Abstract:
A method ( 70 ) of operating a wireless receiver (UST). The method receives a wireless communicated signal, wherein the signal comprises asymmetrically spaced synchronization channel components. The method also defines ( 72 ) a set of signals from the communicated signal, wherein the set spans a number of equal duration time slots and comprises at least a first synchronization channel component and a second synchronization channel component. The method also forms ( 76 ) a first signal combination by combining a first portion of the set of signals with a second portion of the set of signals, and it forms ( 78 ) a second signal combination by combining a third portion of the set of signals with a fourth portion of the set of signals. Finally, the method detects ( 80, 82, 84 ) a location of the first synchronization channel component and a location of the second synchronization channel component in response to at least one of the first and second signal combinations.

Description:
CROSS-REFERENCES TO RELATED APPLICATIONS 
     This application claims the benefit, under 35 U.S.C. §119(e)(1), of U.S. Provisional Application No. 60/157,782 (TI-29754PS), filed Oct. 5, 1999. 
    
    
     STATEMENT REGARDING FEDERALLY SPONSORED RESEARCH OR DEVELOPMENT 
     Not Applicable. 
     BACKGROUND OF THE INVENTION 
     The present embodiments relate to wireless communications systems and are more particularly directed to synchronizing a receiver to a transmitter in response to unevenly time-spaced synchronization signals between the transmitter and receiver. 
     Wireless communications have become prevalent in business, personal, and other applications, and as a result the technology for such communications continues to advance in various areas. One such advancement includes the use of spread spectrum communications, including that of code division multiple access (“CDMA”). In such communications, a user station (e.g., a hand held cellular phone) communicates with a base station, where typically the base station corresponds to a “cell.” More particularly, CDMA systems are characterized by simultaneous transmission of different data signals over a common channel by assigning each signal a unique code. This unique code is matched with a code of a selected user station within the cell to determine the proper recipient of a data signal. 
     CDMA continues to advance along with corresponding standards that have brought forth a next generation wideband CDMA (“WCDMA”). WCDMA includes alternative methods of data transfer, one being time division duplex (“TDD”) and another being frequency division duplex (“FDD”). The present embodiments apply by way of example to TDD and it is further introduced here. TDD data are transmitted as quadrature phase shift keyed (“QPSK”) symbols in data packets of a predetermined duration or time slot within a frame. By way of illustration, such a prior art frame FR is shown in FIG.  1 . Frame FR is a fixed duration, such as 10 milliseconds long, and it is divided into equal duration slots. In the past it was proposed in connection with the 3G standard that the number of these equal duration slots equals 16, while more recently the standard has been modified such that each frame includes 15 equal duration slots. Each of the 15 slots has a duration of approximately 667 microseconds (i.e., 10/15 milliseconds). For the sake of reference, 15 such slots are shown in FIG. 1 as SL 1  through SL 15 , and slots SL 1  and SL 8  are expanded by way of examples to illustrate additional details. Within each TDD frame FR, bi-directional communications are permitted, that is, one or more of the slots within a frame may correspond to communications from a base station to a user station while other slots in the same frame may correspond to communications from a user station to a base station. 
     To accomplish the communication from a user station to a base station the user station must synchronize itself to a base station. This synchronization process is sometime referred to as acquisition of the synchronization channel and is often performed in various stages. The synchronization channel, shown in expanded form as SCH in FIG. 1, includes two codes, namely, a primary synchronization code (“PSC”) and a secondary synchronization code (“SSC”), as transmitted from a base station. The PSC is presently a 256 length pseudo-noise (“PN”) code. As shown in frame FR of FIG.  1  and by way of example of one TDD mode, both the PSC and SSC are included and transmitted in two slots for frame FR, namely, the first slot SL 1  and the eighth slot SL 8 . Moreover, for each slot SL 1  and SL 8  containing the PSC and SSC, those codes may be offset by some period of time, T offset , within the slot. Under the present standard, T offset  is the same for both the PSC and the SSC. However, in alternative implementations, the PSC and SSC may be offset from one another, in which case it may be stated that the PSC has an offset T offset1  from the slot boundary and the SSC has an offset T offset2  from the slot boundary. For the sake of an example in the remainder of this document, assume that T offset1 =T offset2 . The PSC is transmitted with the same encoded information for numerous base stations while each base station group transmits a unique SSC. The actual base station is identified from the third stage of the synchronization process, which may involve correlating with the midamble (in TDD) or long code (in FDD) from the base station transmissions depending on the type of communication involved. The synchronization process typically occurs when a user station is initially turned on and also thereafter when the user station, if mobile, moves from one cell to another, where this movement and the accompanying signal transitions are referred to in the art as handoff. Synchronization is required because the user station does not previously have a set timing with respect to the base station and, thus, while slots are transmitted with respect to frame boundaries by the base station, those same slots arrive at the user station while the user station is initially uninformed of the frame boundaries among those slots. Consequently, the user station typically examines one frame-width of information (i.e., 15 slots), and from that information the user station attempts to determine the location of the actual beginning of the frame (“BOF”), as transmitted, where that BOF will be included somewhere within the examined frame-width of information. Further in this regard, the PSC is detected in a first acquisition stage, which thereby informs the user station of the periodic timing of the communications, and which may further assist as detailed later to identify the BOF. The SSC is detected in a later acquisition stage, which thereby informs the user station of the data location within the frame. Further, once the user station has detected a unique base station SSC, the user station also may identify the long code/midamble that is also unique to, and transmitted by, the base station, and following that determination a specific long code/midamble from that group is ascertained and which is then usable by the user station to demodulate data received in frames from the base station. 
     Returning now to frame FR in general and by way of particular focus to the preferred embodiments described later as well as the state of the art, note that each SCH is asymmetrically located within frame FR. More particularly, six non-synchronization slots follow the SCH in slot SL 1  while seven non-synchronization slots follow the SCH in slot SL 8 . In other words, the location of the SCH (i.e., codes PSC and SSC) is unevenly spaced within frame FR. This asymmetry poses an issue to be addressed by the preferred embodiments, which is further appreciated by first looking to the previous 3G standard as discussed below. 
     Under the prior 3G standard, where recall there were 16 slots in a frame, then the SCH, as transmitted, also was located in the first and eighth slots of the frame. In order to locate these two SCH occurrences in the prior art, a user station could continuously sample 16 slots of received information and perform a PSC correlation on those samples, and by averaging those correlations to eliminate noise the synchronization channel would appear at the same slot locations within the average. For example, this technique may be implemented by applying the received information to a matched filter having the 256 length PN code of the PSC as coefficients to the filter. In this approach, the average peaks over time of those correlations correspond to the location of the synchronization channel within the collected information. However, while this approach locates the two SCH slots as corresponding to peaks within a sample of 16 slots, there is still an ambiguity whether a given peak corresponds to the originally-transmitted first or eighth slot within the frame. Thus, additional processing is required to resolve this ambiguity. Further, with the change of the 3G standard to an odd number (e.g., 15) of slots per frame, the above-described asymmetry is created. Thus, due to these factors, and also due to the lack of known timing between a transmitter and a receiver, the prior art approach does not provide a workable PSC acquisition for present applications. 
     In view of the above, there arises a need to provide an approach for acquisition of the PSC located asymmetrically within a wireless communication frame, as is achieved by the preferred embodiments discussed below. 
     BRIEF SUMMARY OF THE INVENTION 
     In the preferred embodiment, there is a method of operating a wireless receiver. The method receives a wireless communicated signal, wherein the signal comprises asymmetrically spaced synchronization channel components. The method also defines a set of signals from the communicated signal, wherein the set spans a number of equal duration time slots and comprises at least a first synchronization channel component and a second synchronization channel component. The method also forms a first signal combination by combining a first portion of the set of signals with a second portion of the set of signals, and it forms a second signal combination by combining a third portion of the set of signals with a fourth portion of the set of signals. Finally, the method detects a location of the first synchronization channel component and a location of the second synchronization channel component in response to at least one of the first and second signal combinations. Other circuits, systems, and methods are also disclosed and claimed. 
    
