BACKGROUND OF THE INVENTION  
         [0001]    The present invention relates to an optical track sensing device, and in particular to an optical sensor for detecting optical tracking information on a moving medium.  
           [0002]    U.S. Pat. No. 5,991,249 described a method whereby the motion of a moving medium with a grating on its surface can be detected by a sensor consisting of a semiconductor laser and a photodetector. In one example, the moving medium was a floppy disk. This prior art is based on the use of a sinusoidal pattern on the detector to select a particular diffracted wave from the moving grating. By placing the sensor in the self-imaging plane, the need for optical components was reduced. However, in many applications it is necessary to detect the beginning position of the moving grating. In certain applications positional encoding in two dimensions is also required. It is the intention of this application to describe certain improvements to the prior art U.S. Pat. No. 5,991,249, the disclosure of which is incorporated herein by reference.  
         BRIEF SUMMARY OF THE INVENTION  
         [0003]    The present invention reflects the recognition that a very acceptable detected signal can be obtained at other than the self imaging plane of the reflection off a moving medium (or a stationary medium and moving sensor). This provides more flexibility in the placement of the sensor, while still allowing the elimination of optical components by relying on self-imaging instead. In addition, by providing a pattern over the photodetector with a smaller period, higher frequency harmonics are detected, allowing more precise detection of the position of the medium.  
           [0004]    In a first embodiment of this invention the period of the detector pattern is selected to detect the higher harmonics of the grating on the medium. Moreover, in this embodiment the placement of the detector can be on planes other than the self-image plane of the grating to increase the resolution in detecting the motion of the grating.  
           [0005]    In one version of the first embodiment, the detector contains three light sensitive areas with phase shifts among them for the detection of the motion of a moving medium. This invention recognizes that the differential detection benefit of quadrature signals can be obtained with only three, rather than four, detectors. The invention also applies to a stationary medium, but for simplicity, the discussion herein is directed to the example where the medium moves.  
           [0006]    In a second embodiment of the present invention a diffractive cylindrical lens is placed in front of the laser to focus the laser beam to a line on the surface of the moving medium. This line beam is perpendicular to the lines forming the grating. This increases the light collection by the motion detector and reduces noise generated by multiple reflections. In one version of this second embodiment, the period of the detector pattern corresponds to the nth harmonic of the grating. In another variation, the laser beam is focused to a line on the detector. This further improves the light collection at the detector, at the expense of a less sharp image from the medium, which is acceptable in some embodiments.  
           [0007]    A third embodiment of the present invention provides for detection of the index marking recorded on the grating. A two element photodetector is used to detect the index. There is no need for a pattern on the photodetector, a simple reflection from the index marking is detected.  
           [0008]    A fourth embodiment of this present invention provides an integrated position sensor, which can both detect the motion of the medium and the index marking on the medium. A first laser and detector combination, with a pattern over the detector, detect the motion of the medium by detecting the grating pattern. A second laser and detector combination are mounted offset from the first laser and detector combination, to detect an index marking adjacent the grating on the medium.  
           [0009]    A fifth embodiment of the present invention uses a diffracting grating to direct the reflected light to the photodetectors. The grating has the periodic pattern overlayed on it, instead of putting the pattern on the detector itself. This allows the use of a generic detector and reduces the design and manufacturing time for a new pattern. The grating has different periods in different zones, so that the different zones direct the reflected light to different photodetectors.  
           [0010]    A sixth embodiment of this invention provides a sensor which can detect motion of a moving medium in two dimensions. Two sets of detector elements are used, each aligned with an axis of one of the two dimensions. Each set of detector elements has its own pattern, corresponding to the grating frequency along its axis on the moving medium. Diffraction gratings can be used to minimize the interference effect of the medium pattern in the other dimension.  
       
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS  
       [0011]    [0011]FIG. 1 shows the multiple virtual sources produced by a grating  
         [0012]    [0012]FIG. 2( a ) shows a grating profile with uneven mark and space.  
         [0013]    [0013]FIG. 2( b ) shows the spectrum of the grating profile in (a).  
         [0014]    [0014]FIG. 3( a ) shows the first embodiment of the present invention.  
         [0015]    [0015]FIG. 3( b ) shows the top view of the detector device with the laser chip.  
