JPS6321975B2 - - Google Patents

Info

Publication number
JPS6321975B2
JPS6321975B2 JP55139363A JP13936380A JPS6321975B2 JP S6321975 B2 JPS6321975 B2 JP S6321975B2 JP 55139363 A JP55139363 A JP 55139363A JP 13936380 A JP13936380 A JP 13936380A JP S6321975 B2 JPS6321975 B2 JP S6321975B2
Authority
JP
Japan
Prior art keywords
frequency
track
signal
frequencies
pilot
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
Application number
JP55139363A
Other languages
Japanese (ja)
Other versions
JPS5764327A (en
Inventor
Akira Hirota
Seisuke Hirakuri
Taku Uchiumi
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Victor Company of Japan Ltd
Original Assignee
Victor Company of Japan Ltd
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Victor Company of Japan Ltd filed Critical Victor Company of Japan Ltd
Priority to JP55139363A priority Critical patent/JPS5764327A/en
Priority to US06/308,666 priority patent/US4414586A/en
Priority to DE3139810A priority patent/DE3139810C2/en
Publication of JPS5764327A publication Critical patent/JPS5764327A/en
Publication of JPS6321975B2 publication Critical patent/JPS6321975B2/ja
Granted legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G11INFORMATION STORAGE
    • G11BINFORMATION STORAGE BASED ON RELATIVE MOVEMENT BETWEEN RECORD CARRIER AND TRANSDUCER
    • G11B5/00Recording by magnetisation or demagnetisation of a record carrier; Reproducing by magnetic means; Record carriers therefor
    • G11B5/48Disposition or mounting of heads or head supports relative to record carriers ; arrangements of heads, e.g. for scanning the record carrier to increase the relative speed
    • G11B5/58Disposition or mounting of heads or head supports relative to record carriers ; arrangements of heads, e.g. for scanning the record carrier to increase the relative speed with provision for moving the head for the purpose of maintaining alignment of the head relative to the record carrier during transducing operation, e.g. to compensate for surface irregularities of the latter or for track following
    • G11B5/584Disposition or mounting of heads or head supports relative to record carriers ; arrangements of heads, e.g. for scanning the record carrier to increase the relative speed with provision for moving the head for the purpose of maintaining alignment of the head relative to the record carrier during transducing operation, e.g. to compensate for surface irregularities of the latter or for track following for track following on tapes
    • G11B5/588Disposition or mounting of heads or head supports relative to record carriers ; arrangements of heads, e.g. for scanning the record carrier to increase the relative speed with provision for moving the head for the purpose of maintaining alignment of the head relative to the record carrier during transducing operation, e.g. to compensate for surface irregularities of the latter or for track following for track following on tapes by controlling the position of the rotating heads
    • G11B5/592Disposition or mounting of heads or head supports relative to record carriers ; arrangements of heads, e.g. for scanning the record carrier to increase the relative speed with provision for moving the head for the purpose of maintaining alignment of the head relative to the record carrier during transducing operation, e.g. to compensate for surface irregularities of the latter or for track following for track following on tapes by controlling the position of the rotating heads using bimorph elements supporting the heads

Description

【発明の詳細な説明】 本発明はパイロツト信号記録再生方式に係り、
少なくとも4種類の所定周波数の信号をパイロツ
ト信号としてトラツク毎に巡回的に切換えて順次
記録し、再生時は走査すべきトラツクの両側のト
ラツクから再生される2種類のパイロツト信号を
弁別再生することにより、比較的狭帯域でトラツ
クずれ情報を得るためのパイロツト信号を記録再
生でき、もつて特にトラツクの曲り等に追従して
ヘツドを変位制御せしめうる構成のヘリカルスキ
ヤン型磁気記録再生装置やデイスク再生装置等に
適用して好適なパイロツト信号記録再生方式を提
供することを目的とする。
[Detailed Description of the Invention] The present invention relates to a pilot signal recording and reproducing method,
At least four types of predetermined frequency signals are cyclically switched for each track as pilot signals and recorded sequentially, and during reproduction, two types of pilot signals reproduced from tracks on both sides of the track to be scanned are selectively reproduced. Helical scan type magnetic recording and reproducing apparatuses and disk reproducing apparatuses that are capable of recording and reproducing pilot signals for obtaining track deviation information in a relatively narrow band, and that are capable of controlling the displacement of the head in particular by following track bends, etc. It is an object of the present invention to provide a pilot signal recording and reproducing method suitable for application to, etc.

近年、家庭用ヘリカルスキヤン型回転ヘツド磁
気記録再生装置(以下「ホームVTR」と称す)
は、磁気テープの改良、回転ヘツドの高感度化等
と相まつて記録再生密度の一層の高密度化が図ら
れ、テープスピード、トラツクピツチ等を例えば
従来の2時間の記録再生可能な場合のそれの約1/
3に減少して6時間の記録再生を行なうような長
時間のホームVTRが商品化されるに至つている。
しかるに、上記の高密度化は低コスト化のためテ
ープ走行系が簡略化されているホームVTRでは、
ビデオトラツクの曲りに追従して所要のトラツキ
ング精度を安定に保持することが困難となり、特
に他のホームVTRで記録された磁気テープを別
のホームVTRで再生する所謂互換再生時には上
記の所要のトラツキング精度を安定に保持するこ
とは困難であり、高品質な画質が得られていない
のが現状であつた。
In recent years, household helical scan rotary head magnetic recording and reproducing devices (hereinafter referred to as ``home VTR'') have become popular.
In conjunction with improvements in magnetic tape and increased sensitivity of rotating heads, recording and reproducing densities have been further increased, and tape speeds, track pitches, etc. have been changed to, for example, those that can be recorded and reproduced for two hours in the past. Approximately 1/
Home VTRs with long recording and playback times of 6 hours have now been commercialized.
However, in home VTRs, where the tape running system is simplified to reduce costs, the high density described above is
It becomes difficult to follow the bending of the video track and stably maintain the required tracking accuracy, especially when playing back a magnetic tape recorded on another home VTR on another home VTR (so-called compatible playback). It is difficult to maintain stable accuracy, and currently high image quality cannot be obtained.

そこで、上記の高密度な記録再生に伴うトラツ
キング問題を解決し、更にはスローモーシヨン再
生、ステイル再生、フアーストモーシヨン再生等
の特殊再生(トリツクプレー)時のノイズバーを
除去する方法として、回転ヘツドをその回転面と
直交する平面上を変位させ、トラツク長手方向と
直交する方向(すなわちトラツクの幅方向)上に
回転ヘツドを変位させるヘツドムービング機構を
具備したホームVTRの開発が近年盛んに行なわ
れている。
Therefore, as a method to solve the above-mentioned tracking problem associated with high-density recording and playback, and also to eliminate noise bars during special playback (trick play) such as slow-motion playback, still playback, and fast-motion playback, we have developed a rotating head. In recent years, home VTRs have been actively developed that are equipped with a head moving mechanism that displaces the rotary head on a plane perpendicular to its rotating surface and displaces the rotary head in a direction perpendicular to the longitudinal direction of the track (that is, in the width direction of the track). ing.