    
     BRIEF DESCRIPTION OF THE SEVERAL VIEWS OF THE DRAWING 
     FIG. 1 illustrates a prior art frame FR divided into an odd number of equal-duration slots. 
     FIG. 2 illustrates a diagram of a cellular communications system  10  by way of a contemporary code division multiple access (“CDMA”) or wideband CDMA (“WCDMA”) example in which the preferred embodiments operate. 
     FIG. 3 illustrates a first preferred embodiment of user station UST from FIG. 2 in greater detail. 
     FIG. 4 illustrates, in greater detail, a block diagram of stage  1  acquisition block  24  from FIG.  3 . 
     FIG. 5 illustrates a method  70  of operation of stage  1  acquisition block  24  and the stage  2  acquisition of block  26  of FIG.  4 . 
     FIG. 6 illustrates a first example of signals processed according to the preferred embodiment method of FIG.  5 . 
     FIG. 7 illustrates a second example of signals processed according to the preferred embodiment method of FIG.  5 . 
     FIG. 8 illustrates a third example of signals processed according to the preferred embodiment method of FIG.  5 . 
     FIG. 9 illustrates an alternative method  70 ′ of operation of stage  1  acquisition block  24  and the stage  2  acquisition of block  26  of FIG.  4 . 
    
    
     DETAILED DESCRIPTION OF THE INVENTION 
     FIG. 1 was described in the Background Of The Invention section of this document and the reader is assumed familiar with the concepts described in that section. 
     FIG. 2 illustrates a diagram of a cellular communications system  10  by way of a contemporary code division multiple access (“CDMA”) or wideband CDMA (“WCDMA”) example in which the preferred embodiments operate. Within system  10  are shown two base stations BST 1  and BST 2 . Each base station BST 1  and BST 2  includes a respective antenna AT 1  and AT 2  from which each may transmit or receive CDMA signals. The general area of intended reach of each base station defines a corresponding cell; thus, base station BST 1  is intended to generally communicate with cellular devices within Cell  1  while base station BST 2  is intended to generally communicate with cellular devices within Cell  2 . Of course, some overlap between the communication reach of Cells  1  and  2  exists by design to support continuous communications should a communication station move from one cell to the other. Indeed, further in this regard, system  10  also includes a user station UST, which is shown in connection with a vehicle V to demonstrate that user station UST is mobile. In addition, by way of example user station UST includes a single antenna ATU for both transmitting and receiving cellular communications. 
     In some respects, system  10  may operate according to known general techniques for various types of cellular or other spread spectrum communications, including CDMA communications. Such general techniques are known in the art and include the commencement of a call from user station UST and the handling of that call by either or both of base stations BST 1  and BST 2 . Other techniques are ascertainable by one skilled in the art. 
     One aspect that is particularly relevant to the present inventive scope relates to synchronization of user station UST with respect to a base station BST 1  or BST 2  (or still others not shown). Such synchronization may occur either at start up or during handoff, which occurs when user station UST moves from one cell to another. In either of these cases or possibly others, the preferred embodiment relates to primary synchronization code (“PSC”) transmissions by base stations BST 1  and BST 2  and the detection of that code by user station UST. Once the PSC is detected, other acquisition stages may be performed, such as acquiring the secondary synchronization code (“SSC”), the long code group, and the particular long code/midamble corresponding to the specific base station, and then demodulating data from the base station using the ascertained base station long code. Given the preceding, the preferred embodiments are directed to improving the acquisition of a PSC from a base station by a user station, as further detailed below. 
     FIG. 3 illustrates a first preferred embodiment of user station UST in greater detail, and in which a preferred method for synchronization channel acquisition is implemented as further discussed below. By way of introduction, user station UST is shown in block diagram form where given the following discussion one skilled in the art may ascertain various different circuits and combined software and/or firmware techniques for implementing the blocks of user station UST. Further, the various blocks shown are separated to facilitate an understanding of the preferred embodiments and not by way of limitation and, thus, one skilled in the art may add other functionality to such blocks or further subdivide or combine the functions detailed below. Also, for the sake of presentation, the following discussion first examines the functionality of each block generally with some of this functionality detailed further later. 
     Looking to various connections in FIG. 3, antenna ATU of user station UST is for receiving communications from one or more base stations (e.g., from transmit antennas AT 1  and AT 2  of base stations BST 1  and BST 2 ). Within user station UST, signals received by antenna ATU are connected to an input  20 , and input  20  is connected to an analog front end (“AFE”) block  22 . Since transmissions from each of base stations BST 1  and BST 2  are modulated over a radio frequency, AFE block  22  includes circuitry directed to those radio frequency modulated signals. For example, AFE block  22  includes a signal down converter to remove the radio frequency modulation, thereby providing a resulting analog signal. As another example, AFE block  22  includes analog-to-digital circuitry for converting the down-converted analog signal into a digital signal counterpart. This digital signal counterpart is output from AFE block  22  to a stage  1  acquisition block  24  and to a stage  2  acquisition and despreader block  26 . 
     In the preferred embodiment and as detailed in additional Figures later, stage  1  acquisition block  24  acquires the PSC in the synchronization channel embedded within the digital signal provided by AFE block  22 . As a result, stage  1  acquisition block  24  outputs a parameter POS to stage  2  acquisition and despreader block  26 . As discussed later, POS may indicate one or more positions to stage  2  acquisition and despreader block  26  depending on which of various embodiments are implemented. In any event, generally the one or more positions identified by the parameter POS are those slots in the digital signal which are perceived by block  24  to contain the synchronization channel. 