         [0016]    [0016]FIG. 3( c ) shows the embodiment of FIG. 3( a ) with another configuration of the light detectors.  
         [0017]    FIGS.  4 ( a )-( c ) show three different kinds of detector patterns.  
         [0018]    [0018]FIG. 5( a ) shows an improved device, where diffractive elements focus the laser beam to a line on the motion grating.  
         [0019]    [0019]FIG. 5( b ) shows the diffractive element put on top of the detector in FIG. 5( a ).  
         [0020]    [0020]FIG. 6( a ) shows an embodiment that uses a grating as the filter.  
         [0021]    [0021]FIG. 6( b ) shows one embodiment of a diffractive pattern on the cylindrical lens of FIG. 6( a ).  
         [0022]    [0022]FIG. 6( c ) shows the detail of the detector and the laser chip in FIG. 6( a ).  
         [0023]    [0023]FIG. 6( d ) shows another embodiment of the diffractive elements of FIG. 6( b ).  
         [0024]    [0024]FIG. 6( e ) shows another embodiment of a detector structure for use with the embodiment of FIG. 6( d ).  
         [0025]    [0025]FIG. 7( a ) shows a grating with index marking.  
         [0026]    [0026]FIG. 7( b ) shows a device for detecting the starting position of the grating.  
         [0027]    [0027]FIG. 7( c ) shows the top view of the laser/detector device for use with the embodiment of FIG. 7( a ).  
         [0028]    [0028]FIG. 7( d ) shows an embodiment of a diffractive pattern on the glass cylindrical lens of FIG. 7( a ).  
         [0029]    [0029]FIG. 8( a )-( c ) illustrate how a split detector generates the index signal for the embodiment of FIG. 7( a ).  
         [0030]    [0030]FIG. 8( d ) illustrates the signal generated for the example of FIGS.  8 ( a )-( c ).  
         [0031]    [0031]FIG. 9( a ) shows an integrated device for detecting the index mark and the grating motion.  
         [0032]    [0032]FIG. 9( b ) shows the diffractive element on top of the device in FIG. 9( a )  
         [0033]    [0033]FIG. 10( a ) shows a two-dimensional grating motion detecting device.  
         [0034]    [0034]FIG. 10( b ) shows a two-dimensional grating with comer markings.  
         [0035]    [0035]FIG. 10( c ) shows the diffractive element on top of the device in FIG. 10( a )  
         [0036]    [0036]FIG. 11( a ) shows a modification of the device in FIG. 10( a ) for detecting the motion of the two-dimensional grating and the index marking on the grating.  
         [0037]    [0037]FIG. 11( b ) shows the diffractive elements on top of the device in FIG. 11( a ). 
     
    
     DETAILED DESCRIPTION OF THE INVENTION  
       [0038]    Basic Principles  
         [0039]    In FIG. 1 a laser source  101  illuminates a grating  102  with period T 0  at a distance Z 0  from the laser source  101 . The diffracted waves on plane  103  at a distance Z 1  from the grating can be perceived as waves emitting from multiple sources as indicated by  104 ,  105 ,  106 ,  107 . The separation of these sources is given by T=Z 0 λ/T 0 . Hence, the diffracted waves at plane  103  can be written as  
                 F        (     x   ,   y     )       =       ∑   n            A   n                   exp        {     j          2      π     λ                (     x   -   nT     )     2     +     y   2     +     Z   2           }           ,           (   1   )                               
 
         [0040]    where j={square root}{square root over (−1)}, x and y are the spatial coordinates at plane  103  and Z=Z 0 +Z 1 . For x and y much less than Z, the function F(x, y) in Eq. (1) can be approximately written as:  
                 F        (     x   ,   y     )       ≅     ∑     A   n         ,     exp        {     j          π     λ                 Z            [         (     x   -   nT     )     2     +     y   2     +     φ   n       ]         }       ,           (   2   )                               
 
         [0041]    where φ n  is a constant phase. As can be seen, F(x, y) contains signals with spatial frequencies v=nT/λZ=nZ 0 /T 0 Z=n/T 0 M, where M=Z/Z 0 .  
