツト・キヤリアを除去するローパス・フイ
ルタ、BA2は映像信号出力回路、VIDEO OUT
は映像信号出力、BPFはパイロツト・キヤリア
を抜き出すためのバンドパス・フイルタ、DET
はパイロツト・キヤリアを検波する検波器、
LPF2は検波器出力を平滑するローパス・フイ
ルタ、DAはローパス・フイルタLPF2出力と基
準電位とを比較増幅する比較増幅回路の如く構成
されており、自動利得制御AGC動作は、送信側
で挿入されたパイロツト・キヤリアを受信側で検
波・平滑し、基準電位と比較してパイロツトレベ
ルが常に一定になるように利得制御回路を制御す
ることにより行なわれる。(Background Art) Figure 1 shows a block diagram of the conventional pilot AGC system. In Figure 1, VIDEO IN is a video signal input, BA1 is a video input amplification circuit, OSC is a pilot carrier generation circuit, MIX is a mixing circuit that mixes the video signal and pilot carrier,
DR is the transmission output circuit, L is the transmission line, AMP is the receiving side input amplifier, AGC is the gain control circuit, LPF1 is the low-pass filter that removes the pilot carrier, BA2 is the video signal output circuit, VIDEO OUT
is the video signal output, BPF is the bandpass filter for extracting the pilot carrier, DET
is a detector that detects the pilot carrier,
LPF2 is configured as a low-pass filter that smoothes the detector output, and DA is configured as a comparison amplifier circuit that compares and amplifies the low-pass filter LPF2 output and a reference potential.Automatic gain control AGC operation is inserted on the transmitting side. This is done by detecting and smoothing the pilot carrier on the receiving side, comparing it with a reference potential, and controlling the gain control circuit so that the pilot level is always constant.
ここで、映像信号とパイロツト・キヤリアを混
合する混合回路MIXからパイロツト・キヤリア
を除去するローパス・フイルタLPF1までの間
DR,L,AMP,AGCに非直線性が存在すると、
映像信号とパイロツト・キヤリアが混変調を受け
る。 Here, from the mixing circuit MIX that mixes the video signal and the pilot carrier to the low pass filter LPF1 that removes the pilot carrier,
If nonlinearity exists in DR, L, AMP, and AGC,
The video signal and pilot carrier undergo cross modulation.
従つて、混変調によるビート障害を起こす欠点
があつた。 Therefore, it has the disadvantage of causing beat disturbances due to cross-modulation.
(発明の課題)
本発明は、パイロツト・キヤリアを映像信号に
同期して間歇的に挿入し(同期信号期間)、映像
信号とパイロツト・キヤリアが同時に存在しない
ようにしたことを特徴とし、その目的は映像信号
とパイロツト・キヤリアの混変調の除去であり、
以下詳細に説明する。(Problem to be solved by the invention) The present invention is characterized in that a pilot carrier is inserted intermittently in synchronization with a video signal (synchronization signal period) so that the video signal and the pilot carrier do not exist at the same time. is the removal of cross modulation between the video signal and the pilot carrier,
This will be explained in detail below.
(発明の構成及び作用)
第2図は本発明の実施例であつて、VIDEO
INは映像信号入力、BA1は映像入力増幅回路、
CLP1はクランプ回路(直流再生回路)、MIXは
混合回路、DRはLED駆動回路、LEDは発光ダイ
オード、OPT.OUTは光出力、S.Sは水平同期信
号分離回路、BOはブロツキング発振回路、PG1
はクランプパルス発生回路、OSCはパイロツ
ト・キヤリア発生回路、ASWはアナログ・スイ
ツチ、PG2はアナログ・スイツチ制御パルス発
生回路、OFは光フアイバー・ケーブル、OPT.
