Optical track sensing device

The present invention relates to an optical track sensing device, and in particular to an optical sensor for detecting optical tracking information on a magnetic floppy disk.

A high density floppy disk drive has been developed to store 120 megabytes of data on a 3.5" floppy disk. This high capacity floppy disk uses a special floppy disk with optical tracks recorded on one of its surfaces to allow the magnetic recording head to store information with closer track spacing. An optical track is recorded between every two magnetic tracks to provide more precise positioning information than can be achieved using the magnetic data alone. This allows the magnetic tracks to be placed closer together. In order to place the magnetic head precisely with respect to the optical tracks, an optical sensing device is used to detect the error between the magnetic head and the optical track. A prior art sensing device was described in a paper by S.W. Farnsworth, S.D. Wilson and B. Cohen entitled "Diffractive Optical System for Tracking on Floptical Disk", <u style="single">Optical Instrument</u>, SPIE Vol. 1690, pp.72-79, 1992.

Fig. 1 shows this prior art track sensing device. A semiconductor laser source 11 is imaged by a lens 13 and a rooftop mirror 14 to the floppy disk 15. A diffractive optical element 12 is used to divide the laser beam into many beams. While some beams are reflected upwards towards the floppy disk, others are reflected downwards by the lower half of the rooftop mirror to an encoder 16. The encoder provides tracking information to the floppy disk drive when a low density floppy disk without pre-recorded tracks is inserted into the disk drive. The encoder is a strip of optical tracks along the inside housing of the floppy disk drive which allows the position of the magnetic head to be determined optically, even though no optical tracks are on the low density floppy disk itself. The optical sensor is mounted on the magnetic head itself, and a hole is provided through the arm supporting the magnetic head for the optical path. This special optical track sensor permits this high density floppy disk drive to be backward compatible with the low density floppy disks. The returned beams from the floppy disk and the encoder are again reflected by the rooftop mirror 14 and are projected by a lens 17 to a multiple element detector 18.

The detector typically has six elements arranged in two rows. A first row of three elements is used to detect the tracking information from the floppy disk, while the second row is used to detect the encoder on the floppy disk drive housing. A double-slit optical element is used to provide an interference pattern, with the spacing of the interference lobes matching the spacing of the optical tracks. In this way, multiple tracks can be detected at once. Thus, each of the six elements of the detector should see five separate images corresponding to five tracks. The intensity of the received signal will be low, indicating a tracking error, if one or more beams is missing. Thus, the optical sensor splits the laser beam in two, for the floppy disk and the encoder on the housing. Next, each of the two beams are split into three to provide beams which can be detected by the three optical elements in each row of the detector. Finally, each of the six beams is split into five lobes to enable detection of each of five optical tracks.

One of the characteristics of this prior art optical track sensor is that the optical axis of lens 12 and the optical axis of the lens 17 subtend a small angle with respect to the mechanical axis. Consequently, the laser beams produced by the diffractive optical element 12 are not perpendicular to the surface of the floppy disk or the encoder. As a result, the lateral position of the beams on the floppy disk will change when the floppy disk moves up and down with respect to the image plane of the lens 13. Because of the multiple beams and lobes used, even a small variation in up and down movement of a floppy disk can affect the accuracy of the optical tracking.

EP-A-0,311,859 discloses a disk apparatus with a head carriage assembly employing optical heads each of which comprise a transmissive optical detector including a light source and a multi-element detector mounted on the opposite side of a disk. A collimating lens is employed between the light source and detector and the pitch of the detector is an integral multiple of the pitch of an optical grating on the disk. The desired period of the fringe pattern of the detector is achieved in part through the use of the collimating lens.

According to the present invention, there is provided a positional sensor for detecting the position of a moving medium, in accordance with claim 1.

In a preferred embodiment, the invention provides an optical sensor consisting of a nearly monochromatic point source such as a light emitting diode (LED) or a vertical cavity surface emitting laser (VCSEL) which is mounted on a multiple element detector. When this sensor is placed near a moving object with a reflective periodic pattern on its surface, it can produce a signal which can be used to control the position of the object. Unlike other sensors which often use lenses to project the light emitted by the light source onto the object and collect the light reflected from the object and project them onto a photodetector, this new sensor performs the tasks of object illumination and light collection without the use of any optical component.