かかるヘツドムービング機構を具備したホーム
VTRにおいては、トラツクの曲りに追従させ、
あるいは記録時とは異なるテープ走行速度として
行なう特殊再生時におけるヘツド走査軌跡をトラ
ツクに追従させるため、走査すべきトラツクと現
に磁気テープ上を走査中の回転ヘツドとの相対的
なずれ情報(トラツクずれ情報)を検出し、それ
に基づいてトラツキング誤差信号を生成して回転
ヘツドのトラツクずれを補正せしめるトラツキン
グサーボ回路を有しているが、上記トラツクずれ
情報を正確に検出することがトラツクずれの補正
にとつて極めて重要である。
A platform equipped with such a head moving mechanism
In VTR, it follows the curve of the track,
Alternatively, in order to make the track follow the head scanning locus during special playback, which is performed at a tape running speed different from that during recording, information on the relative shift between the track to be scanned and the rotating head currently scanning the magnetic tape (track shift It has a tracking servo circuit that detects the track deviation information) and generates a tracking error signal based on the tracking error signal to correct the tracking deviation of the rotary head.Accurately detecting the above tracking deviation information is the key to correcting the tracking deviation. It is extremely important for

しかして、従来、上記トラツクずれ情報を検出
する方法として、相隣るトラツクでは互いに異な
る周波数で記録されるように周波数が1本のトラ
ツク記録単位毎に切換えられる4種類のパイロツ
ト信号を各トラツク毎に連続的に記録し、再生時
は再生パイロツト信号を周波数弁別し、その再生
レベルよりトラツクずれ情報を検出するものがあ
つたが、再生系に4種類のパイロツト信号を夫々
周波数選択するためのフイルタ回路を必要とし、
広い帯域が必要であつた。
Conventionally, as a method for detecting the track deviation information, four types of pilot signals whose frequencies are switched for each track recording unit are sent to each track so that adjacent tracks are recorded at different frequencies. There is a system that records continuously on a track, and during playback, discriminates the frequency of the playback pilot signal and detects track deviation information from the playback level. requires a circuit,
A wide bandwidth was required.

一方、再生時に回転ヘツドを480Hz程度でトラ
ツクの幅方向へ振動させつつ、トラツクに周波数
変調波信号(FM信号)の形態で記録されている
情報信号の再生FMレベルの変動よりトラツクず
れを検出する方式も従来あつたが、この従来方式
は再生FMレベルの変動の影響が再生画像に現わ
れることもあり、また1トラツクピツチ以上のト
ラツクずれに対してはトラツクずれ情報が正確に
得られないという欠点を有していた。
On the other hand, during playback, the rotating head is vibrated in the width direction of the track at approximately 480 Hz, and track deviation is detected from fluctuations in the playback FM level of information signals recorded in the form of frequency modulated wave signals (FM signals) on the track. There is also a conventional method, but this conventional method has the disadvantage that the influence of fluctuations in the reproduced FM level may appear in the reproduced image, and that track deviation information cannot be obtained accurately for track deviations of one track pitch or more. had.

本発明は上記の諸欠点を除去したものであり、
以下図面と共にその各実施例につき説明する。
The present invention eliminates the above-mentioned drawbacks,
Each embodiment will be described below with reference to the drawings.

第1図は本発明方式の記録系の一実施例のブロ
ツク系統図を示す。同図中、入力端子1に入来し
た複合映像信号は2分岐され、一方は記録信号処
理回路2に供給され、所定周波数帯域のFM信号
とされ、他方は水平同期信号分離回路3に供給さ
れる。水平同期信号分離回路3により取り出され
た水平同期信号は、1/4分周器4により1/4分周さ れた後位相比較器5へ供給される。
FIG. 1 shows a block system diagram of an embodiment of a recording system according to the present invention. In the figure, a composite video signal that enters the input terminal 1 is branched into two, one of which is supplied to the recording signal processing circuit 2 and converted into an FM signal of a predetermined frequency band, and the other is supplied to the horizontal synchronization signal separation circuit 3. Ru. The horizontal synchronization signal extracted by the horizontal synchronization signal separation circuit 3 is frequency-divided by 1/4 by a 1/4 frequency divider 4 and then supplied to a phase comparator 5 .

位相比較器5の出力誤差電圧はループフイルタ
6を経て電圧制御発振器(VCO)7の出力発振
周波数を可変制御し、このVCO7の出力発振周
波数がカウンタ8により分周されて水平走査周波
数fHの1/4倍の周波数1/4fHとされて位相比較器5 に供給され、ここで1/4分周器4よりの周波数1/4 fHの信号と位相比較される。すなわち、位相比較
器5、ループフイルタ6、VCO7及びカウンタ
8は、夫々周知のフエーズ・ロツクド・ループ
(PLL)を構成しており、VCO7の出力発振周波
数はカウンタ8の分周比を1/Mとすると、fH/4・M となり、かつ、1/4分周器4の出力信号に同期し た信号となる。
The output error voltage of the phase comparator 5 passes through a loop filter 6 to variably control the output oscillation frequency of a voltage controlled oscillator (VCO) 7, and the output oscillation frequency of this VCO 7 is divided by a counter 8 to obtain the horizontal scanning frequency fH. The frequency is 1/4 times as high as 1/ 4fH , and is supplied to the phase comparator 5, where the phase is compared with the signal of frequency 1/ 4fH from the 1/4 frequency divider 4. That is, the phase comparator 5, loop filter 6, VCO 7, and counter 8 each constitute a well-known phase locked loop (PLL), and the output oscillation frequency of the VCO 7 is the frequency division ratio of the counter 8 divided by 1/M. Then, it becomes f H /4·M and becomes a signal synchronized with the output signal of the 1/4 frequency divider 4.

ここで、カウンタ8の分周比1/Mは制御回路1 0よりライン11を経て印加される制御信号に応
じて可変されるよう構成されており、制御回路1
0は入力端子9よりのドラムパルスに応じて回転
ヘツド13が1本のトラツクを磁気テープ14上
に形成する毎に異なる値の制御信号を切換えて出
力する。
Here, the frequency division ratio 1/M of the counter 8 is configured to be varied in accordance with a control signal applied from the control circuit 10 through the line 11.
0 switches and outputs a control signal of a different value each time the rotary head 13 forms one track on the magnetic tape 14 in response to a drum pulse from the input terminal 9.