     Stage  2  acquisition and despreader block  26  receives the analog signal from AFE block  22  and completes the acquisition of the synchronization channel in response to the POS parameter from stage  1  acquisition block  24 . The completion of the synchronization channel acquisition in part responds to the POS parameter according to the preferred embodiments. Further, the completion of the acquisition of the synchronization channel also may include various of the steps associated with the prior art, such as detecting the SSC, identifying the group of long codes/midambles from the transmitting base station (i.e., BST 1  or BST 2 ), ascertaining the specific long code for that base station, and demodulating the signal in response to that specific long code. In addition, the despreading aspect of block  26  operates according to known principles, such as by multiplying the CDMA signal times the CDMA code for user station UST and thereby producing a despread symbol stream at its output and at the symbol rate. The despread signals output by block  26  are coupled by way of an example to an MRC block  28  and also to a channel estimator  30 . Channel estimator  30  determines estimated channel impulse responses based on the incoming despread symbols. Channel estimator  30  provides these estimated channel impulse responses, illustrated in FIG. 3 as α i , to MRC block  28 . Further, user station UST is shown by way of example as an open loop system; however, the present teachings also could be implemented in an alternative embodiment using closed loop technology, in which case channel estimator  30  also would output the estimates α i , or values derived from those estimates such as a weight vector W, to a feedback channel for communication back to the base station that is transmitting to user station UST. To illustrate this aspect as an option, such a feedback line is shown in FIG. 3 as a dashed line. In any event, returning to the open loop example of FIG.  3  and the communication of the channel estimates to MRC block  28 , in response MRC block  28  applies the estimates to the despread symbols received from the despreading aspect of block  26 . Further in this regard and although not separately shown, the MRC operation may be by way of various methods, such as using a rake receiver to combine each of the estimate-adjusted paths. Lastly, note that MRC block  28  is only one example of a type of processing in response to the channel estimates; in other embodiments, one can use the channel estimates and the despread signals corresponding to not just the desired user but also other users to perform multi-user detection/interference cancellation. 
     Following MRC block  28  in FIG. 3 are additional blocks/functions known in the art. For example, MRC block  28  outputs its result to a deinterleaver  32  which operates to perform an inverse of the function of an interleaver that is typically included in base stations BST 1  and BST 2 . Such an interleaver operates with respect to a block of encoded bits and shuffles the ordering of those bits so that the combination of this operation with an encoding operation exploits the time diversity of the information. For example, one shuffling technique that may be performed by such an interleaver is to receive bits in a matrix fashion such that bits are received into a matrix in a row-by-row fashion, and then those bits are output for further processing by the base station. In any event, therefore, deinterleaver  32  effectively operates in an opposite fashion to remove the effects on the symbols that were imposed by the corresponding base station interleaver. The output of deinterleaver  32  is connected to a channel decoder  34 . Channel decoder  34  may include a Viterbi decoder, a turbo decoder, a block decoder (e.g., Reed-Solomon decoding), a combination of decoding techniques, or still other appropriate decoding schemes as known in the art. In any event, channel decoder  34  further decodes the data received at its input, typically operating with respect to certain error correcting codes, and it outputs a resulting stream of decoded symbols. Indeed, note that the probability of error for data output from channel decoder  34  is far less than that before processing by channel decoder  34 . For example, under current standards, the probability of error in the output of channel decoder  34  may be between 10 −3  and 10 −6 . Finally, the decoded symbol stream output by channel decoder  34  may be received and processed by additional circuitry in user station UST, although such circuitry is not shown in FIG. 3 so as to simplify the present illustration and discussion. 
     FIG. 4 illustrates, in greater detail, a block diagram of stage  1  acquisition block  24  from FIG. 3, where the following discussion again is directed to the functionality of the blocks and with it understood that one skilled in the art may implement such blocks in various forms to achieve the stated functionality. The digital frame signal from AFE block  22  is connected to an input  40  which connects the digital signal to a PSC correlator  42 . PSC correlator  42  correlates the known PSC with one frame width of information from the incoming digital signal, and this determination may be achieved by way of example using a matched filter having the PSC as its coefficients. Preferably, the number of correlations measured per frame are based on the sample rate of user station UST and the chip rate for the wireless communication; for example, in one approach the number of correlations per frame (i.e., 10 milliseconds) may be the product of the sample rate (e.g., twice per chip) and chip rate (e.g., 3.84 Mcps) and may be on the order of 76,800 PSC correlation measures. However, in alternative embodiments a reduced or different number of PSC correlations measures may be made per frame. In any event, PSC correlator  42  therefore provides a time-dependent signal representing the correlation measures of the PSC to the evaluated frame-width of signal. In the preferred embodiment, the energy (e.g., typically the absolute value of the magnitude squared) of these correlation measures is output by PSC correlator  42 , and examples of such output signals are detailed later. The output from PSC correlator  42  is connected to an input  44  of a first averaging block  46  block. 
     First averaging block  46  computes a first average designated for sake of reference in this document as AVG_ 0 . With respect to items within block  46 , its input  44  is connected as a first multiplicand to a first multiplier  48  which also receives a weight value, α w , as a second multiplicand. The output of first multiplier  48  is connected as a first addend to an adder  50 , and the output of adder  50  is connected to a buffer  52 . Buffer  52  is preferably of sufficient size to store one frame width (i.e., 15 slots) worth of information received at its input, and as detailed below such information corresponds to a set of PSC correlation measures by correlator  42  as well as an average based on successive sets of those measures. The output of buffer  52  is fed back to provide a first multiplicand to a second multiplier  54 , which also receives a weight value, β w , as a second multiplicand. The output of second multiplier  54  is connected as a second addend to adder  50 . Additionally, the output of buffer  52  provides the average value AVG_ 0  to two additional average circuits  56  and  58 . 
