Patent Document

BACKGROUND OF THE INVENTION  
         [0001]    1. Field of the Invention  
           [0002]    The present invention relates to a circuit for detecting synchronization errors, and in particular to a circuit that can be usefully combined with a circuit that detects errors in data received in, for example, a digital wireless communication system.  
           [0003]    2. Description of the Related Art  
           [0004]    The methods generally used for data error control in digital wireless communication systems include cyclic redundancy check (CRC) codes and forward error correction (FEC).  
           [0005]    CRC codes enable errors to be detected. Treating the individual bits of transmit data as the coefficients of a polynomial, the transmitting apparatus divides a block of transmit data by a predetermined generator polynomial, and redundantly appends the remainder to the block as a CRC code. The receiving apparatus divides the received block, including the appended CRC code, by the same generator polynomial, and checks that the result is zero. Output of a non-zero bit by the checking circuit indicates that a data error has occurred in the transmission channel.  
           [0006]    FEC employs a type of redundant code has both an error-detecting and an error-correcting capability. Due to the structure of the codes used, however, long burst errors present difficulties for FEC, while the CRC method can detect long burst errors with a fairly high degree of accuracy. The CRC and FEC methods are therefore most effective when they are used selectively, according to the rate of error occurrence and other channel conditions. Not infrequently, the CRC and FEC methods are used in combination.  
           [0007]    When the CRC method is used alone, or when the FEC method is used but an error that exceeds the FEC error-correcting capability is detected, a retransmission request is sent to the transmitting apparatus.  
           [0008]    Errors may occur in the transmission channel for various reasons, including noise radiating from surrounding areas. When the channel is a wireless channel, errors may also occur because the transmitting apparatus and receiving apparatus are too widely separated and the received radio signal is too weak. Another possible cause is clock jitter in either the transmitting communication apparatus or the receiving communication apparatus. In this case, the channel is regarded as including part of the communication apparatus itself.  
           [0009]    The coding theory on which existing methods of error control such as the CRC and FEC methods are based is predicated on the assumption of perfect synchronization between the transmitting and receiving apparatus. If this assumption is not true, error control performance falls short of theoretical expectations.  
           [0010]    In actual communication, this assumption is often false. Imperfect synchronization can lead to errors known as bit drop-outs or drop-ins. A drop-out occurs when a bit in the original data stream is deleted in the transmission channel. A drop-in occurs when an originally nonexistent bit is inserted into the data stream in the transmission channel.  
           [0011]    Since the CRC and FEC methods assume perfect synchronization, from their coding-theoretical viewpoint, even a single bit drop-out (or drop-in) can cause errors in all the succeeding bits, including the redundant check codes, because a drop-out shifts all succeeding bits forward by one position and a drop-in shifts all succeeding bits back by one position. This can create a very large burst error that can easily exceed not only the FEC error-correcting capability but also the CRC error-detecting capability, making proper error detection impossible.  
           [0012]    When the error detection function is realized by the CRC method alone, for example, a typical generator polynomial is g(D)=D 16 +D 12 +D 5 +1. The redundant code generated by this polynomial has sixteen bits, so the number of different check patterns is 65,536 (=2 16 ). If errors occur randomly, the probability of a wrong CRC indication is only 1/65,536. More specifically, this is the probability that a random sequence of erroneous bits will defeat the CRC check by fortuitously generating the correct (zero) CRC result. When an error is caused by a bit drop-out or drop-in, however, the probability of a wrong CRC indication is much higher. As a result, it becomes difficult to maintain good communication quality in the face of synchronization errors with their attendant bit drop-ins and drop-outs.  
         SUMMARY OF THE INVENTION  
         [0013]    A general object of the present invention is to improve communication quality;  
           [0014]    A more specific object is to avoid the occurrence of unrecognized data errors due to faulty synchronization.  
           [0015]    The invented synchronization error detection circuit includes a transition detector that detects rising or falling transitions in a received pulse train, and a cyclic number generator that generates numbers in a cyclically repeating series having a cycle length corresponding to the pulse rate in the pulse train. A selector selects the number generated when a transition is detected. A predetermined operation is performed on the numbers selected in this way to detect synchronization errors.  
           [0016]    The predetermined operation may include calculating average values of the selected numbers over groups of transitions, and comparing the average values of successive groups. A synchronization error can then be detected when the difference between successive average values exceeds a predetermined threshold value.  
           [0017]    Alternatively, the predetermined operation may include taking a difference between the selected numbers associated with a consecutive pair of transitions to obtain a pulse width value. In this case, a synchronization error can be detected when the pulse width value is, for example, less than a predetermined threshold value.  
           [0018]    The synchronization error detection circuit may include a retransmission request generator for sending a retransmission request to a transmitting source of the received pulse train when a synchronization error is detected. 