これにより、例えばカウンタ8の分周比は1本
のトラツクを形成する毎に1/25、1/34、1/35、1
/26、 1/25、…というように4種類の分周比が順次巡回 的に切換えられていく。この結果、VCO7の出
力発振周波数は1本のトラツク記録単位毎に 25/4fH(=f1)、34/4fH(=f3)、35/4fH(=f4
)、26/4fH(= f2)という順序で切換えられることになる。この
VCO7の出力発振周波数は混合回路12に供給
され、ここで記録信号処理回路2よりのFM映像
信号と周波数分割多重された後、回転ヘツド13
により磁気テープ14上に記録される。
As a result, for example, the frequency division ratio of the counter 8 is 1/25, 1/34, 1/35, 1/25, 1/34, 1/35,
Four types of frequency division ratios are sequentially and cyclically switched such as /26, 1/25, and so on. As a result, the output oscillation frequency of the VCO 7 is 25/4f H (=f 1 ), 34/4f H (=f 3 ), 35/4f H (=f 4 ) for each track recording unit.
), 26/4f H (=f 2 ). this
The output oscillation frequency of the VCO 7 is supplied to the mixing circuit 12, where it is frequency division multiplexed with the FM video signal from the recording signal processing circuit 2, and then sent to the rotary head 13.
The data is recorded on the magnetic tape 14 by.

第2図は回転ヘツド13により記録形成された
磁気テープ14上のトラツクパターンを示し、磁
気テープ14の長手方向に対して傾斜したトラツ
クがt1、t2、t3、t4、t5、t6、…の順序で順次形成
される。ここで、トラツクt1、t2、t3、t4、t5、t6
にはFMされた複合映像信号と共に周波数f1、f3
f4、f2、f1、f3のパイロツト信号が夫々記録され
ている。
FIG. 2 shows a track pattern on the magnetic tape 14 recorded by the rotating head 13, and the tracks inclined with respect to the longitudinal direction of the magnetic tape 14 are t 1 , t 2 , t 3 , t 4 , t 5 , They are formed sequentially in the order of t 6 ,... Here, tracks t 1 , t 2 , t 3 , t 4 , t 5 , t 6
In addition to the FM composite video signal, the frequencies f 1 , f 3 ,
Pilot signals of f 4 , f 2 , f 1 and f 3 are recorded respectively.

本実施例は、パイロツト信号として fai=(2Ni−1)fx/2 (1) なる式を満足する任意の数i個の第1の周波数群
fa1〜faiから、互いに2fx以上離れた周波数のf1
f4を選定し、また fbj=(2Nj−1)fy/2(ただしfx≠fy) (2) なる式を満足する任意の数j個の第2の周波数群
fb1〜fbjから、上記周波数f1、f4との差が2fx以下
の周波数である周波数f2、f3を選定し、第1の周
波数群の周波数と第2の周波数群の周波数とを交
互に、かつ、極めて接近した周波数同士が相隣る
トラツクに記録されるように1トラツク記録単位
毎に切換えてf1、f3、f4、f2の順序で記録したも
のである(f2、f4、f3、f1の順序でもよい)。なお
(1)、(2)式中、Ni、Njは自然数であり、f1〜f4は例
えば である。ただし、パイロツト信号f1〜f4はFM映
像信号の帯域よりも低域にあり、fx=fH/2、fy=fH である。
In this embodiment, the first frequency group of an arbitrary number i that satisfies the formula f ai = (2N i −1) f x /2 (1) is used as a pilot signal.
From f a1 ~ f ai , f 1 of frequencies that are more than 2fx apart from each other,
Select f 4 and select an arbitrary number j of second frequency groups that satisfy the following formula: f bj = (2N j −1) f y /2 (where f x ≠ f y ) (2)
From f b1 to f bj , select frequencies f 2 and f 3 that have a difference of 2fx or less from the frequencies f 1 and f 4 , and combine the frequencies of the first frequency group and the frequencies of the second frequency group. They were recorded in the order of f 1 , f 3 , f 4 , f 2 by alternating and switching every track recording unit so that extremely close frequencies were recorded on adjacent tracks ( (The order may be f 2 , f 4 , f 3 , f 1 ). In addition
In formulas (1) and (2), N i and N j are natural numbers, and f 1 to f 4 are, for example, It is. However, the pilot signals f 1 to f 4 are in a lower band than the FM video signal band, and f x = f H /2 and f y = f H.

ところで、パイロツト信号としては、(1)式、(2)
式を満足するものに限らず、 fai′=Ni・fx (4) fbj′=Nj・fy (5) なる式を満足する各周波数群から上記と同様にし
て2組の周波数f1′、f4′、f2′、f3′をパイロツト信
号としてf1、f4、f2、f3の代りに用いてもよい。
ここで、f1′〜f4′は例えば である。ただし、(4)、(5)式中、fx=fH/2、fy=3/
4 fHである。
By the way, as pilot signals, equations (1) and (2)
In the same way as above, two sets of frequencies are calculated from each frequency group that satisfies the following expressions: f ai ′=N i・f x (4) f bj ′=N j・f y (5) Frequencies f 1 ', f 4 ', f 2 ', f 3 ' may be used as pilot signals instead of f 1 , f 4 , f 2 , f 3 .
Here, f 1 ′ to f 4 ′ are, for example It is. However, in formulas (4) and (5), f x = f H /2, f y = 3/
4 f H.

次に本発明方式の再生系の動作につき説明す
る。第3図は本発明方式の再生系の第1実施例の
ブロツク系統図を示す。同図中、第2図に示す如
きトラツクパターンを有する磁気テープ14より
回転ヘツド13により再生された信号は、前置増
幅器20を経て2分岐され、一方は再生信号処理
回路21に供給されFM復調等の所定の信号処理
が施されてもとの複合映像信号に再生され、他方
は可変遅延素子の一例としてのチヤージ・カツプ
ルド・デバイス(CCD)22に印加される。
Next, the operation of the reproduction system according to the present invention will be explained. FIG. 3 shows a block system diagram of a first embodiment of the regeneration system according to the present invention. In the figure, a signal reproduced by a rotary head 13 from a magnetic tape 14 having a track pattern as shown in FIG. The signal is then subjected to predetermined signal processing and reproduced into the original composite video signal, and the other signal is applied to a charge coupled device (CCD) 22, which is an example of a variable delay element.

再生信号処理回路21より取り出された再生複
合映像信号は水平同期信号分離回路23により水
平同期信号のみが分離抽出されて位相比較器24
に供給される。この位相比較器24はループフイ
ルタ25、VCO26、カウンタ27と共にPLL
を構成している。カウンタ27の分周比は制御回
路28よりの制御信号により回転ヘツド13の1
トラツク再生単位毎に交互に1/455と1/910に切換え られる。従つて、VCO26の出力発振周波数は、
回転ヘツド13の1トラツク再生単位毎に交互に
455fHと910fHとに切換えられる。
From the reproduced composite video signal taken out from the reproduced signal processing circuit 21, only the horizontal synchronizing signal is separated and extracted by the horizontal synchronizing signal separating circuit 23, and then sent to the phase comparator 24.
is supplied to This phase comparator 24 is connected to a PLL along with a loop filter 25, a VCO 26, and a counter 27.
It consists of The frequency division ratio of the counter 27 is set to 1 of the rotary head 13 by a control signal from the control circuit 28.
It is alternately switched between 1/455 and 1/910 for each track reproduction unit. Therefore, the output oscillation frequency of VCO26 is
Alternately for each track playback unit of the rotary head 13
Switchable between 455f H and 910f H.