         [0042]    For example, the interference between the n=1 and n=−1 terms in Eq. (2) can be written as:  
               S        (     x   ,   y     )       =              exp        {     j        π     λ                 Z              (     x   -   T     )     2       }       +     exp        {     j        π     λ                 Z              (     x   +   T     )     2       }              2             (   3   )                               
 
         [0043]    In Eq. (3) we assume that A −1 =A 1  and φ −1 =φ 1 . After simplification, S (x, y) becomes  
               S        (     x   ,   y     )       =       cos        (     2      π        T     λ                 Z          x     )       =       cos        (     2      π                   x   /     MT   0         )       .               (   4   )                               
 
         [0044]    Since the interference pattern with period MT 0  can also be produced by other diffracted orders such as n=0 and n=2, the amplitude of the interference pattern with certain spatial frequency is dependent on the distance Z 1  from the grating. The article “The Talbot Effect” by Masud Mansuripur published in Optics and Photonic News (April 1997 Vol. 8 No. 4) explained that the planes located at Z 1 =2kMT 0   2 /λ where k is an integer are optimal for signal detection.  
         [0045]    However, as pointed out in the previous discussion, signal detection can take place at planes other than the self image planes defined by the Talbot effect. Therefore, a sinusoidal detector with period MT 0  placed at distance Z 1  from the grating can generate a sinusoidal signal corresponding to the motion of the grating.  
         [0046]    As shown in Eq.(2), the grating, after illumination by the laser beam, produces many diffracted waves. The accuracy in detecting the motion of the grating is dependent on the period of the grating used. The smaller is the period of the grating, the higher is the signal accuracy. It is interesting to note that in using the diffracted waves to detect the motion of a moving grating, the signal accuracy can further be improved by using a detector with period corresponding to a higher order diffracted wave. Although detector with the lowest spatial period MT 0  is most commonly used for detecting the motion of grating with period T 0 , higher order spatial frequency from the moving grating can be detected by using spatial period MT 0 /n in the detector structure, where n is the diffracted order.  
         [0047]    [0047]FIG. 2( a ) shows a grating with uneven mark and space. The ratio of the length of the mark b and the space a is q=a/b. It can be shown that the transmission of the grating can be written as,  
                 g        (   x   )       =       ∑   n            A   n          cos        (     2      n                 π                   x   /     T   0         )             ,     
            where                   A   n       =       sin        (     n                 π                 q     )         n                 π                 (   5   )                                 
         [0048]    [0048]FIG. 2( b ) illustrates the harmonic spectrum of a grating with q=10. As can be seen, this grating contains many harmonics. As a result, a detector with period MT 0 /n, where M=(Z 1 +Z 0 )/Z 0  can pick up the nth harmonic of the grating mounted on the moving medium. Suppose that the period of the moving grating is 20 μm. In the case that Z 0  and Z 1  are approximately the same the magnification on the detector plane M is approximately equal to 2. To detect this spatial frequency, the sinusoidal pattern on the detector has a period of M·20 μm=40 μm. But, the 4 th  harmonic of this 20 μm grating has a period of 5 μm, which can be detected by using a sinusoidal pattern on the detector with period of 10 μm. This is a 4 fold improvement on the positional accuracy.  
         [0049]    Three Detectors Instead of Quadrature Detection.  
         [0050]    U.S. Pat. No. 5,991,249 showed periodic detectors having a 90 degree phase difference relative to each other. In one of the embodiments in U.S. Pat. No. 5,991,249 the four periodic detectors are shown to have phase delays of 0, 90, 180, and 270 degrees. Quadrature signals with minimal offsets are produced by taking the difference between the 0 degree and 180 degree signals and also the difference between the 90 degree and 270 degree signals. However, it can be shown that differential detection can also be achieved by only three periodic patterns. For example,  
           S   1 =−sin(2π x/T+ 2π/3)+ q, M= sin(2π x/T )+ q, S   2 =sin(2π x/T+ 2π/3)+ q.    (5)  
         [0051]    The quadrature signals A and B can be generated using the three signals in Eq.(5):  
           A=M−S   1 =sin(2π x/T )+sin(2π x/T+ 2π/3)=2 cos(π/6)sin(2 πx   /T+   π 6),   (6)  
           B=S   2   −M= sin(2π x/T+ 2π/3)−sin(2π x/T )=2 sin(π/6)cos(2π x/T+π/ 6).   (7)  
         [0052]    The position of the grating can be determined from  
       φ   =       2      π                   x   /   T       =         tan     -   1            (       A   B          tan        (     π   6     )         )       -       π   6     .                               