It is well known that when a periodic pattern is illuminated by a nearly monochromatic point source of light, images of the periodic structure can be formed at certain distance from the object without the aid of any optical components. This phenomenon is called self-imaging and is described in a scientific article by Olof Bryngdahl ("Image Formation Using Self Imaging Technique", <u style="single">J. Opt. Soc. Am.,</u> Vol. 63; 416-419, 1973).

The sensor of the preferred embodiment utilizes such a self-imaging principle by placing the detector on the self-imaging plane of the object to detect the motion of the object. In order to detect the periodic signal in the self-image of the periodic object, the detector element is covered with a grating structure having the same period or two times the period of the object. As a result, when the self-image of the periodic pattern moves across such a detector, a maximum signal is produced when the light part of the periodic image is falling on the open section of the detector and a minimum signal is produced when the light part of the periodic image is blocked by the grating on top of the detector. Hence, the detector can produce a periodic time signal as the object moves across the sensor.

In the first preferred embodiment of the present invention, two of the detector elements are first covered with gratings having periods equal to twice that of the grating on the object. The two gratings covering the detectors have a 90 degree phase shift with respect to each other. The output signals from these two detector elements produce the necessary quadrature signals for determining the position of the object relative to the sensor. In the case of a periodic object such as the engraved disc shown in Fig. 3, an additional detector element not covered by any grating structure is used to detect the rotational speed of the rotating disc medium.

In the second preferred embodiment four detector elements with a comb-like structure are used for sensing the tracking information. This provides additional signal enhancement and bias signal removal.

For a further understanding of the nature and the advantages of the invention, reference should be made to the following description of a specific embodiment, taken in conjunction with the accompanying drawings, in which <ul id="ul0001" list-style="none" compact="compact"><li>Fig. 1 illustrates a prior art track sensing device.</li><li>Fig. 2 illustrates a system configuration where the device of the present invention is used.</li><li>Fig. 3 illustrates the nature of the servo tracks recorded on a floppy disk.</li><li>Fig. 4 illustrates the detector used in the first preferred embodiment of the sensor device of the present invention.</li><li>Fig. 5 illustrates a triangular shape grating which can be used in conjunction with the preferred embodiments of the present invention.</li><li>Fig. 6. illustrates a sinusoidal shape grating which can be used in conjunction with the preferred embodiments of the present invention.</li><li>Fig. 7 illustrate the detector used in the second preferred embodiment of the sensor device of the present invention.</li><li>Fig. 8 illustrates a triangular shape detector which can be used in conjunction with the second preferred embodiments of this present invention.</li><li>Fig. 9 illustrates a sinusoidal shape detector which can be used in conjunction with the second preferred embodiments of this present invention.</li></ul>

Fig. 2 shows the placement of the sensor in one preferred embodiment of the present invention, relative to the medium with the periodic structure. A device 101 is shown, consisting of a light emitting device 102 mounted on a multiple elements detector 103, which is mounted in turn on a header 104 with multiple pin outs. The light emitting device could be, for instance, a light emitting diode (LED) with a circular emitting window or a vertical cavity surface emitting laser (VCSEL). The diverging light 105 emitted by light source 102 is incident on the medium 107. Medium 107 is engraved with periodic tracks.

A typical medium 107 is shown in Fig. 3. The medium surface is engraved by a high power laser with circular tracks such as a track of marks 302, with periodic interruptions 304. In discs available commercially, the length of each mark on a track on the inner radius is about 40 µm and the length of a mark on the outer radius is about 80 µm. The distance between the marks along the radial direction is 20.4 µm and the width of each mark is about 2 µm.