       
    
    
     BRIEF DESCRIPTION OF THE DRAWINGS  
       [0019]    In the attached drawings:  
         [0020]    [0020]FIG. 1 is a block diagram schematically showing part of a communication device incorporating a phase variation error detection circuit embodying the present invention;  
         [0021]    [0021]FIG. 2 is a block diagram schematically showing the main parts of the phase variation error detection circuit in FIG. 1;  
         [0022]    [0022]FIG. 3 is a block diagram schematically showing the main parts of the transition detection circuits in FIG. 2;  
         [0023]    [0023]FIG. 4 is a timing diagram illustrating the operation of the phase variation error detection circuit;  
         [0024]    [0024]FIG. 5 is a block diagram schematically showing the main parts of a phase number selection circuit in FIG. 2;  
         [0025]    [0025]FIG. 6 is a block diagram schematically showing part of a communication device incorporating a pulse width error detection circuit embodying the present invention;  
         [0026]    [0026]FIG. 7 is a block diagram schematically showing the main parts of the pulse width error detection circuit in FIG.  6 ; and  
         [0027]    [0027]FIG. 8 is a timing diagram illustrating the operation of the pulse width error detection circuit. 
     
    
     DETAILED DESCRIPTION OF THE INVENTION  
       [0028]    Embodiments of the invented synchronization error detection circuit will now be described with reference to the attached drawings, in which like elements are indicated by like reference characters.  
       FIRST EMBODIMENT  
       [0029]    Referring to FIG. 1, the synchronization error detection circuit in the first embodiment is a phase variation error detection circuit  10  used in a communication apparatus  20  having a receiving function. The communication apparatus  20  also includes a CRC processing circuit  21 , an FEC processing circuit  22 , an error detection control circuit  23 , a retransmission request generator  24 , and other circuits, such as a clock recovery circuit (not shown), which are used in receiving data.  
         [0030]    The communication apparatus  20  receives a data stream RD 1  from a transmission channel such as a phone link PL. The received data stream RD 1  is converted from analog to digital form and processed by various filters (not shown) and other necessary circuits, then supplied to the synchronization error detection circuit  10 , CRC processing circuit  21 , and FEC processing circuit  22 . The transmission channel PL may be a wireless channel or a wireline channel, or a channel including both wireline and wireless sections. Components of the communication apparatus itself, including the filters and analog-to-digital converter, may be treated as part of the transmission channel PL.  
         [0031]    The CRC processing circuit  21  uses the cyclic redundancy check method to detect data errors in the received data stream RD 1 . The FEC processing circuit  22  uses a forward error correction method to detect and correct data errors in the received data stream RD 1 .  
         [0032]    Although the communication apparatus  20  in the first embodiment includes both CRC and FEC processing circuits, if necessary, one of the two circuits, either the CRC processing circuit  21  or FEC processing circuit  22 , may be omitted, or replaced by a circuit using another error control method.  
         [0033]    As will be described in more detail below, the phase variation error detection circuit  10  detects phase variations in the received data stream RD 1 . Such phase variations are a sign of imperfect synchronization and can lead to bit drop-ins and drop-outs. On detecting a large phase variation, the phase variation error detection circuit  10  supplies an error detection signal ED 3  to the error detection control circuit  23 .  
         [0034]    The error detection control circuit  23  performs error control by controlling decoding operations according to the outputs from the CRC processing circuit  21 , FEC processing circuit  22 , and phase variation error detection circuit  10 . More specifically, when the phase error detection signal ED 3  is inactive, the outputs ED 1  and ED 2  from the CRC processing circuit  21  and FEC processing circuit  22  are used for error control; when the phase error detection signal ED 3  is active, the outputs ED 1  and ED 2  from the CRC processing circuit  21  and FEC processing circuit  22  are ignored and a retransmission control signal RS 1  is output. The retransmission control signal RS 1  causes the retransmission request generator  24  to send a retransmission request signal RC 1  to the communicating apparatus (not shown) that transmitted the received data stream RD 1 . This transmitting communication apparatus then sends a data stream with the same content as before. In the receiving communication apparatus  20 , the retransmitted data become a newly received data stream RD 1 .  
         [0035]    The reason for the operations described above is that when the phase error detection signal ED 3  is inactive, the receiving communication apparatus  20  can normally recover an accurate clock signal from the received data stream RD 1 . The receiving communication apparatus  20  can thus maintain accurate synchronization with the transmitting communication apparatus, so the reliability of the outputs ED 1  and ED 2  from the CRC processing circuit  21  and FEC processing circuit  22  is high. When the phase error detection signal ED 3  is active, however, synchronization between the transmitting communication apparatus and the receiving communication apparatus  20  is likely to be inaccurate, making the ED 1  and ED 2  outputs unreliable. In this case, it is safer to disable the FEC and CRC data error detection and correction functions and request retransmission.  
         [0036]    If the synchronization problem that activated the phase error detection signal ED 3  is temporary, the retransmitted data stream RD 1  may be received without triggering another active phase error detection signal ED 3  from the phase variation error detection circuit  10 . In this case, since bit drop-ins and drop-outs are presumably absent, the outputs ED 1  and ED 2  from the CRC processing circuit  21  and FEC processing circuit  22  are presumed reliable and the error detection control circuit  23  controls the decoding operations according to them.  