 
         [0053]    Therefore, only three detectors with periodic structures are required in the detection of the motion of the grating. Other phase relationship between S 1 , M and S 2  is also possible. For example, when the phase angle 2π/6 in Eq.(5) is replaced by π/2,  
       φ   =       2      π                   x   /   T       =         tan     -   1            (     A   B     )       -     π   4                               
 
         [0054]    is even easier to calculate.  
         [0055]    Detector Structure.  
         [0056]    [0056]FIG. 3( a ) shows the first improvement of the present invention. A vertical cavity surface emitting laser (VCSEL) chip  302  is bonded on top of the detector chip  303 . The detector chip  303  is mounted on a header  304  for connecting to the electronic system. The complete device  301  is placed at a distance from the medium  307 . The surface of the medium facing the laser contains a periodic grating. Laser  302  emits a diverging cone of light, indicated by line  305 . After reflecting back from the medium surface, the reflected beam  306  illuminates the light sensitive elements on the detector. The principle of operation of the device  301  according to U.S. Pat. No. 5,991,249 is based on the fact that diffracted light reflected off the periodic medium can form a Talbot image (or self image) of the grating on the detector surface located at Z 1 =2kMT 0   2 /λ. However, in this first embodiment of this present invention, the surface of the detector can be placed at a plane other than the self-imaging planes.  
         [0057]    [0057]FIG. 3( b ) shows the top view of the detector device. Besides the laser  302 , three periodic light sensitive patterns  308 ,  309  and  310  are shown. These patterns overlay the underlying photodetector elements  312 ,  314  and  316 , respectively. The photodetectors are connected to pads  318 ,  320  and  322 , respectively. The periodic patterns in  308  and  309  are 120 degrees out of phase. The periodic patterns in  308  and  310  are 180 degrees out of phase. The phase relationship between these three periodic patterns is defined mathematically by Eq.(5). As pointed out in the previous discussion, it is preferred to make the pattern on the periodic detector to have a period equal to MT 0 /n , where M=(Z 1 +Z 0 )/Z 0 . This will allow this first embodiment of the present invention to pick up the nth harmonic of the grating mounted on the moving medium to improve on the detection accuracy.  
         [0058]    [0058]FIG. 3( c ) shows another configuration of the light sensitive elements for detecting the diffracted waves. Instead of detectors aligned along the axis of the periodic pattern, the detectors are aligned perpendicular, with each detector crossing under multiple periodic structures. Three detectors,  324 ,  326  and  328  are arranged horizontally. The periodic structures  330 ,  332  and  334 , which overlay the three detectors, respectively, are similar to the structures in FIG. 3( b ), except that multiple, parallel structures are used across each detector, having the same phase. The phase changes in the vertical direction, with the phase changing from structure  330  to structure  334 , and then again from structure  334  to structure  336 . Bonding pads  336 ,  338  and  340  connect to detectors  324 ,  326  and  328 , respectively.  
         [0059]    FIGS.  4 ( a )-( c ) show three different periodic patterns which could be used for picking up the motion of the grating. The most preferred pattern is the sinusoidal pattern shown in FIG. 4( a ) with a sinusoidal structure  410  overlying detector  412 . Alternately, the triangular pattern  414  of FIG. 4( b ) could be used over a detector  416 , or the rectangular pattern  418  of FIG. 4( c ) over a detector  420 .  
         [0060]    Diffractive Cylindrical Lens.  
         [0061]    In FIG. 3 the light beam reflected back from the medium diverges towards the detector. The area of the light sensitive element on the detector is smaller than the beam on the detector. Therefore, the detector can only collect a relatively small amount of the reflected light. FIG. 5 shows a second preferred embodiment of the present invention, which can improve the light collection of the first embodiment shown in FIG. 3. A laser chip  501  is shown mounted on a detector chip  502 . Laser beam  503  from chip  501  is incident on a diffractive cylindrical lens  504 . The top view of the grating of diffractive cylindrical lens  504  is shown in FIG. 5( b ). The cylindrical lens  504  is different from a spherical lens in that it has focal power only in one dimension. The phase variation on such a diffractive element has the form.  