INは光入力、APDは受光ダイオード(アバラン
シエ・フオト・ダイオード)、AMPは受光増幅
器、LPE1はローパス・フイルタ、CLP2はク
ランプ回路(直流再生回路)、BA2は映像信号
出力回路、VIDEO OUTは映像信号出力、BPF
はパイロツト信号抽出用の抽出フイルタで、バン
ドパス・フイルタ又はハイパス・フイルタで構成
される。DETはパイロツト・キヤリア検波器、
LPF2はローパス・フイルタ、DAは比較増幅回
路、DC/DCはDC/DCコンバータ、LPF3はロ
ーパス・フイルタ、PG3はクランプパルス発生
回路である。ここで、パイロツト・キヤリア発生
回路OSCの周波数は映像信号の帯域外に設定さ
れ、ブロツキング発振回路BOの自走周波数は水
平同期周波数付近でこれよりやや低い周波数に設
定され、ローパス・フイルタLPF1のカツトオ
フ周波数は映像信号を通過させ、パイロツト・キ
ヤリアを阻止するように設定され、ローパス・フ
イルタLPF2のカツトオフ周波数は水平同期信
号周波数に比べて十分低く設定され、ローパス・
フイルタLPF3のカツトオフ周波数は水平同期
信号周波数よりも高く、かつ、パイロツト・キヤ
リアよりも低く(水平同期パルスを再生できる)
設定されているものとする。(Structure and operation of the invention) Figure 2 shows an embodiment of the present invention.
IN is video signal input, BA1 is video input amplification circuit,
CLP1 is a clamp circuit (DC regeneration circuit), MIX is a mixing circuit, DR is an LED drive circuit, LED is a light emitting diode, OPT.OUT is an optical output, SS is a horizontal synchronizing signal separation circuit, BO is a blocking oscillation circuit, PG1
is a clamp pulse generation circuit, OSC is a pilot carrier generation circuit, ASW is an analog switch, PG2 is an analog switch control pulse generation circuit, OF is an optical fiber cable, and OPT.
IN is optical input, APD is light receiving diode (avalanche photo diode), AMP is light receiving amplifier, LPE1 is low pass filter, CLP2 is clamp circuit (DC regeneration circuit), BA2 is video signal output circuit, VIDEO OUT is video signal Output, BPF
is an extraction filter for extracting the pilot signal, and is composed of a bandpass filter or a highpass filter. DET is a pilot carrier detector;
LPF2 is a low-pass filter, DA is a comparison amplifier circuit, DC/DC is a DC/DC converter, LPF3 is a low-pass filter, and PG3 is a clamp pulse generation circuit. Here, the frequency of the pilot carrier generation circuit OSC is set outside the band of the video signal, the free-running frequency of the blocking oscillator circuit BO is set at a frequency slightly lower than the horizontal synchronization frequency, and the cutoff of the low-pass filter LPF1 is set. The frequency is set to pass the video signal and block the pilot carrier, and the cutoff frequency of the low-pass filter LPF2 is set sufficiently low compared to the horizontal synchronization signal frequency.
The cutoff frequency of filter LPF3 is higher than the horizontal synchronization signal frequency and lower than the pilot carrier (can reproduce the horizontal synchronization pulse).
It is assumed that this has been set.