         [0037]    [0037]FIG. 2 shows an exemplary structure of the phase variation error detection circuit  10 . In this example, the phase variation error detection circuit  10  includes a pair of transition detection circuits  11 ,  12 , a phase counter  13 , a phase number selector  14 , a phase averaging circuit  15 , a denominator register  16 , a phase variation measuring circuit  17 , a phase variation error decision circuit  18 , and a phase variation threshold register  19 .  
         [0038]    The transition detection circuits  11 ,  12  detect points of transition between the High level and the Low level in the received data stream RD 1  (that is, rising and falling edges of the pulses in the pulse train constituting the received data stream RD 1 ): transition detection circuit  11  detects transitions from zero to one (rising edges if positive logic is used, so that the High level is one and the Low level is zero); transition detection circuit  12  detects transitions from one to zero (falling edges if positive logic is used).  
         [0039]    The functions of the transition detection circuits  11 ,  12  may be realized in various types of circuit structures. For example, the circuit structure shown in FIG. 3 may be used. The transition detection circuits  11  and  12  may have the same circuit structure; FIG. 3 will be described below as showing mainly transition detection circuit  11 .  
         [0040]    In FIG. 3, the transition detection circuit  11  includes a sampling circuit  30 , a holding circuit  31 , a comparison circuit  32 , and a threshold setting circuit  33 .  
         [0041]    The sampling circuit  30  samples the received data stream RD 1  by using a high-speed clock signal HC 1 , and outputs the sampled values or sampled potentials SP. The clock rate (the number of clock pulses per unit time) should be adequately higher than the data rate of the received data stream RD 1  (the number of data pulses per unit time). In the first embodiment, the frequency of the high-speed clock signal HC 1  is, for example, eight times the data rate of the received data stream RD 1 .  
         [0042]    This means, as can be seen in the NB 1  and RD 1  waveforms in FIG. 4, that one rising edge or one falling edge is generally detected during an interval in which the received data stream RD 1  is sampled eight times. In FIG. 4, a Non Return to Zero (NRZ) channel code is used for the received data stream RD 1 .  
         [0043]    The holding circuit  31  holds the sampled value SP, outputs the held value or held level HL, and varies the held value HL whenever the sampling circuit  30 , operating according to the high-speed clock signal HC 1 , supplies a new sampled value SP.  
         [0044]    The threshold setting circuit  33  outputs a preset threshold value THS.  
         [0045]    The comparison circuit  32  compares the threshold value THS with the held value HL. The threshold value THS is lower than the High level of the data pulses, and higher than the Low level, with adequate margins between the High, THS, and Low levels.  
         [0046]    Since the purpose of the transition detection circuit  11  is to detect rising edges in the received data stream RD 1 , when the held value HL goes above the threshold value THS, the comparison circuit  32  outputs a (rising) transition detection pulse VT 1 . In the transition detection circuit  12 , the purpose of which is to detect falling edges, a (falling) transition detection pulse VT 2  is output from the comparison circuit  32  when the held value HL goes below the threshold value THS.  
         [0047]    The two transition-detection circuits  11 ,  12  may have the same general structure except for the comparison circuit  32 . The transition detection circuits  11  and  12  may use different threshold values THS, however.  
         [0048]    The phase counter  13  in FIG. 2 receives the same high-speed clock signal HC 1  as is supplied to the transition detection circuits  11 ,  12 , and counts cyclically in the integer range from one to eight. Starting from one, the count value NB 1  is incremented (by +1) when each HC 1  clock pulse is received, until the maximum value of eight is reached, after which the count value NB 1  returns to the minimum value of one again on the next clock pulse.  
         [0049]    The phase number selector  14  receives the transition detection signals VT 1  and VT 2  output from the transition detection circuits  11 ,  12 , and the count value NB 1  output from the phase counter  13 . Each received transition detection pulse (VT 1  or VT 2 ) causes the phase number selector  14  to select and store the current count value NB 1  as a phase number (indicating the phase of an edge). This selection constitutes the operation of associating a phase number with a rising or falling edge in the received data stream RD 1 .  
         [0050]    The functions of the phase number selector  14  may be realized in various types of circuit structures. For example, the phase number selector  14  may have the circuit structure shown in FIG. 5, comprising a distribution circuit  40  and four registers  41 - 44 .  
         [0051]    Each of the registers  41 - 44  is, for example, a memory circuit comprising several parallel D-type flip-flops, having input terminals for receiving the count value NB 1  connected in parallel to the phase counter  13  and output terminals connected in parallel to the phase averaging circuit  15 . These flip-flops also receive the transition detection pulses VT 1  and VT 2  from the distribution circuit  40 . Upon being triggered by a VT 1  or VT 2  pulse, a flip-flop latches the value (one bit of the count value NB 1 ) currently received at its input terminal. The latched value is output from the output terminal of the flip-flop as one bit of a phase number, until the next VT 1  or VT 2  pulse is received and a new input value is latched. The distribution circuit  40  distributes the VT 1  and VT 2  pulses to the registers  41 - 44  in a predetermined order.  
         [0052]    The D-type flip-flops may be structured to operate in synchronization with either the rising or falling edges of the VT 1  and VT 2  pulses. A detailed description will be omitted, as edge-triggered D-type flip-flops are well known.  