                 φ        (   x   )       =         2      π       λ                 F            x   2         ,           (   8   )                               
 
         [0062]    where A is the wavelength of the laser and F is the focal length. Due to the diffractive cylindrical lens, beam  503  is focused to a line perpendicular to the plane of the paper on the grating surface  505  of the moving medium. The diverging beam in the direction normal to the plane of the drawing still interacts with the grating to project an interference pattern on the detector. The reflected beam from surface  505  passes through a periodic grating  506  whose function is to spread the light beam more uniformly across the detector  507 . The light detecting element  507  is similar to the detector shown in FIG. 3( b ) or FIG. 3( c ).  
         [0063]    [0063]FIG. 6( a ) shows another improvement of this present invention. A laser chip  601  is shown mounted on a detector chip  602 . Laser beam  603  from chip  601  is incident on a diffractive cylindrical lens  604 , which is similar to the one described the second embodiment of the present invention. However, instead of focusing the light to a line on the medium surface, the diffractive beam from the cylindrical hologram lens is focused on the detector surface  605  as shown in FIG. 6( a ). By focussing on the detector surface, the amount of light received by the detector is further improved. The light will not be focussed on the medium, resulting in a less sharp image. However, a tradeoff can be made between the sharpness of the image and the amount of light collected by the detector.  
         [0064]    Combined Periodic Structure and Diffraction Lens.  
         [0065]    In another element of the embodiment shown in FIG. 6( a ), there is another grating structure  606  etched on the glass substrate, which is shown in FIG. 6( b ). Instead of putting the periodic pattern on the detector elements, it is put on this grating structure, and the beams are diffracted to different detector elements so each detector element receives a phase-shifted version. The sinusoidal shape of the grating is divided into multiple zones. The period of the sinusoidal boundary is related to the grating on the moving medium by MT 0  where M=(Z 2 +Z 0 )/Z 0  and Z 2  is the distance between the medium and the top surface of the grating. As shown in FIG. 6( b ), there are four zones  607 ,  608 ,  609  and  610 . In this discussion each zone is separated by 90 degree phase shift from each other. Each zone also contains evenly spaced grating with different periodicity. For example, the gratings in zone  607 ,  608 ,  609  and  610  has periods t, t/2, t/3 and t/4 respectively. The purpose of the gratings is to project light incident on each zone to different detectors  671 ,  672 ,  681 ,  682 ,  691 ,  692 ,  611  and  612  as shown in FIG. 6( c ).  
         [0066]    A central detector  613  collects the undiffracted beam. The central detector is not used, and is there simply because it allows a standard detector structure to be used for the product. The next closest pair of detectors  671  and  672  to the center collect the ±1 st  order diffracted light from zone  607 . The next pair of detectors  681  and  682  collect the ±1 st  order diffracted light from zone  608 . The detectors  691  and  692  collect the ±1 st  order diffracted light from zone  609 . The detectors  611  and  612  collect the ±1 st  order diffracted light from zone  610 . The advantage of this embodiment is that the filtering of the motion signal is done by the grating  606 , and not by the structure on the detector as in U.S. Pat. No. 5,991,249 or in the previous embodiments discussed in this present invention. This greatly reduces the time required to design a new device with a different grating period on the moving medium. Typically it takes about 3 months to implement a new detector. However, it takes about two weeks to have a new grating fabricated. Variations in the grating are possible. For example, instead of using 4 zones for the grating with 90 degree phase shift, a three zone structure with 120 degree phase shift can also be used.  