     Each of average circuits  56  and  58  operates to compute an average in response to AVG_ 0  and according to respective methodologies detailed below. For sake of reference, the average computed by average circuit  56  is referred to as AVG_ 1  and the average computed by average circuit  58  is referred to as AVG_ 2 . In the preferred embodiment, both AVG_ 1  and AVG_ 2  are determined by combining a first portion of AVG_ 0  with a second portion of AVG_ 0 , where the selection of those portions differs for circuits  56  and  58  and, thus, the differences in those selected portions also causes different values to be determined for AVG_ 1  and AVG_ 2 . In any event, since the averaging operations by circuits  56  and  58  are related to AVG_ 0  which will include various peaks along its time-dependent positions, then the respective average values determined by circuits  56  and  58  also will include peaks within each computed average. Further in this regard, for each computed average AVG_ 1  and AVG_ 2 , each of average circuits  56  and  58  outputs a magnitude of the largest peak within its respective average as well as the position of that peak within the average. For sake of reference, the peak magnitude from average circuit  56  is referred to as MAX_ 1  and its position is referred to as POS_ 1 . Similarly, the peak magnitude from average circuit  58  is referred to as MAX_ 2  and its position is referred to as POS_ 2 . Lastly, note that positions POS_ 1  and POS_ 2  are readily determined from a counter which advances as each PSC correlation sample is taken so that the count at any given time identifies the position of the corresponding sample. 
     In the embodiment illustrated in FIG. 4, both MAX_ 1  and MAX_ 2  are connected as inputs to a comparator  60 , which outputs a SELECT signal that has its state based on which of its two input values MAX_ 1  and MAX_ 2  is a maximum. The SELECT signal is connected as a select input to a multiplexer  62  and to a multiplexer  64 . Multiplexer  62  is also connected to receive the position values POS_ 1  and POS_ 2  as data inputs, while multiplexer  64  receives two fixed values as inputs, namely, 0 and 8 times 5,120 (i.e., 40,960) by way of example, where other values may be input based on sampling rate and so forth as further appreciated below. The outputs of multiplexers  62  and  64  are connected as addend inputs to an adder  66 , and the output of adder  66  outputs the POS signal shown in both FIG.  4  and FIG. 3, where in FIG. 3 recall that the POS signal is connected to stage  2  acquisition and despreader block  26 . For reasons detailed later, if MAX_ 1  is larger than MAX_ 2 , then SELECT is asserted in a manner such that multiplexer  62  outputs the value of POS_ 1  and multiplexer  64  outputs the value of 0, whereas if MAX_ 2  is larger than MAX_ 1 , then SELECT is asserted in a manner such that multiplexer  62  outputs the value of POS_ 2  and multiplexer  64  outputs the value of 8×5,120. 
     FIG. 5 illustrates a method  70  of operation of stage  1  acquisition block  24  of FIG.  4 . Method  70  begins with a step  72  where buffer  52  stores a first set of energy signals from PSC correlator  42 , where preferably the set spans the number of slots (e.g., 15) in one frame. Note that this first set of energy signals passes through multiplier  48 , and to simplify the present example assume that no weight adjustment is made, that is, assume α w =1. Further, because the signal set from step  72  is a first sample, than it is a sole addend into adder  50  and it directly passes to buffer  52  with no further signal added to it by adder  50 . 
     To further illustrate step  72  and to facilitate a discussion of the remaining steps of method  70 , FIG. 6 illustrates an example of one frame-sized set FS 1  of energy signals thereby spanning 15 slots for the example of the preferred embodiment. In other words, for the example of FIG.  6  and recalling that buffer  52  stores the PSC correlation measures for one frame width of information, then assume that the frame width considered for step  72  is those 15 sample slots illustrated in FIG.  6 . Note that the terminology “sample slot” is chosen to provide a timing reference for when the sample is taken by user station UST; however, because at this point in the method there is no known timing relationship between user station UST and the base station that transmitted the sampled frame, then the location of data within sample slot positions likely differs from the location that each data was transmitted in an actual slot by the base station. In the example of FIG. 6, the synchronization channel (shown as “SCH”) as received is located in sample slots  1  and  8  of FS 1 . Thus, the two instances of SCH are unevenly located within the 15 slots of FS 1  in that the SCH in sample slot  1  is followed by six non-synchronization channel slots while the SCH in sample slot  8  is followed by seven non-synchronization channel slots. Further, at the point at which FS 1  is received, there is an ambiguity as to whether the SCH in sample slot  1  or the SCH in sample slot  8  represents the actual first SCH transmitted in a given frame by the base station. In other words, it is known in the art that under a given TDD mode the base station will transmit the SCH twice per frame, and under this mode, the second SCH is transmitted seven slots after the first SCH. For example, often, the first SCH in a given frame is at the beginning of the frame (“BOF”), that is, in slot  1  of the frame and, thus, the second SCH in this case will be in slot  8  of the frame. However, in other cases, the first SCH may be transmitted in a slot other than the first slot, but also in this case again the second SCH in that frame will be transmitted seven slots after the first slot. In any event, when an SCH is received by user station UST, there is an ambiguity as to whether that SCH is in fact the first SCH originally transmitted in a frame or it is in fact the second SCH originally transmitted in a frame. This ambiguity, however, is resolved by the preferred embodiment as appreciated from the remaining discussion. 