第3図は第2図の動作説明図であつて、第3図
の1〜19の番号は第2図に対応する。第3図に
おいて左側の図は正常時の波形図で、右側は送信
側映像入力断の時の波形図である。正常時は、送
信側で入力映像信号の水平同期信号部分にパイロ
ツト・キヤリアが挿入され、受信側でパイロツ
ト・キヤリアが検波・平滑され、比較増幅回路
DAで基準電位と比較増幅され、さらにDC/DC
コンバータで高圧に変換されて受光ダイオード
APDのバイアスとして加えられ、AGC動作が行
なわれる。利得制御された映像信号17は、クラ
ンプ回路CLP2で直流変動及び低域歪が改善さ
れる。クランプパルス16は、検波出力14をロ
ーパス・フイルタLPF3を経由してクランプパ
ルス発生回路PG3に与えて作られる。送信側映
像入力断の時は、同期分離回路出力4がなくなる
ので、ブロツキング発振回路BDは水平同期周波
数に近い自走周波数で発振し、正常時と同様にパ
イロツト・キヤリアを送出する。従つて、受信側
のAGCループAPD,AMP,BPF,DET,LPF
2,DA,DC/DCは正常時と同様に動作し、い
つ映像信号が入力されてもAGCループは瞬時に
動作できるようになつている。 FIG. 3 is an explanatory diagram of the operation of FIG. 2, and the numbers 1 to 19 in FIG. 3 correspond to those in FIG. In FIG. 3, the diagram on the left is a waveform diagram during normal operation, and the diagram on the right is a diagram when video input on the transmitting side is cut off. Under normal conditions, a pilot carrier is inserted into the horizontal synchronization signal portion of the input video signal on the transmitting side, and the pilot carrier is detected and smoothed on the receiving side, and then sent to the comparison amplifier circuit.
The DA compares and amplifies the reference potential, and then DC/DC
The converter converts it to high voltage and the light receiving diode
It is added as a bias to APD and performs AGC operation. The gain-controlled video signal 17 has DC fluctuations and low-frequency distortion improved by the clamp circuit CLP2. The clamp pulse 16 is generated by applying the detection output 14 to a clamp pulse generation circuit PG3 via a low-pass filter LPF3. When the video input on the transmitting side is cut off, the synchronization separation circuit output 4 disappears, so the blocking oscillation circuit BD oscillates at a free-running frequency close to the horizontal synchronization frequency and sends out the pilot carrier as in normal times. Therefore, the receiving side AGC loop APD, AMP, BPF, DET, LPF
2. DA and DC/DC operate as they normally would, and the AGC loop can operate instantly no matter when a video signal is input.
本実施例では、パイロツト・キヤリアの挿入位
置は水平同期信号部分(シンクチツプ)である
が、映像信号のないバツク・ポーチもしくはフロ
ント・ポーチに挿入しても効果は同じである。 In this embodiment, the pilot carrier is inserted in the horizontal synchronizing signal section (sync chip), but the effect is the same even if it is inserted in the back pouch or front pouch where there is no video signal.
(発明の効果)
以上説明したように実施例では、映像信号とパ
イロツト・キヤリアが同時に存在しないようにな
つているので、発光ダイオードLED、受光ダイ
オードAPD,LED駆動回路、受光増幅器AMPに
非直線性があつても混変調によるビート障害を起
こさない利点がある。(Effects of the Invention) As explained above, in the embodiment, the video signal and the pilot carrier do not exist at the same time, so nonlinearity occurs in the light emitting diode LED, the light receiving diode APD, the LED drive circuit, and the light receiving amplifier AMP. This has the advantage of not causing beat disturbances due to cross-modulation even if there is a problem.
また、水平同期信号に同期してパイロツト・キ
ヤリアが挿入されるので、受信側でパイロツト・
キヤリア検波器することにより直流再生用のクラ
ンプパルス16を確実に再生することができる。
すなわち、映像信号のAPL変動及びノイズの影
響を受けにくい利点がある。さらに、ブロツキン
グ発振回路をもつので、映像信号が断のときでも
AGC動作が行なわれる。 In addition, since the pilot carrier is inserted in synchronization with the horizontal synchronization signal, the pilot carrier is inserted on the receiving side.
By using a carrier detector, the clamp pulse 16 for DC reproduction can be reliably reproduced.
That is, it has the advantage of being less susceptible to APL fluctuations and noise of the video signal. Furthermore, since it has a blocking oscillation circuit, it can be used even when the video signal is cut off.
AGC operation is performed.