         [0067]    [0067]FIG. 6( d ) shows another embodiment,  606 ′, of the grating  606  of FIG. 6( b ). Instead of interleaving the four zones, zones  620  and  622  occupy the top half of the grating, and zones  624  and  626  occupy the lower half of the grating. Each pair of zones is 180 degrees out of phase, and the zone pair  624  and  626  is delayed by a 90 degree phase shift from zones  620  and  622 . The light sensitive elements necessary to detect the four quadrature signals are shown in FIG. 6( e ). The detector still has nine light sensitive elements similar to the detector in FIG. 6( c ). However, there are only two pairs of detectors horizontally, two on top, and two on the bottom. Zone  620  diffracts to detectors  631  and  632 , while zone  622  diffracts to detectors  633  and  634 . Similarly, on the bottom half, zone  624  diffracts to detectors  635  and  636 , while zone  626  diffracts to zones  637  and  638 .  
         [0068]    There are two advantages in this embodiment. One is that there are only two different periods in the four zones. Secondly, the second order diffraction from the lower frequency grating may leak into the detector  634  and  633 . Since the quadrature signals is obtained by taking the difference between the signals from the detector  634  and  631 , the crosstalk between the detectors  631  into  634  only reduces the signal modulation by a small amount.  
         [0069]    Index Mark Detection.  
         [0070]    [0070]FIG. 7( a ) shows a portion of a moving medium  720  with a grating  722  having index markings  724 ,  726  at either end of the grating. The dark area of the index marking indicates metal coating has been applied to the glass. It can be seen that the index mark is a transition from metal coating to no metal coating.  
         [0071]    [0071]FIG. 7( b ) shows how the index marking is detected. Similar to FIG. 4, the light from the laser  701  is incident on a diffractive cylindrical lens  702 , formed on a glass element  710 , which focuses the light beam to a line slightly behind the grating surface and on the adjacent index marking portion of the grating  703 . The light reflected by the index marking falls on a split detector  704 ,  705 , which is part of a detector chip  706 .  
         [0072]    [0072]FIG. 7( c ) shows the top view of the device in FIG. 7( b ). A VCSEL laser  701  is mounted on a detector chip  706 . Next to the VCSEL are two light sensitive elements  704  and  705 . The difference between the outputs from  704  and  705  constitutes the index signal.  
         [0073]    [0073]FIG. 7( d ) shows the glass element  710  of FIG. 7( b ) from the top, with the cylindrical diffractive lens element  702 .  
         [0074]    FIGS.  8 ( a )- 8 ( c ) illustrate how the split detector generates the index signal. To simplify the discussion the detector is shown on the right (A, B) behind index marking plane ( 802 ) and on the opposite side of the laser (on the left, not shown). Laser beam  804  is shown focused at a point  806  after passing by the index marking plane, then expanding again until it contacts the detectors A, B. This configuration is shown, instead of a reflective configuration, to demonstrate the concept. The concept applies equally well to a reflective configuration, which is simply more complicated to draw.  
         [0075]    [0075]FIG. 8( a ) shows the metal coating area is outside the laser beam. As a result both detector A and detector B are both illuminated. Hence, the difference signal A−B is zero. In FIG. 8( b ) the metal coating is blocking half of the laser beam (in a reflective configuration, the metal coating would reflect the beam, and the non-metal would not, reversing the detector signal. Detector A is still illuminated. However, the metal coating is obstructing the light from reaching detector B. Therefore, A−B&gt;0.  
         [0076]    Finally, in FIG. 8( c ) the metal coating filly blocks the light from reaching detector A and B. Once again, A−B=0.  
         [0077]    The signal  820  generated by A−B is shown in FIG. 8( d ). The signal increases, then decreases as the metal coating, indicating an index marking, passes in front of the detectors. A similar explanation can be applied to the situation where the detector is placed on the same side as the laser.  
         [0078]    Combined Index and Grating Detector.  
         [0079]    [0079]FIG. 9( a ) shows the top view of another embodiment of the present invention which detects both the index mark and the position of the grating on a moving medium. In FIG. 9( a ) laser chips  901  and  903  are bonded on top of detector chip  900 . A glass element  908  with diffractive elements  905 ,  906  and  907  shown in FIG. 9( b ) is placed on top of the detector device in the same manner as in FIG. 7( b ). Diffractive element  906  is a cylindrical diffractive lens like lens  504  of FIG. 5( b ), and focuses the laser beam from laser chip  901  to a line parallel to the line separating detector  904  and  905 . That line is then reflected off the medium onto diffractive element  905 , which spreads the reflected beam over three element detector  902  to detect the position of the grating (similar to diffractive element  506  of FIG. 5 ( b )).  