VCO26の出力発振周波数455fH又は910fH
1/2分周器29により1/2分周された後CCD22 へクロツクパルスとして印加される。CCD22
は455段で構成されており、クロツクパルス周波
数が455/2fHのときには再生信号を2H(Hは水平走 査期間)遅延し、他方、クロツクパルス周波数が
910/2fHのときには再生信号をH遅延して出力す る。CCD22の出力遅延再生信号は加算器30
に供給され、ここで前置増幅器20よりの遅延さ
れていない再生信号と加算される。これにより、
CCD22、加算器30は遅延時間Tの遅延回路
と加算回路よりなる所謂くし形フイルタを構成
し、その周波数特性は第4図aにおいてCCD2
2の遅延時間Tが2Hのときには実線で示す如く
になり、遅延時間TがHのときには破線で示す如
くになる。
The output oscillation frequency 455f H or 910f H of the VCO 26 is divided by 1/2 by the 1/2 frequency divider 29 and then applied to the CCD 22 as a clock pulse. CCD22
consists of 455 stages, and when the clock pulse frequency is 455/2f H , the reproduced signal is delayed by 2H (H is the horizontal scanning period);
When 910/2f H , the reproduced signal is delayed by H and output. The output delayed reproduction signal of the CCD 22 is sent to the adder 30.
where it is added to the undelayed reproduced signal from preamplifier 20. This results in
The CCD 22 and the adder 30 constitute a so-called comb filter consisting of a delay circuit with a delay time T and an adder circuit, and its frequency characteristics are shown in FIG.
When the delay time T of 2 is 2H, it becomes as shown by a solid line, and when the delay time T is H, it becomes as shown by a broken line.

従つて、加算器30の出力信号中にはCCD2
2の遅延時間Tが2Hのときの1トラツク再生期
間中にはパイロツト信号f2、f3は含まれ得るが、
パイロツト信号f1、f4は阻止されて含まれること
はない。またCCD22の遅延時間TがHのとき
の1トラツク再生期間中にはパイロツト信号f1
f4は加算器30より取り出されるが、パイロツト
信号f2、f3は阻止される。
Therefore, in the output signal of the adder 30, CCD2
Pilot signals f 2 and f 3 may be included during one track playback period when the delay time T of 2 is 2H.
Pilot signals f 1 and f 4 are blocked and are not included. Also, during one track reproducing period when the delay time T of the CCD 22 is H, the pilot signal f 1 ,
f 4 is taken out by adder 30, but pilot signals f 2 and f 3 are blocked.

加算器30の出力信号は第4図bに曲線で示
す如く周波数f1、f2のパイロツト信号を通過させ
る特性を有する帯域フイルタ31と、同図bに曲
線で示す如く周波数f3、f4のパイロツト信号を
通過させる特性を有する帯域フイルタ32とに
夫々供給される。帯域フイルタ31の出力信号は
検波回路(図示せず)を経て切換スイツチ33の
固定端子33a及び切換スイツチ34の固定端子
34bに夫々供給され、他方、帯域フイルタ32
の出力信号は検波回路(図示せず)を経て切換ス
イツチ33の固定端子33b及び切換スイツチ3
4の固定端子34aに夫々供給される。切換スイ
ツチ33及び34は夫々連動して切換えられる。
The output signal of the adder 30 is passed through a bandpass filter 31 having a characteristic of passing the pilot signals of frequencies f 1 and f 2 as shown by the curve in FIG . and a bandpass filter 32 having a characteristic of passing the pilot signal. The output signal of the band filter 31 is supplied to the fixed terminal 33a of the changeover switch 33 and the fixed terminal 34b of the changeover switch 34 through a detection circuit (not shown), respectively.
The output signal passes through a detection circuit (not shown) to the fixed terminal 33b of the changeover switch 33 and the changeover switch 3.
4 fixed terminals 34a, respectively. The changeover switches 33 and 34 are switched in conjunction with each other.

また、切換スイツチ33,34は制御回路28
とカウンタ27で分周比が切換えられる周期つま
りドラムパルスの2倍の周期で切換制御されるよ
う構成されており、回転ヘツド13がパイロツト
信号f1とf3が記録されているトラツクを再生する
期間中は、固定端子33a,34a側に夫々接続
され、パイロツト信号f2とf4が記録されているト
ラツクを再生する期間中は、固定端子33b,3
4b側に夫々切換接続される。
In addition, the changeover switches 33 and 34 are connected to the control circuit 28.
The rotating head 13 reproduces the track on which the pilot signals f1 and f3 are recorded. During the period, the fixed terminals 33b and 34a are connected to the fixed terminals 33a and 34a, respectively, and during the period of reproducing the tracks on which the pilot signals f2 and f4 are recorded, the fixed terminals 33b and 34a are connected to the fixed terminals 33a and 34a, respectively.
4b side, respectively.

ところで、再生時、回転ヘツド13がパイロツ
ト信号f1が記録されているトラツクを再生してい
る期間は、隣接トラツクからは第2図よりわかる
ようにパイロツト信号f2及びf3が夫々クロストー
クとして再生される。この再生期間中、カウンタ
27の分周比は1/455とされ、切換スイツチ33及 び34は夫々固定端子33a,34aに接続され
る。この結果、この再生期間中は再生すべきトラ
ツクからのパイロツト信号f1はCCD22及び加算
器30よりなるくし形フイルタにより阻止され、
かつ、クロストークとして再生されたパイロツト
信号f2、f3が帯域フイルタ31及び32へ供給さ
れる。これにより、帯域フイルタ31よりクロス
トークとして再生されたパイロツト信号f2が取り
出され、切換スイツチ33を経て差動増幅器35
の正相入力端子に印加される。一方、帯域フイル
タ32からはクロストークとして再生されたパイ
ロツト信号f3が取り出され、更に切換スイツチ3
4を経て差動増幅器35の逆相入力端子に印加さ
れる。
By the way, during reproduction, during the period when the rotary head 13 is reproducing the track on which the pilot signal f 1 is recorded, the pilot signals f 2 and f 3 from the adjacent tracks are generated as crosstalk, respectively, as can be seen from FIG. will be played. During this reproduction period, the frequency division ratio of the counter 27 is set to 1/455, and the changeover switches 33 and 34 are connected to fixed terminals 33a and 34a, respectively. As a result, during this reproduction period, the pilot signal f 1 from the track to be reproduced is blocked by the comb filter consisting of the CCD 22 and the adder 30.
In addition, pilot signals f 2 and f 3 reproduced as crosstalk are supplied to band filters 31 and 32. As a result, the pilot signal f 2 regenerated as crosstalk is extracted from the bandpass filter 31 and passed through the changeover switch 33 to the differential amplifier 35.
is applied to the positive phase input terminal of On the other hand, the pilot signal f3 reproduced as crosstalk is taken out from the band filter 32, and is further output to the selector switch 3.
4 and is applied to the anti-phase input terminal of the differential amplifier 35.