     To further illustrate step  72 , FIG. 6 also illustrates an energy signal ES 1   1 , where ES 1   1  is intended to depict the set of energy values stored by buffer  52  as generated from the PSC correlation by correlator  42  with respect to FS 1 ; in other words, assuming no noise in the signal and the resulting PSC correlation, then ES 1   1  as stored by buffer  52  has two peaks P 1a  and P 1b  corresponding in time to the SCH located in sample slots  1  and  8  of FS 1 . Further, for sake of simplification, energy signal ES 1   1 , as well as other energy signals illustrated later, are shown as having a single peak, if any, centered per sample slot whereas in actuality many PSC correlation samples per sample slot are taken (e.g., 5,120) and, thus, many other peaks could occur within a same sample slot or different sample slots, and various peaks also may not necessarily be centered within a sample slot. In other words, note further that an SCH as transmitted by a base station need not be centered in a slot and, indeed, it may be transmitted at any chip position within a slot. Moreover, because the user station when first receiving the signal does not have a known timing with respect to the base station, then the SCH may appear at any chip within a slot as perceived by the user station. In other words, assume by way of an example that the base station transmits the SCH in slots  1  and  8  and at the first chip position of each of those slots, and assume also that user station UST has S samples per slot (i.e., in one frame it has 15S samples). Now since user station UST does not have any time information of the time reference of the base station and due to other delays etc., the SCH will be received at positions mod(1,15S) and mod(1+8S,15S). The value “1” is the offset between the user station&#39;s perceived frame position and the actual frame position. One skilled in the art may therefore appreciate from this illustration that the first SSC position received by user station in a frame can actually belong to the second SSC being transmitted by the base station. 
     Returning to FIG. 5, following step  72 , method  70  continues to step  74 . In step  74 , buffer  52  combines a second frame-sized set of energy signals from PSC correlator  42  with the set it stored from step  72 . Again to simplify the present example, assume that this second set of signals passes through multiplier  48  with α w =1 (i.e., no weighting). Further, this second set is combined with the first set by feeding back the first set from buffer  52 , through multiplier  54 , to be added by adder  50  the second set. Also, again for simplification, assume that β w =1 such that multiplier  54  does not weight the first sample set as it passes through that multiplier. To further illustrate step  74 , FIG. 6 also illustrates the second set of energy signals as ES 2   1 , which is combined into buffer  52  with ES 1   1  from step  72 . Note that the terminology that the two sets of signals are combined is used to indicate that the sets of signals may be merged with one another using various approaches. For example, the two could be only added to one another. As another example, the two could be directly averaged, that is, the sum of the two may be divided by two. As still another example, either ES 1   1  or ES 2   1  may be weighted by adjusting the values of α w  and β w  as desired by one skilled in the art to perform various types of scaled averaging, where one preferable type of scaling may be single pole averaging whereby the most recent sample set (e.g., ES 2   1 ) is given greater weight than a previous sample set (e.g., ES 1   1 ). In any event, the combination of two successive sample sets is referred to by way of reference, but not by limitation, as an average, and is designated as AVG_ 0 . To illustrate an example, assume that AVG_ 0  is the sum of two successive samples divided by two; further, FIG. 6 a  illustrates such an average with respect to ES 1   1  and ES 2   1  and designated as AVG_ 0   1 . Because the present example is an ideal case with no noise, multipath, or other delays, then ES 1   1  and ES 2   1  are identical and, hence, the average AVG_ 0   1  merely appears to be the same as either one of ES 1   1  and ES 2   1 . In actuality, however, ES 1   1  and ES 2   1  may differ to various degrees and include some level of noise, but the combination achieved in AVG_ 0   1  will remove some of these effects. In any event, after step  74 , method  70  continues with two steps  76  and  78  that may occur at the same time and, hence, are shown in parallel fashion in FIG.  5 . Each of steps  76  and  78  is discussed below. 
     Step  76  computes AVG_ 1 , and recall that AVG_ 1  is formed by combining a first portion of AVG_ 0  with a second portion of AVG_ 0 . In the preferred embodiment, this combination is an average of the values of AVG_ 0  in its sample slot positions  1 - 8  with the values of AVG_ 0  in its sample slot positions  8 - 15 , that is, the set of energy signals corresponding to sample slot positions  1 - 8  are added to the set of energy signals corresponding to sample slot positions  8 - 15 , and the sums are divided by two (although again, other averaging techniques may be used). FIG. 6 further illustrates the operation of step  76  with respect to the example of AVG_ 0   1  to thereby produce an example of AVG_ 1  shown as AVG_ 1   1 . Particularly, FIG. 6 first illustrates the signals at sample slot positions  1 - 8  of AVG_ 0   1 , abbreviated in FIG. 6 as AVG_ 0   1 : 1 - 8 , followed by the signals at sample slot positions  8 - 15  of AVG_ 0   1 , abbreviated in FIG. 6 as AVG_ 0   1 : 8 - 15 . Below those signals is the average of those signals, thereby forming AVG_ 1   1 . For purposes of later discussion, note that AVG_ 1   1  includes two peaks, P 1c  and P 1d , where P 1c  is greater than P 1d  (by a factor of two in the illustrated ideal case). 
     Step  78  computes AVG_ 2 , where AVG_ 2  is also formed by combining a first portion of AVG_ 0  with a second portion of AVG_ 0 . In the preferred embodiment, this combination is an average of the values of AVG_ 0  in its sample slot positions  1 - 7  with the values of AVG_ 0  in its sample slot positions  9 - 15 , that is, the set of energy signals corresponding to sample slot positions  1 - 7  are added to the set of energy signals corresponding to sample slot positions  9 - 15 , and the sums are divided by two. FIG. 6 further illustrates the operation of step  78  with respect to the example of AVG_ 0   1  to thereby produce an example of AVG_ 2  shown as AVG_ 2   1 . Particularly, FIG. 6 illustrates the signals at sample slot positions  1 - 7  of AVG_ 0   1  (i.e., shown as AVG_ 0   1 : 1 - 7 ), followed by the signals at sample slot positions  9 - 15  of AVG_ 0   1  (i.e., shown as AVG_ 0   1 : 9 - 15 ). Below those signals is the average of those signals, thereby forming AVG_ 2   1 , and note that AVG_ 2   1  includes one peak, P 1e . 
     In addition to the preceding, step  76  identifies MAX_ 1  which is the magnitude of the largest peak in AVG_ 1  and step  76  also identifies POS_ 1  which is the position of MAX_ 1  within AVG_ 1 . Thus, in the example of FIG. 6, step  76  identifies P 1c  as MAX_ 1   1  and its position within AVG_ 1   1 , POS_ 1   1 , which as shown in FIG. 6 is position  1 . Similarly, step  78  identifies MAX_ 2  which is the magnitude of the largest peak in AVG_ 2  and step  78  also identifies POS_ 2  which is the position within AVG_ 2  of MAX_ 2 . Thus, in the example of FIG. 6, step  78  identifies P 1e  as MAX_ 2   1  and its position, POS_ 2   1 , as position  1 . Next, method  70  continues from steps  76  and  78  to a step  80 . 