         [0053]    In FIG. 4, the count value NB 1  indicating the phase number is an integer ranging from one to eight, but this integer may be represented in the registers  41 - 44  as follows. If D indicates decimal notation and B indicates binary notation, then 1D may be represented as 000B, 2D as 001B, and 8D as 111B, so that the decimal range 1D-8D becomes the binary range 000B-111B, in which case each of the registers  41 - 44  can be a three-bit register (comprising three D-type flip-flops).  
         [0054]    The distribution circuit  40  distributes the transition detection pulses VT 1  and VT 2  output from the transition detection circuits  11 ,  12  to the registers  41 - 44  one by one in a predetermined order, following the pulse output sequence. The predetermined order may be a cyclical order: for example, the distribution circuit  40  may send the first four transition detection pulses to registers  41 ,  42 ,  43 ,  44  in this order, and send the next transition detection pulse to register  41  again.  
         [0055]    As rising edges alternate with falling edges in the received data stream RD 1 , if the distribution circuit  40  distributes the transition detection pulses VT 1  and VT 2  to the registers  41 - 44  as described above, the registers  41 - 44  will receive count values NB 1  indicating the phases of rising and falling edges alternately. The count values NB 1  latched in the registers  41 - 44  will always represent four consecutive edges in the received data stream RD 1  (for example, edges EG 11 -EG 14  in FIG. 4).  
         [0056]    If the count values NB 1  latched in the registers  41 - 44  are denoted NB 11 -NB 14 , respectively, then at a given time the count values NB 11  and NB 13  may indicate, for example, phase number four for rising edges EG 11  and EG 13 , and the count values NB 12  and NB 14  may indicate, for example, phase numbers five and seven for falling edges EG 12  and EG 14 , as is shown in FIG. 4.  
         [0057]    Needless to say, the count values NB 11 -NB 14  latched in the registers  41 - 44  may change as new transition detection pulses VT 1  and VT 2  are supplied from the distribution circuit  40 .  
         [0058]    The phase averaging circuit  15  receives the transition detection pulse (VT 1  or VT 2 ) supplied from the distribution circuit  40  to register  44  as a timing signal TM. The timing signal TM tells the phase averaging circuit  15  when to start the averaging operation described below.  
         [0059]    The phase averaging circuit  15  in FIG. 2 reads the count values NB 11 -NB 14  latched in the four registers  41 - 44  as phase numbers SL, executes an averaging operation according to the following equation (1), and outputs a phase average value AV 1 .  
           AV 1=reference value+(difference-1+difference-2+difference-3)/number of counts   (1)  
         [0060]    The reference value in this equation is the phase number SL given by the count value NB 11  latched in register  41 . The three differences are the differences between the reference value and the phase numbers SL given by the three count values NB 12 -NB 14  latched in registers  42 - 44 . In the averaging operation performed at the timing signal TM generated by edge EG 14  in FIG. 4, for example, the reference value (REF) is the phase number of edge EG 11  (NB 11 =4), and difference-1 is the difference between this reference value and the phase number of edge EG 12  (NB 12 =5). Difference-1 is accordingly equal to one (5−4=1).  
         [0061]    In the ideal case without any jitter (hence with no bit drop-outs or drop-ins), the received data stream RD 1  should have the waveform labeled as expected data in FIG. 4, in which all rising and falling edges (EL 11 -EL 19 ) have the same phase number (e.g., 5) as the first edge (EL 11 ). This is possible because the frequency of the high-speed clock signal HC 1  is an integer multiple of the data rate of the received data stream RD 1  (the data rate is the frequency of the data clock in FIG. 4).  
         [0062]    In an actual transmission channel, however, jitter generally causes the phase numbers of the edges to vary, as illustrated by the RD 1  waveform in FIG. 4. If the jitter is moderate and the phase variation is not too large, the data sampling points at the rising edges in the data clock are still located near the middle of the High and Low bit intervals in the received data stream RD 1 , so accurate samples are obtained and the correct ‘1’ and ‘0’ data values are recognized. In this case, the communication apparatus  20  can stay in synchronization with the transmitting communication device, thereby maintaining proper communication. If the jitter is excessive and the phase variation is large, however, bit drop-ins or drop-outs may occur.  
         [0063]    The phase average value AV 1  indicates the average jitter in the transmission channel PL over an interval including four edges. The phase variation error detection circuit  10  in the first embodiment can detect excessive jitter regardless of whether it leads to a bit drop-in or drop-out.  
         [0064]    The phase averaging circuit  15  must first be activated by the trigger signal TR 1  shown in FIG. 4, which is a timing signal that starts the phase jitter measurement process. After receiving a rising edge of the trigger signal TR 1 , the phase averaging circuit  15  is ready to start the averaging operation at any time. The averaging operation actually starts when the timing signal TM is supplied.  
         [0065]    Incidentally, the phase averaging circuit  15  can be structured so that only one of the two signals, either the trigger signal TR 1  or the timing signal TM, is necessary. If the effect of jitter is considered, use of the timing signal TM, which indicates that the count values NB 11 -NB 14  for the four consecutive edges needed for an averaging operation are latched in the registers  41 - 44 , leads to efficient implementations of the phase number selector  14  and the phase averaging circuit  15 .  