Referring back to Fig. 2, with these periodic servo tracks engraved on the medium surface, self images of the engraved tracks will be formed as light 106 is reflected back by the medium. The distance between the laser chip and the medium is adjusted so that one of the self images is formed on the surface of the detector. The distances where the self images can be found are given by the equation <maths id="math0001" num="(1)"><math display="block"><mrow><mrow><mrow><mi mathvariant="normal">z</mi><mi>φ</mi><mi mathvariant="normal">z</mi><mn>1</mn></mrow><mo>/</mo><mrow><mrow><mo>(</mo><mrow><mi mathvariant="normal">z</mi><mi>φ</mi><mo>+</mo><mi mathvariant="normal">z</mi><mn>1</mn></mrow><mo>)</mo></mrow><mo>=</mo><mrow><mrow><mn>2</mn><mi mathvariant="normal">N</mi><mo>∗</mo><msup><mi mathvariant="normal">T</mi><mn>2</mn></msup></mrow><mo>/</mo><mrow><mi mathvariant="normal">WAVE</mi></mrow></mrow><mo>,</mo></mrow></mrow></mrow></math><img file="EP0895239B1_D0001.tif" /></maths> where N is an integer, T is the period of the servo tracks, zφ is the distance between the laser and the medium, z1 is the distance between the medium and the surface of the detector and WAVE is the wavelength of the light source. In practice, the thickness of the laser chip is much smaller than the distance between the laser and the medium. As a result, Equation (1) can be approximated by <maths id="math0002" num="(2)"><math display="block"><mrow><mi mathvariant="normal">z</mi><mi>φ</mi><mo>=</mo><mn>4</mn><mi mathvariant="normal">N</mi><mo>∗</mo><mrow><mrow><msup><mi mathvariant="normal">T</mi><mn>2</mn></msup></mrow><mo>/</mo><mrow><mi mathvariant="normal">WAVE</mi></mrow></mrow><mo>.</mo></mrow></math><img file="EP0895239B1_D0002.tif" /></maths> For example, if N=1, T=0.01 mm and WAVE=0.0008 mm, zφ = 0.5 mm. The period of the image on the detector is equal to <maths id="math0003" num="(3)"><math display="block"><mrow><mi mathvariant="normal">T</mi><mn>1</mn><mo>=</mo><mi mathvariant="normal">T</mi><mrow><mo>(</mo><mrow><mi mathvariant="normal">z</mi><mi>φ</mi><mo>+</mo><mi mathvariant="normal">z</mi><mn>1</mn></mrow><mo>)</mo></mrow><mo>.</mo><mi mathvariant="normal"> </mi><mi mathvariant="normal">z</mi><mi>φ</mi><mo>=</mo><mn>2</mn><mi mathvariant="normal">T</mi><mo>.</mo></mrow></math><img file="EP0895239B1_D0003.tif" /></maths> In other words, a two times magnified image of the tracks is formed at the detector plane.

Fig. 4 shows the first embodiment of the detector used in such a sensor.