ここで、いま回転ヘツド13が第2図中、上方
向にずれて走行した場合は、パイロツト信号f3
クロストークレベルがパイロツト信号f2のクロス
トークレベルに比し相対的に高くなるから、差動
増幅器35の出力トラツクずれ検出電圧はトラツ
クずれが無いときに比し低くなる。逆に、回転ヘ
ツド13が第2図中、下方向にずれて走行した場
合は、パイロツト信号f3のクロストークレベルが
パイロツト信号f2のクロストークレベルに比し相
対的に低くなるから、差動増幅器35の出力トラ
ツクずれ検出電圧はトラツクずれが無いときに比
し高くなる。
If the rotary head 13 now moves upward in FIG. 2, the crosstalk level of the pilot signal f3 will be relatively high compared to the crosstalk level of the pilot signal f2 . The output track deviation detection voltage of the differential amplifier 35 is lower than when there is no track deviation. Conversely, if the rotary head 13 moves downward in FIG. 2, the crosstalk level of the pilot signal f3 will be relatively low compared to the crosstalk level of the pilot signal f2 , so the difference The output track deviation detection voltage of the dynamic amplifier 35 is higher than when there is no track deviation.

次に回転ヘツド13がパイロツト信号f2がFM
映像信号と共に記録されているトラツクを再生す
る再生期間中は、カウンタ27は1/910の分周比と され、前記くし形フイルタにより再生すべきトラ
ツクからの再生パイロツト信号f2が阻止され、か
つ、隣接トラツクからクロストークとして再生さ
れるパイロツト信号f1、f4が波された後更に帯
域フイルタ31よりパイロツト信号f1が、また帯
域フイルタ32よりパイロツト信号f4が夫々波
される。またこのパイロツト信号f2の既記録トラ
ツク再生期間中は、切換スイツチ33,34は固
定端子33b,34b側に切換接続されるため、
クロストークとして再生され、かつ、帯域フイル
タ31,32より取り出されたパイロツト信号
f1、f4は差動増幅器35の逆相、正相の入力端子
に印加される。
Next, the rotary head 13 receives the pilot signal f2 from FM.
During the playback period in which the track recorded together with the video signal is played back, the counter 27 is set at a frequency division ratio of 1/910, and the playback pilot signal f2 from the track to be played is blocked by the comb filter, and , pilot signals f 1 and f 4 reproduced as crosstalk from adjacent tracks are waved, and then a pilot signal f 1 is waved from a band filter 31 and a pilot signal f 4 is waved from a band filter 32, respectively. Also, during the reproduction period of the recorded track of the pilot signal f2 , the changeover switches 33 and 34 are switched to the fixed terminals 33b and 34b.
Pilot signal reproduced as crosstalk and extracted from band filters 31 and 32
f 1 and f 4 are applied to the negative phase and positive phase input terminals of the differential amplifier 35.

従つて、この場合、回転ヘツド13が第2図
中、上方向にずれて再生が行なわれると、パイロ
ツト信号f1のクロストークレベルの方がパイロツ
ト信号f4のクロストークレベルよりも相対的に大
になり、よつて差動増幅器35より出力端子36
へ出力されるトラツクずれ検出電圧は、トラツク
ずれが無い時に比し低くなる。また逆に、回転ヘ
ツド13が第2図中、下方向にずれて再生が行な
われると、上記とは逆にトラツクずれ検出電圧は
トラツクずれが無い時に比し高くなる。
Therefore, in this case, if the rotary head 13 is shifted upward in FIG. 2 and reproduction is performed, the crosstalk level of the pilot signal f1 will be relatively higher than the crosstalk level of the pilot signal f4 . Therefore, the differential amplifier 35 output terminal 36
The track deviation detection voltage output to is lower than when there is no track deviation. Conversely, when the rotary head 13 is shifted downward in FIG. 2 and reproduction is performed, the track shift detection voltage becomes higher than when there is no track shift, contrary to the above.

そして次に第2図の例では回転ヘツド13によ
りパイロツト信号f4の既記録トラツクが再生され
るが、この再生期間中はカウンタ27の分周比は
1/455に切換えられ、かつ、切換スイツチ33,3 4も固定端子33b,34b側に切換接続され
る。これにより、上記の説明より明らかなように
帯域フイルタ31,32より隣接トラツクからク
ロストークとして再生されるパイロツト信号f2
f3は差動増幅器35の逆相、正相の入力端子に印
加される。従つてトラツクずれ検出電圧はトラツ
クずれが第2図中、上方向の時は低く、下方向の
時は高くなる。
Next, in the example of FIG. 2, the previously recorded track of the pilot signal f4 is reproduced by the rotary head 13, but during this reproduction period, the frequency division ratio of the counter 27 is switched to 1/455, and the changeover switch is switched to 1/455. 33 and 34 are also switched and connected to the fixed terminals 33b and 34b. As a result, as is clear from the above explanation, the pilot signals f 2 ,
f 3 is applied to the negative phase and positive phase input terminals of the differential amplifier 35. Therefore, the track deviation detection voltage is low when the track deviation is upward in FIG. 2, and high when it is downward.

同様に、パイロツト信号f3の既記録トラツク再
生期間中は、カウンタ27の分周比は(1/910)
に切換えられ、かつ、切換スイツチ33,34も
固定端子33a,34a側に切換接続される。こ
の結果、帯域フイルタ31,32より隣接トラツ
クからクロストークとして再生されるパイロツト
信号f4,f1は差動増幅器35の正相、逆相の入力
端子に印加される。従つて、トラツクずれ検出電
圧はトラツクずれが第2図中、上方向に発生した
時は低く、他方、下方向に発生した時は高くな
る。
Similarly, during the reproduction period of the recorded track of the pilot signal f3 , the frequency division ratio of the counter 27 is (1/910).
At the same time, the changeover switches 33 and 34 are also connected to the fixed terminals 33a and 34a. As a result, the pilot signals f 4 and f 1 reproduced as crosstalk from the adjacent tracks by the bandpass filters 31 and 32 are applied to the positive phase and negative phase input terminals of the differential amplifier 35. Therefore, the track deviation detection voltage is low when the track deviation occurs in the upward direction in FIG. 2, and becomes high when the track deviation occurs in the downward direction.