         [0066]    The equation (1) above is given to facilitate understanding of the averaging operation. In actual implementations, the calculations shown in the equation (1) can be optimized for more efficient processing by hardware or software in the phase averaging circuit  15 . For example, subtracting the reference value three times from the sum of the phase numbers in registers  42 - 44 , instead of adding three differences obtained one by one, may lead to higher processing efficiency (or space efficiency), because the three differences do not have to be latched temporarily during the averaging process.  
         [0067]    The number of counts AR 1  (AR 1 =4 in FIG. 4) used as a denominator in equation (1) is prestored in the denominator register  16 . The phase averaging circuit  15  can read the number of counts AR 1  from the denominator register  16  at any time.  
         [0068]    The phase variation measuring circuit  17 , which receives the phase average value AV 1  from the phase averaging circuit  15 , is a subtractor that detects and outputs a phase variation value PV 1  as the absolute value of the difference between two consecutive phase average values AV 1 .  
         [0069]    The phase variation error decision circuit  18  compares the phase variation value PV 1  with a threshold value TH 1  (TH 1 =2 in FIG. 4) supplied from the phase variation threshold register  19 . If the phase variation value PV 1  is greater than the threshold value TH 1 , the phase variation error decision circuit  18  activates the phase error detection signal ED 3 . The threshold value TH 1  thus defines the maximum allowable phase variation PV 1 . The threshold value TH 1  is prestored in the phase variation threshold register  19 .  
         [0070]    The functions of the phase averaging circuit  15 , phase variation measuring circuit  17  and phase variation error decision circuit  18  can be realized in hardware with simple combinatorial logic circuits, or in software using general-purpose registers, a RAM work area, and a general-purpose operation unit.  
         [0071]    The data clock in FIG. 4 is, in a narrow sense, a decoding clock, since the received data stream RD 1  is sampled at the rising edges in the data clock to identify ‘1’ and ‘0’ data values. Constituent elements  11 - 13  and  11 - 19  in the phase variation error detection circuit  10  in FIG. 2 operate according to the high-speed clock signal HC 1 , and do not need to receive the data clock. If necessary, however, the data clock may be supplied to elements  15 - 18 .  
         [0072]    The operation in the first embodiment of the phase variation error detection circuit, having the structure described above, will be described below with reference to the timing waveforms in FIG. 4.  
         [0073]    The phase variation error detection circuit  10  starts operating when the trigger signal TR 1  is supplied to the phase averaging circuit  15  while, for example, the RD 1  waveform in FIG. 4 is being received.  
         [0074]    In the communication apparatus  20  shown in FIG. 1, the phase variation error detection circuit  10 , CRC processing circuit  21 , and FEC processing circuit  22  may always operate concurrently. Alternatively, normally only the CRC processing circuit  21  and FEC processing circuit  22  may operate, the phase variation error detection circuit  10  being triggered when communication quality is degraded.  
         [0075]    In any case, the phase variation error detection circuit  10  starts effective operation when the trigger signal TR 1  is supplied. Constituent elements  11 - 14  in the phase variation error detection circuit  10  may also operate before the trigger signal TR 1  is supplied to the phase averaging circuit  15 .  
         [0076]    In FIG. 4, time flows from left to right. Accordingly, the transition detection circuits  11 ,  12  receive edges EG 11 -EG 19  in the data stream RD 1  in this order. When rising edges EG 11 , EG 13 , EG 15  etc. are detected, transition detection circuit  11  outputs a transition detection pulse VT 1 ; when falling edges EG 12 , EG 14 , EG 16  etc. are detected, transition detection circuit  12  outputs a transition detection pulse VT 2 .  
         [0077]    As illustrated by the RD 1  waveform in FIG. 4, the first detected edge is rising-edge EG 11 , at which a transition detection pulse VT 1  is supplied from the transition detection circuit  11  to the phase number selector  14 . Following the predetermined order, the distribution circuit  40  in the phase number selector  14  distributes this VT 1  pulse to register  41 , so the count value NB 1  (phase number  4  in FIG. 4) output from the phase counter  13  at this instant is latched in register  41  as count value NB 11 . The phase number given by the count value NB 11  is the reference value in the averaging operation in equation (1).  
         [0078]    The next detected edge is a falling edge EG 12 , at which a transition detection pulse VT 2  is supplied from the transition detection circuit  12  to the phase number selector  14 . Following the same predetermined order, the distribution circuit  40  in the phase number selector  14  distributes this VT 2  pulse to register  42 , so the count value NB 1  (phase number  5  in FIG. 4) output from the phase counter  13  at this instant is latched in register  42  as count value NB 12 . The difference between the reference value and the phase number given by count value NB 12  is difference-1 in the averaging operation in equation (1).  
         [0079]    Similarly, when transition detection pulses VT 1  and VT 2  for edges EG 13  and EG 14  are supplied from the transition detection circuits  11 ,  12 , the distribution circuit  40  distributes them to registers  43 ,  44 , still following the predetermined order. The count values NB 1  in the phase counter  13  at the times of these two edges are latched in registers  43 ,  44  as count values NB 13  and NB 14  (phase numbers  4  and  7  in FIG. 4).  