     Step  80  represents the operation of comparator  60  in FIG.  4  and performs a comparison, where the result of the comparison resolves the ambiguity as to whether a first peak or a second peak in AVG_ 0  represents the actual first SCH transmitted in a given frame. Specifically, step  80  compares MAX_ 1  to MAX_ 2 , and if MAX_ 1  is the larger of the two then method  70  continues to step  82 , whereas if MAX_ 2  is the larger of the two then method  70  continues to step  84 . As further demonstrated below, the flow to either step  82  or step  84  is accomplished by comparator  60  of FIG. 4 by asserting the SELECT signal to a respective binary state. Once more looking to the example of FIG.  6  and recalling that MAX_ 1   1 =P 1c  and MAX_ 2   1 =P 1e , then a visual inspection of these peaks demonstrates that MAX_ 1   1  is the larger of the two and, hence, for this example method  70  continues to step  82 . 
     In step  82 , having been reached because MAX_ 1  exceeds MAX_ 2 , then step  82  resolves that the SCH transmitted by the base station as a first SCH in a frame has been received by user station UST somewhere in FS 1  among sample slots  1  through  8  (as opposed to in sample slots  9  through  15 ). Further, step  82  identifies the actual position of the transmitted SCH within FS 1 . Specifically, in step  82 , SELECT is asserted to a state to cause multiplexers  62  and  64  to select what is shown as the lower input to each multiplexer; as a result, the outputs to adder  66  cause it to add the value of POS_ 1  as an offset to the fixed value 0. In the present example, recall that POS_ 1   1  should identify the sample position of peak P 1c  which, recall by way of example is assumed to be centered within slot  1 ; thus, peak P 1c  will occur at sample position 2,560 (i.e., half-way through the 5,120 sample positions in slot  1 ). Accordingly, this value is added by adder  66  to 0 for a total value, POS, equal to 2,560 and, thus, this value of POS from step  82  indicates that the actual position of the first SCH transmitted in the present frame is at sample position 2,560 of FS 1 . Further, recall from FIG. 3 that this value of POS is further communicated to block  26  for use therein. Finally, by visually inspecting FS 1  as illustrated in FIG. 6, one skilled in the art may confirm that the step  82  determination is accurate, that is, that SCH in slot  1  is the first SCH transmitted in a given frame because that slot  1  SCH is followed by six non-synchronization channel slots whereas the SCH in sample slot  8  is followed by seven non-synchronization channel slots. 
     In step  84 , having been reached because MAX_ 2 , exceeds MAX_ 1 , then step  84  resolves that the SCH transmitted by the base station as a first SCH in a frame has been received by user station UST somewhere in FS 1  among its sample slots  9  through  15  (as opposed to in slots  1  through  8 ). To further illustrate this operation, FIG. 7 depicts another example of a received frame-sized set FS 2  of energy signals spanning a total of 15 sample slots. In the example of FIG. 7, one SCH is received in sample slot  1  and another SCH is received in sample slot  9 . Again, only by way of example, assume that both of these SCHs are centered within the respective sample slots. Further, one of these two SCH occurrences is therefore the first SCH as transmitted in a given frame to user station UST; indeed, by a visual inspection of FS 2 , one skilled in the art may conclude that the SCH in sample slot  9  is the first SCH as transmitted in a given frame because it is followed by six non-synchronization channel slots whereas the SCH in sample slot  1  is followed by seven non-synchronization channel slots. Thus, method  70  is now discussed with respect to FS 2  of FIG. 7 to confirm that the method reaches this proper result, and this example as detailed below makes this determination by ultimately reaching step  84 . 
     Applying method  70  to FS 2  of FIG. 7, step  72  buffers a first frame-sized set of energy values shown in FIG. 7 as ES 1   2 , and step  74  combines a second framed-size set of energy values ES 2   2  with ES 1   2 , where both sets again are shown without noise to simplify the illustration and which thereby form an average AVG_ 0   2  also shown in FIG.  7 . Again, ES 1   2  with ES 2   2  may differ to various degrees and include some level of noise, and the preferred combination achieved in AVG_ 0   2  removes some of these effects. 
     Next with respect to FIGS. 5 and 7, steps  76  and  78  determine the AVG_ 1  and AVG_ 2  values based on the sample slot positions of AVG_ 0   2  shown in FIG. 7, namely, positions  1 - 8  are averaged with positions  8 - 15  to form the example of AVG_ 1  shown as AVG_ 1   2  in FIG. 7, while positions  1 - 7  are averaged with positions  9 - 15  to form the example of AVG_ 2  shown as AVG_ 2   2  in FIG.  7 . Further, note that AVG_ 1   2  includes two peaks P 2c  and P 2d  while AVG_ 2   2  includes one peak P 2e . In addition to the preceding, step  76  identifies MAX_ 1   2  and POS_ 1   2  relating to the largest peak in AVG_ 1   2 . In this regard, note that peaks P 2c  and P 2d  may be approximately the same magnitude because noise is not included in the illustrated ideal example; however, in an actual implementation where noise is present, one of the peaks will most likely exceed the other. As further shown below, regardless of which is chosen for purposes of defining MAX_ 1   2  and POS_ 1   2 , the ultimate outcome of operation should not be negatively affected. With respect to step  78 , it identifies P 2e  as MAX_ 2   2  and position POS_ 2   2  is identified as position  1 . Next, method  70  continues from steps  76  and  78  to step  80 . 
     