         [0080]    Diffractive element  907  focuses the laser beam from laser  903  into a line parallel to the sinusoidal detectors  902 . The reflected beam, used to detect the index marking, impacts two element detectors  904  and  905 . Laser chip  903  is placed a distance from laser chip  001  corresponding to the distance on the media between the grating structure and the index marking. If the grating is arranged in rows, with index markings for each one, the index marking detected could be one several rows over to allow a practical placement of the laser chips and detectors.  
         [0081]    Two Dimensional Grating Detection.  
         [0082]    The top view of another embodiment of this present invention is shown in FIG. 10( a ) . A VCSEL laser  1001  is mounted on a detector chip  1002 . The detector chip has two separate light detection areas. Light detection areas  1003 ,  1004 ,  1005  and  1006  are used to detect the motion of the moving grating in one axis. Light detection areas  1007 ,  1008 ,  1009  and  1010  are used to detect the motion of the moving grating in along an axis perpendicular to the first axis.  
         [0083]    [0083]FIG. 10( b ) shows the structure of the two-dimensional grating is shown in FIG. 10( b ). The dark corners  1020 ,  1022 ,  1024  and  1026  are the index markings for the grating  1028 . The detectors  1003 ,  1004 ,  1005  and  1006  all have proper sinusoidal patterns to detect the motion of the grating in the right and left direction. Detectors  1007 ,  1008 ,  1009  and  1010  detect movement of the grating in the up and down (on the figure) direction.  
         [0084]    Additional Grating to Eliminate Effect of Modulation Along Other Axis.  
         [0085]    When the reflection from the grating on the moving medium moves in the up and down direction, it is necessary that the signal produced by light sensitive areas  1003 ,  1004 ,  1005  and  1006  remain constant. A regular phase grating  1015  (see FIG. 10( c )) is placed on top of the detectors  1003 ,  1004 ,  1005  and  1006 . This grating  1015  will smooth out the light fluctuation so that the output signal from detectors  1003 ,  1004 ,  1005  and  1006  are not sensitive to up and down motion and is only sensitive to left and right motion. In a similar fashion a grating  1016  is placed on top of the detectors  1007 ,  1008 ,  1009  and  1010  will render the detectors  1007 ,  1008 ,  1009  and  1010  less sensitive to the left and right motion of the grating.  
         [0086]    [0086]FIG. 11( a ) shows another embodiment of this present invention. This device combines two of the devices of FIG. 7 and one device of FIG. 10 in order to detect the indeces along two axes and the motion of the two-dimensional gratings. A laser  1101  illuminates the two-dimensional grating for motion detection. Detectors  1104 ,  1105  and  1106  generate a motion signal in the first axis of the grating. Detectors  1107 ,  1108 , and  1109  generate a motion signal in the second axis perpendicular to the first axis.  
         [0087]    Lasers  1102  and  1103  in combination with the quadrant detector  1110 ,  1111 ,  1112  and  1113  generate the index signals.  
         [0088]    [0088]FIG. 11( b ) shows a pair of cylindrical lens,  1114  and  1115 , which focus the laser beams from lasers  1102  and  1103  to a line on the grating surface as discussed in the device described in FIG. 7.  
         [0089]    As will be understood by those of skill in the art, the present invention may be embodied in other specific forms without departing from the essential characteristics thereof. For example, the medium could be stationary, and the sensor could be moving, or vice-versa. Accordingly, the foregoing description is intended to be illustrative, but not limiting, of the scope of the invention which is set forth in the following claims.
An optical track sensing device, and in particular to an optical sensor for detecting optical tracking information on a moving medium (or stationary medium and moving sensor). The sensing device relies on self-imaging, rather than optics, and obtains a very acceptable detected signal at other than the self imaging plane of the reflection off a moving medium. This provides more flexibility in the placement of the sensor, while still allowing the elimination of optical components by relying on self-imaging instead. In addition, by providing a pattern over the photodetector with a smaller period, higher frequency harmonics are detected, allowing more precise detection of the position of the medium. In one embodiment, the period of the detector pattern is selected to detect the higher harmonics of the grating on the moving medium.