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pick-up relative to the disc, the tracking error signal

OPTICAL DISC TRACKING SYSTEM WITH tends to accompany a steady drift which will bring

SWITCHING OF TRACKING ERROR SIGNALS AT about a continuing shift in tracking. Accordingly, in the

BOUNDARY BETWEEN TRACK GUIDE AND event that the pick-up has inclined relative to the disc,

TRACK ADDRESS 5 the pattern of diffraction occurring at the guide groove

region and that at the address information region differ

BACKGROUND OF THE INVENTION from each other and> as a result thereof( the amount of

1. (Field of Technology) tracking shift necessarily deviates to such an extent as to The present invention relates to a tracking system for result in a disturbed tracking at the boundary. FIGS.

an optical memory device of a type wherein any of the 10 12(a) to 12(c) and FIGS. 13(a) to 13(c) are schematic

information recording, reproduction and erasing can be representations illustrative of the change in tracking

carried out by radiating a laser beam to a memory me- error signal occurring during the tracking at the bound

dium. ary according to these two methods, respectively.

2. (Description of the Prior Art) In these figures, the servo region is considered to be Optical memory devices have recently drawn the 15 sufficiently lower than the pit reproducing frequency

attention of people as a high density, high capacity and> therefore, an output of the detector during the

memory device. The reason that an optical memory tracking at the address information region is shown as

device is of high density and high capacity is because an a e yalue FIG 12 ^ where {he difference

the size of each bit which represents a unit of informa- ifl mnt of beam reflected fa taken M a tracki efror

twnstoragecanbereducedtoadiameterofaboutl^m. 20 &. 13 applies where the difference in

This, in turn, however, imposes some limitations on the ° . . , . . c , .. „ ... ,

. . j • »/ -t- H ■ j f output from detectors for detecting two split beam

optical memory device. More specifically, m order for v . , . ,. ° . * .

information to be recorded on, or reproduced from, a 'W*nts ,s taken as the tracking error signal.

predetermined location, the light beam is required to be SUMMARY OF THE INVENTION

accurately positioned. 25 ,. , . . , . ,

Because of the foregoing, when using a disc capable Accordingly, the present invention has been devised

of recording information simultaneously with erasure of t0 substantially eliminate the above described problems

previously recorded information, it is a general practice and nas for lts essential object to provide a tracking

for the disc substrate to be permanently provided with system wherein a relatively easy signal processing

beam guide tracks or address information. 30 means is employed to enable tracking to be performed

The guide tracks generally have a shape as shown in in a stabilized manner, even to discontinuous guide

FIG. 10 of the accompanying drawings and are in the grooves, with no need to take special measures for any

form of grooves of a depth generally equal to the wave- disc substrate.

... ... » **** DBSCRtPTION OF THE DRAWNGS

reproduction and erasing is earned out while the light This and other objects and features of the present

beam scans the tracks of the disc guided along these invention will become clear from the following descrip

guide grooves. tion taken in conjunction with preferred embodiments

As a means for sensing a tracking signal from the thereof with reference to the accompanying drawings,

guide grooves, two methods are well-known; a Twin 40 jn which:

Spot method (a three-beam method) such as generally piG. 1 is a schematic diagram showing an optical

used in association with VD (video disc) and CD (com- head for a magneto-optic disc according to one embodi

pact disc) and a push-pull method such as generally ment of the present invention;

used in association with an optically writeable disc. The FIG 2 is a diagram sh0wing an electric circuit formTwin Spot method and the push-pull method are illus- 45 a detecting means for detecting a tracking error trated respectively m FIGS. 12 and 13 of the accompa- signal

nyj^ drawin|s- FIG. 3 is a circuit block diagram showing the circuit

The Twin Spot method has an advantage in that a of {he detectinmeans.

stable tracking performance can be achieved even pIG 4 { b). ^ showi waveforms of si als

though a pick up ,s inclined relative to the optical disc 50 \ ^ *

substrate. However, it has a problem in that, when a JU,-* = • ii i_- i

* i,- u _ u J u * -j FIG. 5 is a schematic diagram showing an optical

tracking beam scans a boundary between a guide , , , . , ,. ^ ®. . ^ ,..e f

groove region G and an address information region A head. f°r an °Ptlcal dlsc to which a tracking system is

constituted by a plurality of pits as shown in FIG. 12(a), aPPhed accordlng t0 a second embodiment of the pres

the tracking tends to be disturbed because of the differ- 55 en* invention;

ence between a diffraction efficiency on the leading FIG- 618 a schematic diagram showing a relationship

beam Bi and that on the trailing beam B2. It is to be between the respective positions of laser beam spots

noted that reference character R used in FIG. 12(b) incident on the optical disc, the arrangement of detect

represents recorded bits. m§ elements of a photo-detector and the respective

On the other hand, although the push-pull method is 60 positions of the laser beam spots reflected toward the

generally free from the above mentioned problem in- detecting elements;

herent in the Twin Spot method because of the tracking KG- 7 is a circuit block diagram showing a circuit performed by a single beam B4 as shown in FIG. 13(a), used to effect a processing necessary to produce a feedit has a problem in that, because the position of the light back control signal;

beam which has been reflected towards a detector D 65 FIGS. 8(a,b) are charts showing waveforms of sig

shown in FIG. 13(6) tends to become displaced relative nals;

thereto in the event of a shift in position of a lens as a FIG. 9 is a diagram similar to FIG. 7 showing a modiresult of tracking or in the event of inclination of the fied form of the circuit;

3

FIGS. W(a,b,c) are charts showing waveforms of signals;

FIG. 11 is a perspective view of a portion of a disc substrate;

FIGS. \2{a,b,c) are plan views of a portion of the disc 5 substrate onto which the laser beams are projected;

FIG. 13(a) is a plan view of a portion of the disc substrate onto which the laser beams are projected;

FIG. 13(6) is a schematic diagram showing the detector on which the beam spot is reflected; and 10

FIG. 13(c) is a diagram showing waveforms of the signals.