このようにして、帯域フイルタ31,32から
は再生すべきトラツクの両側の隣接トラツクから
クロストークとして再生されるパイロツト信号が
取り出され、回転ヘツド13が第2図中、上方向
にトラツクずれを生じて再生している時には、ト
ラツクずれ量に応じて低い値となり、他方、下方
向にトラツクずれを生じて再生している時にはト
ラツクずれ量に応じて高い値となるトラツクずれ
検出電圧が出力端子36より出力される。従つ
て、このトラツクずれ検出電圧に基づいてトラツ
クずれを補正することができることは明らかであ
る。
In this way, the pilot signals reproduced as crosstalk from the adjacent tracks on both sides of the track to be reproduced are extracted from the band filters 31 and 32, and the rotary head 13 causes the track to shift upward in FIG. The track deviation detection voltage is output from the output terminal 36 and has a low value depending on the amount of track deviation when the track is being played back, and a high value depending on the amount of track deviation when playing with a downward track deviation. It is output from Therefore, it is clear that the track deviation can be corrected based on this track deviation detection voltage.

なお、切換スイツチ33,34を制御する信号
は、図示しないがドラムパルスを1/2分周して作
るために、再生開始時には、切換スイツチ33,
34が、回転ヘツド13がパイロツト信号f1とf3
が記録されているトラツクを再生する期間中に、
固定端子33a,34a側に夫々接続され、パイ
ロツト信号f2とf4が記録されているトラツクを再
生する期間中に固定端子33b,34b側に夫々
接続されることもあり得る。しかし、このシーケ
ンスの場合には回転ヘツド13が少しでも上方向
にずれた場合には差動増幅器35の出力が低くな
り、さらに上方にずらすように制御され、結局2
トラツクピツチ分上にずれ、前記シーケンスと同
じになり安定する。また、下方向に少しでもずれ
た場合には差動増幅器35の出力が高くなり、さ
らに下方にずらすように制御され、結局2トラツ
クピツチ分下にずれ、前記のシーケンスと同じに
なり安定する。
Note that the signals that control the changeover switches 33 and 34 are generated by dividing the frequency of the drum pulse by 1/2 (not shown), so at the start of playback, the changeover switches 33 and
34, the rotary head 13 receives pilot signals f 1 and f 3
During the period when playing the recorded track,
They are connected to the fixed terminals 33a and 34a, respectively, and may be connected to the fixed terminals 33b and 34b, respectively, during the period of reproducing the track on which the pilot signals f2 and f4 are recorded. However, in the case of this sequence, if the rotary head 13 shifts upward even slightly, the output of the differential amplifier 35 becomes low, and the output is controlled to shift further upward, resulting in 2
The sequence shifts up by the track pitch and becomes stable, becoming the same as the above sequence. Furthermore, if there is even a slight shift downward, the output of the differential amplifier 35 becomes high, and control is performed to shift it further downward, eventually shifting downward by two track pitches, resulting in the same sequence as described above and stabilization.

第5図は本発明方式の再生系の第2実施例のブ
ロツク系統図を示す。本実施例は磁気テープ1
4′上の傾斜トラツクに、第2図にf1〜f4で示す
パイロツト信号の代りに、前記(4)〜(6)式と共に説
明したパイロツト信号f1′〜f4′が記録されている
時の再生系であり、第3図と同一部分には同一符
号を付し、その説明を省略する。
FIG. 5 shows a block system diagram of a second embodiment of the regeneration system according to the present invention. In this embodiment, the magnetic tape 1
On the inclined track above 4', instead of the pilot signals f 1 to f 4 shown in FIG. The same parts as in FIG. 3 are given the same reference numerals and their explanations will be omitted.

第5図において、PLLを構成するカウンタ3
8は制御回路37の出力制御信号により、回転ヘ
ツド13がパイロツト信号f2′、又はf3′の既記録
トラツクを再生する期間は分周比が1/1365とされ て1/4分周器43よりクロツクパルスが印加され るCCD22の遅延時間を4/3Hとし、他方、パイ ロツト信号f1′又はf4′の既記録トラツク再生期間
は分周比が1/910とされてCCD22の遅延時間を 2Hとする。CCD22の出力遅延信号は加算器4
0において、反転増幅器39により反転増幅され
た再生信号と加算される。すなわち、前置増幅器
20よりの再生信号は、CCD22により遅延さ
れた再生信号と減算される。このCCD22、反
転増幅器39及び加算器40は夫々くし形フイル
タを構成し、CCD22の遅延時間が2Hのときに
は第6図aに実線で示す周波数特性を示し、遅延
時間が4/3Hのときには同図aに破線で示す周波 数特性を示す。
In Fig. 5, counter 3 that constitutes the PLL
8 is a 1/4 frequency divider with a frequency division ratio of 1/1365 during the period in which the rotary head 13 reproduces the recorded track of the pilot signal f 2 ' or f 3 ' according to the output control signal of the control circuit 37. The delay time of the CCD 22 to which the clock pulse is applied from 43 is set to 4/3H, and on the other hand, during the reproduction period of the recorded track of the pilot signal f 1 ' or f 4 ', the frequency division ratio is set to 1/910 and the delay time of the CCD 22 is set to 4/3H. It will be 2H. The output delay signal of CCD22 is output by adder 4
0, it is added to the reproduced signal that has been inverted and amplified by the inverting amplifier 39. That is, the reproduced signal from the preamplifier 20 is subtracted from the reproduced signal delayed by the CCD 22. The CCD 22, the inverting amplifier 39, and the adder 40 each constitute a comb filter, and when the delay time of the CCD 22 is 2H, the frequency characteristics shown by the solid line in FIG. The frequency characteristics indicated by broken lines are shown in a.

従つて、回転ヘツド13がパイロツト信号
f1′又はf4′の既記録トラツクを再生する期間は、
上記くし形フイルタにより(6)式に示すf2′及び
f3′が波され、かつ、f1′,f4′が阻止される。他
方、パイロツト信号f2′又はf3′の既記録トラツク
再生期間は、f1′及びf4′が波され、かつ、f2′,
f3′が阻止される。加算器40より取り出された
信号は帯域フイルタ41及び42に夫々供給され
る。
Therefore, the rotary head 13 receives the pilot signal.
The period for playing back the recorded track of f 1 ′ or f 4 ′ is as follows:
With the above comb filter, f 2 ′ and
f 3 ′ is waved, and f 1 ′ and f 4 ′ are blocked. On the other hand, during the reproduction period of the recorded track of the pilot signal f 2 ′ or f 3 ′, f 1 ′ and f 4 ′ are waved, and f 2 ′,
f 3 ′ is blocked. The signals extracted from adder 40 are supplied to bandpass filters 41 and 42, respectively.