         [0080]    The fourth transition detection pulse (VT 2 ) is supplied simultaneously to register  44  and to the phase averaging circuit  15 . The phase averaging circuit  15  receives this VT 2  pulse as a timing signal TM, recognizes that the count values NB 11 -NB 14  of the four edges needed for execution of the averaging operation in equation (1) have been latched in the registers  41 - 44 , reads the count values NB 11 -NB 14  as phase numbers SL, executes the averaging operation, and outputs the calculated phase average value AV 1 .  
         [0081]    The phase numbers of the count values NB 11 -NB 14  are:  
         (NB 11 , NB 12 , NB 13 , NB 14 )=(4, 5, 4, 7)  
         [0082]    In equation (1), these values become:  
         4+(1+0+3)/4=5  
         [0083]    Accordingly, the phase average value AV 1  is 5. This phase average value AV 1  (=5) is the first phase average value supplied to the phase variation measuring circuit  17 , so the phase variation measuring circuit  17  merely stores the phase average value AV 1 .  
         [0084]    For the four edges EG 15 - 18  following edges EG 11 - 14 , the operation described above is repeated in the transition detection circuits  11 ,  12 , phase counter  13 , phase number selector  14 , and phase averaging circuit  15 .  
         [0085]    As can be seen from the NB 1  and RD 1  waveforms in FIG. 4, the phase numbers of the count values NB 11 -NB 14  for edges EG 15 -EG 18  differ from the phase numbers of the count values for edges EG 11 -EG 14 . NB 11 -NB 14  are now given as follows.  
         (NB 11 , NB 12 , NB 13 , NB 14 )=(6, 6, 2, 2)  
         [0086]    Equation (1) now becomes:  
         6+(0+4+4)/4=8  
         [0087]    Accordingly, the phase average value AV 1  is  8 . When this phase average value AV 1  (=8) is supplied from the phase averaging circuit  15  to the phase variation measuring circuit  17 , the phase variation measuring circuit  17  calculates the difference between it and the phase average value AV 1  (=5) for the preceding four edges EG 11 -EG 14 , and outputs the difference as a phase variation value PV 1  (PV 1 =8−5=3).  
         [0088]    When the phase variation value PV 1  (=3) is supplied to the phase variation error decision circuit  18 , the phase variation error decision circuit  18  compares it with the threshold value TH 1  (=2) stored in the phase variation threshold register  19 . In this case, the phase variation value PV 1  is greater than the threshold value TH 1 , so the phase variation error decision circuit  18  activates the phase error detection signal ED 3  by driving it to the High logic level as shown in FIG. 4, thereby informing the error detection control circuit  23  of a synchronization error. This synchronization error is accompanied by a bit drop-in just before edge EG 17 .  
         [0089]    As described above, when the error detection control circuit  23  in FIG. 1 receives the active phase error detection signal ED 3 , the error detection control circuit  23  ignores the outputs ED 1  and ED 2  from the CRC processing circuit  21  and FEC processing circuit  22  and outputs a retransmission control signal RS 1 . The retransmission request generator  24  then sends a retransmission request signal RC 1 .  
         [0090]    When the phase error detection signal ED 3  is activated, the operations in the phase variation error detection circuit  10  may either stop or continue. If the operations continue without stopping, then when the next phase average value AV 1  is supplied, the phase variation measuring circuit  17  operates in the same way, subtracting the preceding phase average value AV 1  (=8) to obtain a difference PV 1  for comparison with the threshold value TH 1 .  
         [0091]    The number of consecutive edges used in the averaging operation can be increased or decreased by varying the number of counts AR 1 .  
         [0092]    According to the first embodiment, the phase variation error detection circuit can accurately detect synchronization errors that have a high probability of producing wrong indications from the CRC processing circuit  21  and FEC processing circuit  22 . The phase variation error detection circuit can thereby limit the effect of the wrong indications, eliminate reliability gaps in error detection, maintain communication quality, and assure communication reliability.  
         [0093]    The synchronization errors that the phase variation error detection circuit in the first embodiment can detect include not only the bit drop-outs and drop-ins described above but also excessive jitter.  
       SECOND EMBODIMENT  
       [0094]    Referring to FIG. 6, the second embodiment replaces the phase variation error detection circuit of the first embodiment with a pulse width error detection circuit  50 . The differences between the pulse width error detection circuit in the second embodiment and the phase variation error detection circuit in the first embodiment will be described below.  
         [0095]    [0095]FIG. 7 shows an exemplary structure of the pulse width error detection circuit in the second embodiment, using the same reference characters as in FIG. 2 for similar elements. The pulse width error detection circuit  50  includes several of the same circuit elements as the phase variation error detection circuit  10  in the first embodiment, but differs from the phase variation error detection circuit by replacing the phase averaging circuit  15  with a pulse width measuring circuit  55 , the phase variation error decision circuit  18  with a pulse width error decision circuit  58 , and the phase variation threshold register  19  with a pulse width threshold register  59 , and by eliminating the denominator register  16  and phase variation measuring circuit  17 .  