Step  80  again compares MAX_ 1  to MAX_ 2 , where in the example of FIG. 7 this comparison is of MAX_ 1   2  to MAX_ 2   2 . From this comparison, the peak P 2e  of MAX_ 2   2  is found to exceed either peak P 2c  or P 2d  of MAX_ 1   2  (based on whichever was selected as described above), with the result thereby passing the method flow to step  84 , and recall that step  84  was introduced by the example of FIG.  7 . Looking now to the specific application of step  84  to FIG. 7, step  84  resolves that the SCH transmitted first in a given frame has been received somewhere in FS 2  among sample slots  9  through  15  (as opposed to in sample slots  1  through  8 ), and step  84  also identifies the slot position in which this first-SCH was transmitted within FS 2 . Specifically, in step  84 , SELECT is asserted to a state opposite that of step  82 , where the step  84  state causes multiplexers  62  and  64  to select what is shown as the upper input to each multiplexer; as a result, the outputs to adder  66  cause it to add the value of POS_ 2  as an offset to the fixed 8×5,120 (i.e., 8S, where S is shown above to be the number of samples per slot). In the present example, POS_ 2   2  should identify the sample position of peak P 2e  which, because the example assumes it is centered within slot  1 , it will occur at sample position 2,560 (i.e., half-way through the 5,120 sample positions); accordingly, this value is added by adder  66  to 8×5,120 for a total value, POS, equal to 43,520 (i.e., 2,560+[8×5,120]=43,520) and, thus, this value of POS from step  82  indicates that the actual position of the first SCH transmitted in the presently analyzed frame is centered within sample slot position  9  of FS 2 . Finally, by visually inspecting FS 2  as illustrated in FIG. 7, one skilled in the art may confirm that the step  84  determination is accurate, that is, that the first SCH transmitted in the present frame is the SCH in sample slot  9  because that SCH is followed by six non-synchronization channel slots whereas the SCH in sample slot  1  is followed by seven non-synchronization channel slots. 
     As a final illustration of the operation of method  70 , FIG. 8 depicts still another example of a received frame-sized set FS 3  of energy signals. In the example of FIG. 8, one SCH is received in sample slot  4  and another SCH is received in sample slot  11 . Further, a visual inspection of FS 3  reveals that the SCH in sample slot  4  is the first SCH transmitted in the present frame because it is followed by six non-synchronization channel slots whereas the SCH in sample slot  11  is followed by seven non-synchronization channel slots (assuming a wraparound count back to the SCH in sample slot  4 ). Since method  70  has been described above with respect to other examples, then one skilled in the art should readily appreciate the following brief description of that method as applied to the example of FIG.  8 . 
     Through step  74  two samples ES 1   3  and ES 2   3  are buffered and combined to form an average AVG_ 0   3 . Next, AVG_ 1   3  is formed by averaging positions  1 - 8  and  8 - 15  of AVG_ 0   3 , while AVG_ 2   3  is formed by averaging positions  1 - 7  and  9 - 15  of AVG_ 0   3 . The maximums and respective positions of those maximums are determined for AVG_ 1   3  and AVG_ 2   3  followed by step  80  determining that the largest of those maximums (i.e., peak P 3c ) occurs in AVG_ 1   3  at sample slot position  4  (i.e., POS_ 1   3 =4) and passing the flow to step  82 . Step  82  thereby resolves that the first SCH as transmitted in the present frame being analyzed is in FS 3  among its sample slots  1  through  8 , and by adding the value of POS_ 1   3  as an offset to 0 it determines that the actual position, POS, of this first transmitted SCH. Again, assuming peak P 3c  is centered within slot  4 , then its sample position, POS_ 1   3 , equals 17,920, and that value is added to 0 to indicate that POS=17,920, that is, the first SCH transmitted by the present frame being analyzed is located at sample position 17,920 of FS 3  (i.e., centered with slot  4 ). 
     Having examined FIGS. 6 through 8 in connection with the preferred embodiments, various additional observations may be made with respect to the inventive scope. As a first observation, the examples of FIGS. 6 through 8 demonstrate that the preferred embodiments receive a communication sequence having an odd number of slots and with two SCH occurrences therein and use various averaging methods to identify a peak value which then identifies which of the SCH occurrences corresponds to the SCH that was transmitted as the first of two SCH&#39;s transmitted in a given frame by a base station. As a second observation, from the preceding example one skilled in the art may readily consider the many other possible sequences having different locations for the two SCH occurrences, where for each of those instances it will be confirmed that method  70  identifies in a received sequence which of two SCH&#39;s received in that sequence is the SCH transmitted in a given frame by a base station as the first SCH in that frame, and method  70  also identifies the position of that first-transmitted SCH within each such sequence. As a third observation, while a preferred embodiment is illustrated in the example of a WCDMA sequence having fifteen slots, still other communication data streams may be analyzed using the preceding inventive teachings. 
     Returning to FIG. 5, note that after either step  82  or step  84 , method  70  concludes with a step  86 . In step  86 , block  26  (see FIG. 3) performs the stage  2  acquisition which is the acquisition of the SSC. More particularly, as known in the TDMA art, SSC detection is achieved by correlating the SSCs in two successive frames with a different so-called comma free code (“CFC”), where each CFC is a series of four 256 length composite codes, that is, each composite code may be three SSCs sent in parallel. For example, assume that such a given CFC may be represented by the following series of four 256-length composite codes: 
     C 1 , C 2 , C 3 , C 4    
     In other words, for two successively received frames, there are a total of four composite SSCs and, thus, in the stage  2  acquisition a correlation is measured by user station UST between each successive one of the four composite CFCs and a respective one of the total of four composite SSCs. 
     As an additional consideration to step  86 , attention is now directed to the use of the POS value from either step  82  or step  84  in FIG.  5 . Specifically, recall that the POS value indicates, for a given frame width of information, which of the two SCH slots in that information corresponds to the first of two SCH&#39;s transmitted by a base station in a given frame. Since the SCH includes both a PSC and a composite SSC, then the POS indication likewise informs step  86  which of the two composite SSCs in the information was transmitted first in a given frame. This indication, therefore, reduces the required number of stage  2  correlation measures, as may be further demonstrated by way of the following example. 
     As an example of stage  2  correlation measures in step  86 , assume that in two successive frames, the following four composite SSC are received in the order shown: 
     SSC 1 , SSC 2 , SSC 3 , SSC 4    
     Further, from either step  82  or step  84 , the POS value will indicate, for each pair of composite SSCs (i.e., the first pair SSC 1  and SSC 2  and the second pair SSC 3  and SSC 4 ), which of the composite SSCs in the pair was actually transmitted first in a given frame by a base station. For example, assume that POS indicates that SSC 1 , the first SSC in the pair SSC 1  and SSC 2 , was the first SCH transmitted in the given frame; thus, it also follows therefore that SSC 3 , the first SSC in the pair SSC 3  and SSC 4 , also was transmitted first in another frame. As a result, step  86  performs the following two CFC correlation measures shown in Table 1: 
     