帯域フイルタ41は第6図bに曲線で示す如
くf1′,f2′の周波数を通過させる周波数特性を有
し、他方、帯域フイルタ42は同図bに曲線で
示す如くf3′,f4′の周波数を通過させる周波数特
性を有する。従つて、帯域フイルタ41,42に
は、上記のくし形フイルタにより取り出された回
転ヘツド13の再生トラツクの両側のトラツクか
ら夫々クロストークとして再生されるパイロツト
信号が供給され、これらを各々周波数選択して出
力することになる。
The bandpass filter 41 has frequency characteristics that pass the frequencies f 1 ' and f 2 ' as shown by the curve in FIG. It has frequency characteristics that allow the 4 ' frequency to pass through. Therefore, the band filters 41 and 42 are supplied with pilot signals reproduced as crosstalk from the tracks on both sides of the reproduced track of the rotary head 13 extracted by the above-mentioned comb filter, and each of these is frequency-selected. will be output.

帯域フイルタ41,42の出力信号は切換スイ
ツチ33,34を経て差動増幅器35に供給さ
れ、第3図と同様にしてトラツクずれ検出電圧が
出力端子36より出力される。
The output signals of the bandpass filters 41 and 42 are supplied to a differential amplifier 35 via changeover switches 33 and 34, and a track deviation detection voltage is outputted from an output terminal 36 in the same manner as in FIG.

なお、パイロツト信号周波数を、重畳記録する
複合映像信号と一定の関係の周波数に選定した場
合は、CCDやバケツト・ブリゲード・デバイス
(BBD)等の可変遅延素子により、再生パイロツ
ト信号にワウ・フラツタ等の変動分が含まれて
も、容易にパイロツト信号を判別することができ
るものである。また、ワウ・フラツタ等の時間軸
変動分を無視し得る場合には、パイロツト信号周
波数を複合映像信号と一定の周波数関係に選定す
る必要がなく、このような場合にはCCD、BBD
等の可変遅延素子によらず、安価なガラス遅延素
子等の遅延時間固定の素子を切換え使用すること
もできる。
Note that if the pilot signal frequency is selected to have a certain relationship with the composite video signal to be superimposed and recorded, a variable delay element such as a CCD or bucket brigade device (BBD) will cause wow, flutter, etc. to occur in the reproduced pilot signal. The pilot signal can be easily distinguished even if it contains a variation. Furthermore, if time axis fluctuations such as wow and flutter can be ignored, there is no need to select the pilot signal frequency to have a constant frequency relationship with the composite video signal.
Instead of using a variable delay element such as the above, it is also possible to switch and use an element with a fixed delay time such as an inexpensive glass delay element.

上述の如く、本発明になるパイロツト信号記録
再生方式は、 fai=Ki・fx (ただし、Kiは任意のi個の自然数をNiとした
ときNi−1/2又はNiで、fxは所定の周波数) なる式を満足するi個の周波数よりなる第1の周
波数群から、互いに2fx以上離れた周波数の第1
の周波数と第2の周波数を夫々選定し、また fbj=Kj・fy (ただし、kjは任意のj個の自然数をNjとした
ときNj−(1/2)又はNjで、fy≠fx) なる式を満足するj個の周波数よりなる第2の周
波数群から、上記第1の周波数との差が2fx以下
の周波数である第3の周波数と上記第2の周波数
との差が2fx以下の周波数である第4の周波数を
夫々選定し、該第1乃至第4の周波数をパイロツ
ト信号として情報信号に周波数分割多重して記録
媒体上1トラツク単位毎に順次第1、第4、第2
及び第3の順序(又はこれとは逆の順序)で切換
えて1トラツク全体に亘つて記録し、再生時は再
生信号中にクロストークとして含まれる再生すべ
きトラツクの両側のトラツクに記録されている互
いに異なる周波数のパイロツト信号を1トラツク
再生期間毎に遅延時間を切換えられる遅延回路を
含む可変フイルタ回路により周波数選択し、これ
ら両パイロツト信号のレベル差よりトラツクずれ
情報を得るよう構成したため、第1及び第3、第
2及び第4の各周波数は極めて接近しているか
ら、弁別分離に必要な周波数帯域幅は2周波分を
少し越える程度であり、比較的狭帯域で4種類の
パイロツト信号の記録再生ができ、周波数fx,fy
を水平走査周波数に関連した値にした場合は、可
変フイルタ回路を用いてワウ・フラツタ等の変動
分が含まれていても容易にパイロツト信号を判別
でき、上記パイロツト信号を情報信号の記録周波
数帯域よりも低域の周波数に選定したため、アジ
マス記録再生方式の磁気記録再生装置においても
隣接トラツクのパイロツト信号を効率良くクロス
トークとして再生できる等の特長を有するもので
ある。
As mentioned above, the pilot signal recording/reproducing method according to the present invention is f ai = K i ·f x (where K i is N i −1/2 or N i where N i is any i natural number. (where f x is a predetermined frequency) From the first frequency group consisting of i frequencies that satisfy the formula,
and the second frequency, respectively, and f bj = K j・f y (where, k j is N j −(1/2) or N j when any j natural numbers are N j From the second frequency group consisting of j frequencies satisfying the formula f y ≠ fx), a third frequency whose difference from the first frequency is 2fx or less and the second frequency The first to fourth frequencies are frequency-division multiplexed to the information signal as pilot signals, and the information signal is sequentially divided into one track unit at a time on the recording medium. , 4th, 2nd
and the third order (or the reverse order) to record the entire track, and during playback, the tracks on both sides of the track to be played that are included as crosstalk in the playback signal are recorded. The frequency of the pilot signals having different frequencies is selected by a variable filter circuit including a delay circuit whose delay time can be changed every track reproduction period, and the track deviation information is obtained from the level difference between these two pilot signals. Since the third, second, and fourth frequencies are very close to each other, the frequency bandwidth required for discrimination and separation is just over two frequencies, and the four types of pilot signals can be separated in a relatively narrow band. Recording and playback possible, frequency f x , f y
If is set to a value related to the horizontal scanning frequency, the pilot signal can be easily distinguished using a variable filter circuit even if fluctuations such as wow and flutter are included, and the pilot signal can be set to a value related to the recording frequency band of the information signal. Since the frequency is selected to be lower than that of the azimuth recording/reproducing method, the pilot signal of the adjacent track can be efficiently reproduced as crosstalk even in an azimuth recording/reproducing type magnetic recording/reproducing apparatus.