         [0096]    The pulse width error detection circuit  50  in the second embodiment is used in the communication apparatus  20  in the same way as the phase variation error detection circuit  10  in the first embodiment.  
         [0097]    [0097]FIG. 8 is a timing diagram illustrating the operation of the second embodiment. The received data stream RD 1  uses the same NRZ channel code as in the first embodiment and the high-speed clock signal HC 1  has the same frequency, equal to eight times the data rate, but for purposes of illustration, the RD 1  waveform in FIG. 8 differs from the RD 1  waveform in FIG. 4. The RD 1  waveforms in FIGS. 4 and 8 may be considered to represent different sections of the same RD 1  data stream.  
         [0098]    Since the RD 1  waveforms in FIGS. 4 and 8 differ, the phase numbers SL of the rising and falling edges differ.  
         [0099]    Whereas the phase averaging circuit  15  in the first embodiment takes a phase average value AV 1  over four consecutive edges, the pulse width measuring circuit  55  in the second embodiment determines the difference between two consecutive edges. This difference is the width of a High or Low pulse, that is, the duration of a high or low interval in the RD 1  waveform.  
         [0100]    The phase averaging circuit  15  in the first embodiment has to wait for the count values of four consecutive edges to be latched in registers  41 - 44  before executing an averaging operation, but the pulse width measuring circuit  55  in the second embodiment can determine a High or Low pulse width when any two consecutive edges have been latched.  
         [0101]    The nominal duty cycle in FIG. 8 is 50%, as illustrated by the expected data waveform. The basic Low pulse width and the High pulse width are theoretically the same, so synchronization errors can be detected without discriminating between the two types of pulses. To calculate and output a High or Low pulse width, the pulse width measuring circuit  55  only has to determine the difference between the latched phase numbers of any two consecutive edges.  
         [0102]    Therefore, the phase number selector  14  in the second embodiment needs only two registers, instead of four registers  41 - 44 . Whenever a new phase number is latched in either one of the two registers, the phase number selector  14  executes a pulse width measurement according to equation (2) below and outputs the measured pulse width PW 1 . As an exception, the first time a new phase number is latched after operation starts, the pulse width measurement is not performed, because the phase number selector  14  has to wait until a second phase number has been latched.  
         PW 1 =new phase number−preceding phase number+N×(maximum phase number)   (2)  
         [0103]    The maximum phase number in this equation is eight, the maximum value in the range from one to eight of the count value NB 1 . The preceding phase number is the phase number latched earlier in one of the two registers in the phase number selector  14 ; the new phase number is the phase number latched later in the other one of the two registers. N is the number of times the phase counter  13  is reset to one between the latching of these two phase numbers.  
         [0104]    When the phase number (4) of the first edge EG 21  and the phase number (5) of the second edge EG 22  in the received data stream RD 1  shown in FIG. 8 are latched in the two registers in this order as a preceding phase number and a new phase number, for example, equation (2) becomes:  
         PW 1 =5−4+(1×8)=9  
         [0105]    This pulse width PW 1  (=9) is the first High pulse width PW 1  in FIG. 8.  
         [0106]    Similarly, when the phase number (4) of the third edge EG 23  is latched in the register in which the phase number (4) of the first edge EG 21  was latched earlier, the phase number (4) of the third edge EG 23  becomes the new phase number, and the phase number (5) of the second edge EG 22 , which was formerly the new phase number, becomes the preceding phase number. Equation (2) now becomes:  
         PW 1 =4−5+(1×8)=7  
         [0107]    This pulse width PW 1  (=7) is the first Low pulse width PW 1  in FIG. 8.  
         [0108]    Whenever a new phase number is latched in either one of the registers, the operation described above is repeated: the pulse width is calculated according to equation (2) and output as pulse width PW 1 . High and Low pulse widths PW 1  are obtained alternately as shown in FIG. 8.  
         [0109]    In the second embodiment, the threshold value TH 2  that defines the minimum allowable pulse width is stored in the pulse width threshold register  59 , and the pulse width error decision circuit  58  compares the pulse width PW 1  obtained by the pulse width measuring circuit  55  with the threshold value TH 2 . When a pulse width PW 1  less than the threshold value TH 2  is observed, the pulse width error decision circuit  58  outputs a pulse width error detection signal ED 4 , indicating a synchronization error, to the error detection control circuit  23 .  
         [0110]    In the general case, the pulse width error detection circuit may include structures for storing a threshold value defining a maximum allowable pulse width PW 1  and outputting a pulse width error detection signal when a pulse width PW 1  exceeding this threshold value is obtained. In the second embodiment, however, the received data stream RD 1  uses an NRZ channel code, so long pulses may occur normally (theoretically, the pulse width PW 1  may be infinitely long). The pulse width error detection circuit therefore uses only a threshold value TH 2  defining the minimum pulse width PW 1 .  
         [0111]    If the received data stream RD 1  is encoded using a return-to-zero (RZ) channel code, for example, then the threshold value TH 2  may define either a maximum or a minimum allowable pulse width PW 1 .  