DETAILED DESCRIPTION OF THE

EMBODIMENTS 15

FIGS. 1 and 2 illustrate the structure of an optical head for a magneto-optic disc and a circuit forming a detecting means for detecting a tracking error signal outputted form the optical head, respectively.

Referring first to FIG. 1, reference numeral 1 repre- 20 sents a magneto-optic disc comprising a disc substrate which contains guide grooves and address information and is coated with a magnetizable layer having an anisotropy of magnetism in a vertical direction. A laser beam produced from a semiconductor laser device 2 25 travels through a collimator lens 3 and then through a shaping prism 4 by which the elliptical cross-sectional representation of the laser beam is transformed into a generally circular shape. Reference numeral 5 represents a diffraction grating for splitting the laser beam, 30 diffracted light of a spectral degree of 0 and ± 1 being utilized. A polarizing beam splitter 6 is disposed between the diffraction grating 5 and an objective lens 8 for projecting a tiny spot of laser beam onto the magnetizable layer of the magneto-optic disc after having been 35 deflected 90° by a total reflecting mirror 7. This polarizing beam splitter 6 serves to improve the polarization ratio of the incoming light and to further rotate the plane of polarization of the light, reflected from the disc, for generally increasing the angle of magneto-op- 40 tic rotation. This beam splitter 6 also serves to guide a portion of the laser beam toward photo-detectors 11,12 and 17 as will be described later.

The objective lens 8 referred to above is in practice driven by a servo control circuit (not shown) so that the 45 size and position of the light spot projected onto the information tracks of the magnetizable layer of the disc can be adjusted. Reference numeral 9 represents a polarizing beam splitter having, as is the case with the beam splitter 6, a function of increasing the angle of 50 magneto-optic rotation with respect to the reflected light. Reference numeral 10 represents a spot lens for projecting the information light, reflected from the beam splitter 9, onto the photo-detectors 11 and 12 in a predetermined spot size. A half wavelength plate 13 is 55 positioned between the beam splitter 9 and the spot lens 10 for rotating the plane of the polarization of the information light in a direction intermediate between the S-axis and P-axis of a polarizing beam splitter 14 which acts as an analyzer. Reference numeral 15 represents a 60 spot lens, and reference numeral 16 represents a cylindrical lens so disposed as to have its focal line inclined 45° relative to the direction of connection of the guide grooves of the magneto-optic disc 1.

Positioned on one side of the cylindrical lens 16 oppo- 65 site to a spot lens 15 is the photo-detector 17 of the composite element type which includes six photo-detector elements A to F that are arranged in a pattern as

4

shown in FIG. 2. By the cumulative effects of the spot lens 15 and the cylindrical lens 16, both the change in relative distance between the magnetizable layer of the magneto-optic disc 1 and the objective lens 8, and the deviation of position of the light spot between the magnetizeable layer and the information track (guide grooves) can be detected. A method of detecting these servo signals is similar to that used in any of the astigmatism method, the three-beam method and the push-pull method, all generally used in association with the optical disc.

FIG. 2 illustrates the relationship in position between the photo-detector 17 of the composite element type and the reflected information light from the magnetooptic disc 1, and also a detecting means. Based on respective outputs SA, SB, SC and SD of four light receiving elements A, B, C and D positioned centrally of the detecting means 17, a focusing error signal Fgand a main beam tracking error signal Teo can be obtained from the following equations.

Fe=(sa+sq-(sb+sd)
Tm=(SC+SD)-(.SA+SB)

Also, based on respective outputs of light receiving elements E and F positioned on respective sides of the four light receiving elements A, B, C and D, a tracking error signal Tgi resulting from two auxiliary beams can be obtained from the following equation.

TEl =se-sf

Of these error signals, the focusing error signal F£ is used to control the drive of the objective lens 8 in a direction parallel to the optical axis which is effected by the servo control circuit and a drive device.

On the other hand, the main beam tracking error signal Teo and the tracking error signal Tei resulting from the two auxiliary beams are, after having been processed by some processes as will be described later, used to control the drive of the object lens 8 in a direction transverse to the track which is effected by the servo control circuit and the drive device.

Hereinafter, the processes necessary to effect the tracking by the use of the above-mentioned two tracking error signals will be described.

FIG. 3 is a circuit block diagram used to explain the first process. Reference numeral 18 represents a low pass filter unit for obtaining a low frequency component of the main beam tracking error signal T^o- The low frequency component filtered through the low pass filter unit 18 is fed to a sample-and-hold circuit 19 for sampling and holding the output from the filter unit 18 in synchronism with a timing signal as will be described later. Reference numeral 20 represents a differential circuit for outputting a difference signal indicative of the difference between the output from the sample-andhold circuit 19 and the main beam tracking error signal Ted, said difference signal being in turn fed to a switching circuit 21 which is operable to switch between the tracking error signal Tgi and the tracking error signal output from the differential circuit 20 in synchronism with the timing signal. The switching operation of the switching circuit 21 is performed by the utilization of timing signal, the waveform of which is shown by (a) in FIG. 4, in such a way that, at regions other than the address regions and the boundary regions, tracking can

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