A unique multiple element detector with different light blocking grating structures is shown. The detector 400 in Fig. 4 contains three (3) detector elements, 404, 405, and 406, each having bonding pads 407, 408, and 409. A surface emitting laser diode chip or a LED (light emitting diode) chip 401 is attached to the detector on top of a isolated bonding pad 403. Light is emitted from the window 402 on the laser chip or LED chip. The detector elements 404 and 405 are covered with light blocking structures with period 2T or T as shown in Fig. 4. As can be seen, the mask or grating 412 on top of the detector element 405 is shifted by 1/4 of the period of the grating 414 on detector 404, to generate a 90 degree phase shift between the output signals from detector element 404 and detector element 405. As a result, when a medium with tracks moves relative to the sensor, the signal from detector elements 404 and 405 can be written as <maths id="math0004" num="(5)"><math display="block"><mrow><mi mathvariant="normal">S</mi><mn>1</mn><mo>=</mo><mi mathvariant="normal">A</mi><mi mathvariant="normal">cos</mi><mi mathvariant="normal">θ</mi><mo>+</mo><mi mathvariant="normal">C</mi><mo>,</mo></mrow></math><img file="EP0895239B1_D0004.tif" /></maths><maths id="math0005" num="(6)"><math display="block"><mrow><mi mathvariant="normal">S</mi><mn>2</mn><mo>=</mo><mi mathvariant="normal">A</mi><mi mathvariant="normal">sin</mi><mi mathvariant="normal">θ</mi><mo>+</mo><mi mathvariant="normal">C</mi><mo>,</mo></mrow></math><img file="EP0895239B1_D0005.tif" /></maths> S1 and S2 are 90 degrees out of phase with respect to each other to form the quadrature signals needed for the determination of the radial position of the medium. The radial position of the medium relative to the sensor is linearly related to θ, which can be derived as <maths id="math0006" num="(7)"><math display="block"><mrow><mi mathvariant="normal">Tan</mi><mi mathvariant="normal">θ</mi><mo>=</mo><mrow><mrow><mrow><mo>(</mo><mrow><mi mathvariant="normal">S</mi><mn>2</mn><mo>−</mo><mi mathvariant="normal">C</mi></mrow><mo>)</mo></mrow></mrow><mo>/</mo><mrow><mrow><mo>(</mo><mrow><mi mathvariant="normal">S</mi><mn>1</mn><mo>−</mo><mi mathvariant="normal">C</mi></mrow><mo>)</mo></mrow></mrow></mrow><mo>.</mo></mrow></math><img file="EP0895239B1_D0006.tif" /></maths> In Equation (5) and Equation (6), we assume that the signals S1 and S2 have identical amplitude A and bias C. In practice they could be different. However, the general technique for extracting tracking information is similar to that given in Equation (7). The detector 406 in Fig. 4 is not covered by any mask. It is used to detect the rotational signal of the medium produced by the interrupted tracks.

Fig. 5 shows another variation of the periodic light blocking structure shown in fig. 4. These periodic structures 510, 512 shown in Fig. 5 have a triangular profile. It is well known that the harmonic content for a rectangular wave is proportional to 1/M, where M is the index for the harmonics of the waveform. On the other hand, the harmonic content of a triangular wave is proportional to 1/M², which is 18dB lower for the first harmonic.

Fig. 6 shows another variation of the periodic light structure. In this embodiment, the periodic structure 610, 612 has a sinusoidal profile (i.e., the height of the shape is proportional to sin2πx/T, where T is the period of the structure). The advantage of the sinusoidal profile is that it has only the first harmonic and no other higher harmonics. It is the ideal profile for extracting only a single spatial frequency from the servo tracks.

Note that more than half of the light sensitive area in the detector elements 404 and 405 in the first embodiment shown in Fig. 4 are blocked by the grating structures. Fig. 7 shows another preferred embodiment of the sensor which has better light collection efficiency than the first embodiment. In this embodiment, instead of using a grating mask on top of the light sensitive areas, a comblike structure for the detectors are used. In the embodiment of the detector as illustrated in Fig. 5, the detector now contains five elements. Each detector element has a comb structure with period T, or 2T. Detector element 501 is interlaced with detector element 502. Detector elements 503 and 504 are similarly interlaced. There is a 1/4 period shift between the detector group 501, 502 and the detector group 503, 504. In this second embodiment, the signals from detector elements 501, 502, 503 and 504 are given, respectively, by: <ul id="ul0002" list-style="none" compact="compact"><li>S1 = A cos⊖ + C</li><li>S2 = -A cos⊖ + C</li><li>S3 = A sin⊖ + C</li><li>S4 = -Asin⊖ + C.</li></ul> As a result, the radial information can be obtained from <ul id="ul0003" list-style="none" compact="compact"><li>D1 = S1-S2 = 2A sin⊖</li><li>D2 = S3-S4 = 2A cos⊖ and</li><li>Tanø = D2/D1.</li></ul> The advantages of the second embodiment over the first embodiment are: 1) the differential signal D1 and D2 has amplitude 2A versus A in the non-differential outputs in Equation (5) and Equation (6), and 2) there is no bias level in signal D1 and D2. Fig. 8 and Fig. 9 show two other variations of the second embodiment where the detectors are either triangular shape or sinusoidal shape. The shape of the detector is selected to reduce the harmonic distortion from the output signal.