         [0112]    In the second embodiment, the threshold value TH 2  that defines the minimum allowable pulse width PW 1  is five, as shown in FIG. 8. Accordingly, when a pulse width PW 1  less than five is obtained, the pulse width error detection signal ED 4  is activated.  
         [0113]    In FIG. 8, the pulse width error detection signal ED 4  is activated twice, during periods EP 1  and EP 2 . The first activation (EP 1 ) is due to a duty cycle error: the Low pulse width between edges EG 24  and EG 25  (PW 1 =4) is less than the threshold value (TH 2 =5). The second activation (EP 2 ) is due to noise, which appears as a narrow High pulse between edges EG 27  and EG 28  (PW 1 =1). Although this noise pulse is not sampled in FIG. 8, if it coincided with a rising edge of the data clock, it would be sampled, causing a data error. The detected synchronization errors (EP 1  and EP 2 ) do not by themselves cause either a bit drop-in or drop-out, but they are symptomatic of unstable channel conditions that can easily lead to a bit drop-in or drop-out, as in fact happens shortly after the second synchronization error (EP 2 ) is signaled, when falling edge EG 30  is delayed.  
         [0114]    When the pulse width error detection circuit  50  activates the pulse width error detection signal ED 4 , the error detection control circuit  23  may operate in the same way as when a phase error detection signal ED 3  is output in the first embodiment, by ignoring the outputs ED 1  and ED 2  of the CRC and FEC processing circuits and activating the retransmission control signal RS 1 .  
         [0115]    Although the pulse width error detection circuit in the second embodiment differs from the phase variation error detection circuit in the first embodiment, it produces similar effects. Since the pulse width error detection circuit in the second embodiment can determine whether the pulse width between two consecutive edges is correct or not, however, the pulse width error detection circuit can detect synchronization errors more rapidly than can the phase variation error detection circuit in the first embodiment, which requires four edges to obtain a phase average value AV 1  and outputs a difference between two phase average values.  
         [0116]    As described above, even under conditions in which existing methods of error control (such as the CRC and FEC methods) are likely to give wrong indications, the present invention can override these wrong indications, thereby maintaining communication quality and assuring communication reliability.  
         [0117]    In the first embodiment, the phase averaging circuit  15  executed an averaging operation on the count values of four consecutive edges. If rapid detection of synchronization errors is not essential, however, it is permissible to skip edges. Substantially the same effect as described above is obtained if the averaging operation is executed on the count values of every other edge (ignoring edges EG 12 , EG 14 , EG 16  in FIG. 4), for example, or every third edge. Edges may also be skipped in the second embodiment.  
         [0118]    The communication apparatus  20  may include both the phase variation error detection circuit  10  of the first embodiment and pulse width error detection circuit  50  of the second embodiment. In this case, a synchronization error may be recognized from, for example, the output of an error detection signal ED 3  or ED 4  from either one of the phase variation error detection circuit  10  or the pulse width error detection circuit  50 .  
         [0119]    In the second embodiment, the duty cycle in the received data stream RD 1  is 50%. If the duty cycle is not 50%, in other words, if the High pulse width and the Low pulse width theoretically differ, the pulse width measuring circuit  55  may discriminate between the two types of pulses, and calculate and output separate High and Low pulse widths. Two threshold values are then required, one for the High pulse width and one for the Low pulse width. When a High pulse width PW 1  is calculated and output, the pulse width error decision circuit  58  compares it with the threshold value for the High pulse width; when a Low pulse width PW 1  is calculated and output, the pulse width error decision circuit  58  compares it with the threshold value for the Low pulse width.  
         [0120]    There may be two modes of communication between the transmitting communication apparatus and the receiving communication apparatus  20 : a first communication mode emphasizing transmission speed more than transmission quality, and a second communication mode emphasizing transmission quality more than transmission speed. In this case, the following mode selection scheme may be effective: the frequency of activation of phase error detection signals ED 3  and/or pulse width error detection signals ED 4  is compared with a predetermined threshold value; if the frequency is less than the threshold value, communication is carried out in the first communication mode; if the frequency is greater than the threshold value, the channel PL is considered to be unstable, and the mode is switched from the first communication mode to the second communication mode to obtain improved transmission quality. After the mode is switched to the second communication mode, the frequency of activation of signals ED 3  and/or ED 4  continues to be monitored and compared with the threshold value, and if the frequency returns to a value less than the threshold value, the mode is returned to the first communication mode.  
         [0121]    The frequency of activation of signals ED 3  and/or ED 4  may be detected and compared with a threshold value by either hardware or software. Since it is not necessary to detect the frequency of activation of the ED 3  and/or ED 4  signals as often as it is necessary to perform the averaging operation and pulse width calculation operation, the activation frequency detection function can normally be realized in software. If this function can be realized in either hardware or software, then software is generally preferable for flexibility and extensibility.  
         [0122]    The invention as a whole is realized in hardware in the description above, but the invention as a whole can be also realized in software.  
         [0123]    Those skilled in the art will recognize that further variations are possible within the scope of the invention, which is defined in the appended claims.

Technology Category: h