本発明は、伝送系に非直線性があつても混変調
によるビート障害を受けない利点があり、直接光
強度変調による映像信号の伝送に利用することが
できる。送信側で挿入されたパイロツト・キヤリ
アは、AGCの他回線監視、クランプパルス発生
に利用することができる。 The present invention has the advantage that even if there is nonlinearity in the transmission system, there is no beat disturbance due to cross modulation, and it can be used for transmitting video signals by direct optical intensity modulation. The pilot carrier inserted on the transmitting side can be used for AGC monitoring other lines and generating clamp pulses.
第1図は従来のパイロツトAGC方式のブロツ
ク図、第2図は本発明の実施例のブロツク図、第
3図は第2図の動作説明図である。
VIDEO IN…映像信号入力、BA1…映像入力
増幅回路、OSC…パイロツト・キヤリア発生回
路、MIX…混合回路、DR…送信出力回路/LED
駆動回路、L…伝送路、AMP…受信側入力増幅
器/受光増幅器、AGC…利得制御回路、LPF1,
LPF2,LPF3…ローパス・フイルタ、BA2…
映像信号出力回路、VIDEO OUT…映像信号出
力、BPF…バンドパス・フイルタ、DET…検波
器、DA…比較増幅回路、CLP1,CLP2…クラ
ンプ回路(直流再生回路)、LED…発光ダイオー
ド、OPT.OUT…光出力、S.S…水平同期信号分
離回路、BO…ブロツキング発振回路、PG1,
PG2,PG3……パルス発生回路、ASW…アナ
ログ・スイツチ、OF…光フアイバ・ケーブル、
OPT.IN…光入力、APD…受光ダイオード(ア
バランシエ・フオト・ダイオード)、DC/DC…
DC/DCコンバータ。
FIG. 1 is a block diagram of a conventional pilot AGC system, FIG. 2 is a block diagram of an embodiment of the present invention, and FIG. 3 is an explanatory diagram of the operation of FIG. 2. VIDEO IN...Video signal input, BA1...Video input amplifier circuit, OSC...Pilot carrier generation circuit, MIX...Mixing circuit, DR...Transmission output circuit/LED
Drive circuit, L...transmission line, AMP...receiving side input amplifier/light receiving amplifier, AGC...gain control circuit, LPF1,
LPF2, LPF3...Low pass filter, BA2...
Video signal output circuit, VIDEO OUT...Video signal output, BPF...Band pass filter, DET...Detector, DA...Comparison amplifier circuit, CLP1, CLP2...Clamp circuit (DC regeneration circuit), LED...Light emitting diode, OPT.OUT …Optical output, SS…Horizontal synchronization signal separation circuit, BO…Blocking oscillation circuit, PG1,
PG2, PG3...Pulse generation circuit, ASW...Analog switch, OF...Optical fiber cable,
OPT.IN…Optical input, APD…Photodetector diode (avalanche photo diode), DC/DC…
DC/DC converter.
Claims (1)
号期間のみにパイロツト信号を挿入し、映像信号
の伝送系の受信側では、該パイロツト信号の受信
レベルに従つて利得制御するパイロツトAGC方
式において、 送信側には、同期信号をふくむ映像信号を受容
する入力端子VIDEO INと、映像信号から同期
信号を抜き出す水平同期信号分離回路SSと、抜
き出された水平同期信号によりトリガされ自走周
波数が水平同期周波数よりやや低いブロツキング
発振回路BOと、映像信号の帯域外の周波数を発
生するパイロツト・キヤリア発生回路OSCと、
該発生回路の出力をブロツキング発振回路BOの
出力に同期してスイツチングする手段PG2,
ASWと、該手段の出力のパイロツト信号と映像
信号とを混合して水平同期期間にパイロツト信号
を挿入する混合回路MIXと、その出力を伝送路
に送出する手段とが具備され、受信側では、利得
制御手段APDと、受信信号からパイロツト信号
を抜き出す抽出フイルタBPFと、その出力を検
波する検波器DETと、検波器の出力を平滑する
ローパス・フイルタLPF2と、その出力レベル
を基準電位と比較し両者の差分に従つて前記利得
制御手段APDの利得を制御する比較増幅回路DA
と、利得制御手段の出力から映像信号と同期信号
のみをとり出すローパス・フイルタLPF1と、
その出力にクランプ回路CLP2を介して接続さ
れ映像出力を与える出力端子VIDEO OUTと、
前記検波器DETの出力に従つてクランプ回路
CLP2にクランプパルスを与える手段LPF3,
PG3とを具備して構成されることを特徴とする
同期式パイロツトAGC方式。 2 パイロツト信号を抜き出す抽出フイルタ
BPFがバンドパス・フイルタである特許請求の
範囲第1項記載の同期式パイロツトAGC方式。 3 パイロツト信号の周波数が映像信号の周波数
よりも高い時にはパイロツト信号を抜き出す抽出
フイルタが、ハイパス・フイルタである特許請求
の範囲第1項記載の同期式パイロツトAGC方式。[Scope of Claims] 1. On the transmitting side of the video signal transmission system, a pilot signal is inserted only in the horizontal synchronization signal period, and on the receiving side of the video signal transmission system, gain control is performed according to the reception level of the pilot signal. In the pilot AGC method, on the transmitting side, there is an input terminal VIDEO IN that receives the video signal including the synchronization signal, a horizontal synchronization signal separation circuit SS that extracts the synchronization signal from the video signal, and a trigger that is triggered by the extracted horizontal synchronization signal. a blocking oscillation circuit BO whose free-running frequency is slightly lower than the horizontal synchronization frequency, and a pilot carrier generation circuit OSC which generates a frequency outside the video signal band.