【図面の簡単な説明】[Brief explanation of the drawing]

第1図は本発明方式の記録系の一実施例を示す
ブロツク系統図、第2図は本発明方式により記録
再生される磁気テープ上のトラツクパターンの一
例を示す図、第3図は本発明方式の再生系の第1
実施例を示すブロツク系統図、第4図a,bは
夫々第3図の各部の周波数特性を示す図、第5図
は本発明方式の再生系の第2実施例を示すブロツ
ク系統図、第6図a,bは夫々第5図の各部の周
波数特性を示す図である。 1…複合映像信号入力端子、3,23…水平同
期信号分離回路、8,27,38…カウンタ、9
…ドラムパルス入力端子、14…磁気テープ、2
2…チヤージ・カツプルド・デバイス(CCD)、
30,40…加算器、31,32,41,42…
帯域フイルタ、33,34…切換スイツチ、35
…差動増幅器、39…反転増幅器。
FIG. 1 is a block system diagram showing an embodiment of a recording system according to the present invention, FIG. 2 is a diagram showing an example of a track pattern on a magnetic tape recorded and reproduced according to the present invention, and FIG. 3 is a diagram showing an example of a track pattern according to the present invention. The first method of reproduction system
4a and 4b are diagrams showing the frequency characteristics of each part of FIG. 3, respectively. FIG. 5 is a block system diagram showing a second embodiment of the reproduction system of the present invention. 6a and 6b are diagrams showing the frequency characteristics of each part in FIG. 5, respectively. 1...Composite video signal input terminal, 3, 23...Horizontal synchronization signal separation circuit, 8, 27, 38...Counter, 9
...Drum pulse input terminal, 14...Magnetic tape, 2
2...Charge coupled device (CCD),
30, 40...Adder, 31, 32, 41, 42...
Band filter, 33, 34...Switch switch, 35
...Differential amplifier, 39...Inverting amplifier.

Claims (1)

【特許請求の範囲】 1 fai=Ki・fx(ただし、Kiは任意のi個の自然
数をNiとしたときNi−(1/2)又はNiで、fxは
所定の周波数)なる式を連続するi個の周波数よ
りなる第1の周波数群から互いに2fx以上離れた
周波数の第1の周波数と第2の周波数を夫々選定
し、また fbj=Kj・fy (ただし、Kjは任意のj個の自然数をNjとした
ときNj−(1/2)又はNjで、fy≠fx) なる式を満足するj個の周波数よりなる第2の周
波数群から、上記第1の周波数との差が2fx以下
の周波数である第3の周波数と上記第2の周波数
との差が2fx以下の周波数である第4の周波数を
夫々選定し、該第1乃至第4の周波数をパイロツ
ト信号として情報信号に周波数分割多重して記録
媒体上1トラツク単位毎に順次第1、第4、第2
及び第3の順序(又はこれとは逆の順序)で切換
えて1トラツク全体に亘つて記録し、再生時は再
生信号中にクロストークとして含まれる再生すべ
きトラツクの両側のトラツクに記録されている互
いに異なる周波数のパイロツト信号を1トラツク
再生期間毎に遅延時間を切換えられる遅延回路を
含む可変フイルタ回路により周波数選択し、これ
ら両パイロツト信号のレベル差よりトラツクずれ
情報を得るよう構成したことを特徴とするパイロ
ツト信号記録再生方式。 2 該情報信号は複合映像信号とし、該周波数
fx、fYは水平走査周波数に関連した値としたこと
を特徴とする特許請求の範囲第1項記載のパイロ
ツト信号記録再生方式。 3 該第1乃至第4の周波数は、該情報信号記録
周波数帯域よりも低域の周波数に選定したことを
特徴とする特許請求の範囲第1項又は第2項記載
のパイロツト信号記録再生方式。
[Claims] 1 f ai = K i fx (where K i is N i -(1/2) or N i when any i natural numbers are N i , and fx is a predetermined frequency ) from the first frequency group consisting of i consecutive frequencies, select the first frequency and the second frequency that are separated from each other by 2fx or more, and f bj = K j・f y (however, , K j is N j - (1/2) or N j where N j is any j natural number, and the second frequency group is made up of j frequencies that satisfy the formula f y ≠ fx) , a third frequency whose difference from the first frequency is 2fx or less and a fourth frequency whose difference from the second frequency is 2fx or less are selected, respectively. The fourth frequency is used as a pilot signal and is frequency division multiplexed onto the information signal to sequentially transmit the first, fourth, and second frequencies on the recording medium in units of one track.
and the third order (or the reverse order) to record the entire track, and during playback, the tracks on both sides of the track to be played that are included as crosstalk in the playback signal are recorded. The frequency of the pilot signals having different frequencies is selected by a variable filter circuit including a delay circuit that can change the delay time for each track reproduction period, and track deviation information is obtained from the level difference between these two pilot signals. A pilot signal recording and reproducing method. 2. The information signal shall be a composite video signal, and the frequency
2. The pilot signal recording and reproducing method according to claim 1, wherein fx and fY are values related to a horizontal scanning frequency. 3. The pilot signal recording and reproducing method according to claim 1 or 2, wherein the first to fourth frequencies are selected to be frequencies lower than the information signal recording frequency band.
JP55139363A 1980-10-07 1980-10-07 Pilot signal recording and reproducing system Granted JPS5764327A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
JP55139363A JPS5764327A (en) 1980-10-07 1980-10-07 Pilot signal recording and reproducing system
US06/308,666 US4414586A (en) 1980-10-07 1981-10-05 Pilot signal recording and reproducing system
DE3139810A DE3139810C2 (en) 1980-10-07 1981-10-07 Control signal recording and playback system for video tape recorders

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP55139363A JPS5764327A (en) 1980-10-07 1980-10-07 Pilot signal recording and reproducing system

Publications (2)

Publication Number Publication Date
JPS5764327A JPS5764327A (en) 1982-04-19
JPS6321975B2 true JPS6321975B2 (en) 1988-05-10

Family

ID=15243580

Family Applications (1)

Application Number Title Priority Date Filing Date
JP55139363A Granted JPS5764327A (en) 1980-10-07 1980-10-07 Pilot signal recording and reproducing system

Country Status (1)

Country Link
JP (1) JPS5764327A (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58194480A (en) * 1982-05-07 1983-11-12 Matsushita Electric Ind Co Ltd Magnetic video recording and reproducing device
JPS5940784A (en) * 1982-08-31 1984-03-06 Sony Corp Still picture reproducer
JPS59117877A (en) * 1982-12-24 1984-07-07 Matsushita Electric Ind Co Ltd Tracking control system of magnetic picture recording and reproducing device
JPH0664786B2 (en) * 1984-01-30 1994-08-22 キヤノン株式会社 Information signal reproducing device

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5396655A (en) * 1977-02-03 1978-08-24 Marukon Denshi Kk Pll synthesizer
JPS53127255A (en) * 1977-04-13 1978-11-07 Torio Kk Phase lock loop circuit

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS5396655A (en) * 1977-02-03 1978-08-24 Marukon Denshi Kk Pll synthesizer
JPS53127255A (en) * 1977-04-13 1978-11-07 Torio Kk Phase lock loop circuit

Also Published As

Publication number Publication date
JPS5764327A (en) 1982-04-19

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