means PG2 for switching the output of the generating circuit in synchronization with the output of the blocking oscillation circuit BO;
The ASW is equipped with a mixing circuit MIX that mixes the pilot signal and video signal output from the means and inserts the pilot signal into the horizontal synchronization period, and means that sends the output to the transmission line. A gain control means APD, an extraction filter BPF that extracts the pilot signal from the received signal, a detector DET that detects the output thereof, a low pass filter LPF2 that smoothes the output of the detector, and compares the output level with a reference potential. a comparison amplifier circuit DA that controls the gain of the gain control means APD according to the difference between the two;
and a low-pass filter LPF1 that extracts only the video signal and synchronization signal from the output of the gain control means,
an output terminal VIDEO OUT which is connected to the output via the clamp circuit CLP2 and provides video output;
Clamp circuit according to the output of the detector DET
means LPF3 for applying a clamp pulse to CLP2;
A synchronous pilot AGC system characterized by being configured with PG3. 2 Extraction filter that extracts the pilot signal
The synchronous pilot AGC system according to claim 1, wherein the BPF is a bandpass filter. 3. The synchronous pilot AGC system according to claim 1, wherein the extraction filter for extracting the pilot signal when the frequency of the pilot signal is higher than the frequency of the video signal is a high-pass filter.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP20815981A JPS58111495A (en) | 1981-12-24 | 1981-12-24 | Synchronizing pilot agc system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP20815981A JPS58111495A (en) | 1981-12-24 | 1981-12-24 | Synchronizing pilot agc system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS58111495A JPS58111495A (en) | 1983-07-02 |
| JPH0348709B2 true JPH0348709B2 (en) | 1991-07-25 |
Family
ID=16551621
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP20815981A Granted JPS58111495A (en) | 1981-12-24 | 1981-12-24 | Synchronizing pilot agc system |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS58111495A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5410363A (en) * | 1992-12-08 | 1995-04-25 | Lightwave Communications, Inc. | Automatic gain control device for transmitting video signals between two locations by use of a known reference pulse during vertical blanking period so as to control the gain of the video signals at the second location |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPS51120608A (en) * | 1975-04-16 | 1976-10-22 | Nec Corp | Tv transmission automatic gain control system |
-
1981
- 1981-12-24 JP JP20815981A patent/JPS58111495A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS58111495A (en) | 1983-07-02 |
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