       
         
               
               
               
               
               
             
           
               
                 TABLE 1 
               
               
                   
               
               
                 Correlation 
                 composite 
                 composite 
                 composite 
                 composite 
               
               
                 number 
                 SSC 1   
                 SSC 2   
                 SSC 3   
                 SSC 4   
               
               
                   
               
             
             
               
                 1 
                 C 1   
                 C 2   
                 C 3   
                 C 4   
               
               
                 2 
                 C 3   
                 C 4   
                 C 1   
                 C 2   
               
               
                   
               
             
          
         
       
     
     Correlation number 1 in Table 1 is a straightforward correlation given the knowledge that SSC 1  was transmitted as a first of two codes in a given frame, that is, then the CFC in correlation number 1 (i.e., C 1 , C 2 , C 3 , C 4 ) is correlated to the SSCs as received in the two successive frames. However, because the CFC is presented along two frames, at this point in the method there is the possibility that SSC 1  and SSC 2  were transmitted in a second frame of a pair of frames rather than in a first frame of a pair of frames. Thus, the correlation number 2 shown in Table 1 is also performed in step  86  whereby the second pair of CFC codes (i.e., C 3  and C 4 ) in the CFC sequence are correlated with the SSCs in the first received frame (i.e., SSC 1  and SSC 2 ), while the first pair of CFC codes (i.e., C 1  and C 2 ) are correlated with the SSCs in the second received frame (i.e., SSC 3  and SSC 4 ). Once the correlations measures are complete, the strongest correlation is deemed to correspond to a proper detection of the SSCs and, thus, completes the SSC acquisition. 
     FIG. 9 illustrates an alternative method  70 ′ of operation of stage  1  acquisition block  24  and the stage  2  acquisition of block  26  of FIG.  4 . Method  70 ′ includes the same steps  72  through  78  of method  70  from FIG. 5; however, following steps  76  and  78 , method  70 ′ proceeds to a step  88 . Thus, in method  70 ′, the values of POS_ 1  and POS_ 2  are both used in step  88  rather than being compared by an intermediate step as is the case in method  70 . Further, to embody this approach in user station UST of FIG. 4, then comparator  60 , multiplexers  62  and  64 , and adder  66  are removed, and the values of POS_ 1  and POS_ 2  are passed as the output POS to block  26 . The specific operation of step  88  is discussed immediately below. 
     In step  88 , block  26  performs the stage  2  SSC acquisition, again using correlation measures by correlating the SSCs in two successive of frames with CFCs. Using the example provided above, assume again therefore that the CFC is represented by the following series of four 256-length composite codes: 
     C 1 , C 2 , C 3 , C 4    
     However, because step  88  has two different positions provided by POS (i.e., POS_ 1  and POS_ 2 ), then step  88  requires more correlation measures as compared to step  86  in method  70 . Specifically, because the POS value indicates both POS_ 1  and POS_ 2 , then at the time step  88  is reached then the SCH positions have been determined for a frame width of information, but there has not been a determination of which of the two SCH slots in that information was transmitted as a first SCH in a given frame. This status, therefore, increases the required number of stage  2  correlation measures as compared to method  70  described above, as may be further demonstrated by way of the following example. 
     As an example of stage  2  correlation measures in step  88 , assume again that in two successive frames, the following four composite SSCs are received in the order shown: 
     SSC 1 , SSC 2 , SSC 3 , SSC 4    
     However, because it is not known which code was transmitted first in the pair of codes transmitted in a given frame, then any one of the four SSCs may represent such a first-transmitted code. In other words, POS_ 1  and POS_ 2  indicate the slot positions of two SCHs per one frame width of information (and thereby the respective SSCs in those SCHs), but at this point there is no indication as to which of those positions was transmitted first in a frame. As a result, step  88  performs the following four CFC correlation measures shown in Table 2: 
     
       
         
               
               
               
               
               
             
           
               
                 TABLE 2 
               
               
                   
               
               
                 Correlation 
                 composite 
                 composite 
                 composite 
                 composite 
               
               
                 number 
                 SSC 1   
                 SSC 2   
                 SSC 3   
                 SSC 4   
               
               
                   
               
             
             
               
                 1 
                 C 1   
                 C 2   
                 C 3   
                 C 4   
               
               
                 2 
                 C 4   
                 C 1   
                 C 2   
                 C 3   
               
               
                 3 
                 C 3   
                 C 4   
                 C 1   
                 C 2   
               
               
                 4 
                 C 2   
                 C 3   
                 C 4   
                 C 1   
               
               
                   
               
             
          
         
       
     
     Correlation number 1 in Table 2 is measured given the possibility that SSC 1  was transmitted as part of the first of four SCHs in two successive frames. However, there exists three other possibilities, that is, that any of SSC 2 , SSC 3 , or SSC 4  was received as part of the first of four SCHs in two successive frames. Accordingly, correlations numbers 2 through 4 of Table 2 correspond to these respective possible scenarios. 
     Having detailed both methods  70  and  70 ′, note that the selection between one over the other may be left to one skilled in the art based on various considerations. For example, the total time for stage  1  and stage  2  acquisition, T acq , is in general a non-linear function of T 1 , T 2 , T 3 , P d1 , P d2 , and P d3 , where T 1  is the time for stage  1  acquisition, T 2  is the time for stage  2  acquisition, T 3  is the time for stage  3  acquisition, P d1  is the probability of detection in stage  1 , P d2  is the probability of detection in stage  2 , and P d3  is the probability of detection in stage  3 . Also P d1  and P d2  are non-linear and typically P d1  is much less than P d2 . Therefore, in some instances it may be desirable to reduce T 1  to offset the aspect that P d1  is relatively small. In this regard, method  70 ′ accomplishes such a reduction of T 1  relative to method  70 ; in other words, while method  70 ′ requires additional correlation measures over method  70  as shown by a comparison of Tables 2 and 1, respectively, the time for these measures thereby increases T 2  while T 1  is also reduced because the comparison and ambiguity resolution of steps  80 ,  82 , and  84  from method  70  are eliminated in method  70 ′. As a result, while additional time is shifted from T 1  to T 2 , the total acquisition time T acq  may be reduced. Thus, these as well as other considerations ascertainable by one skilled in the art may lead to the selection of either method  70  or  70 ′. 
     From the above, it may be appreciated that the above embodiments provide an improved system and method for identifying a synchronization channel with a sequence of received slots. The preceding also has demonstrated various alternatives that are within the present inventive scope. Indeed, in addition to the various options provided above, still others are contemplated within the present inventive scope. For example, while the preceding example is applied in the context of user station synchronization, one skilled in the art may possibly adapt these teachings to synchronization by a base station. As another example, while the preferred embodiment has application to CDMA (i.e., WCDMA), and the TDD data transfer technique thereof, the present teachings may apply to other wireless communication formats. Indeed, the previous example has illustrated one TDD mode wherein the synchronization channel is located in two slots of a frame; however, the preferred embodiment may operate with other modes such as mode  1  of TDD wherein the synchronization channel is located in only one slot per frame in which case only one average need be taken or, if two averages are taken, the preferred embodiment will still properly identify the synchronization channel from the larger peak of the two averages. As still another example, while method  70  preferably forms AVG_ 0  to remove noise and then uses its signals to generate AVG_ 1  and AVG_ 2 , in an alternative embodiment AVG_ 1  and AVG_ 2  could be determined directly from the set FS without the benefit of the first averaging to remove noise. As still another example, while method  70  preferably forms AVG_ 0  by averaging two sets of signals, in still another embodiment a greater number of signal sets may be combined to form AVG_ 0 . As still another example, while the preferred embodiment focuses on only a single maximum peak for each of AVG_ 1  and AVG_ 2 , in other embodiments a larger number of peaks per each of AVG_ 1  and AVG_ 2  may be processed; for example, to respond further to the possibility of multipaths, two peaks per each of AVG_ 1  and AVG_ 2  may be passed to the stage  2  acquisition. As yet a final example, while the present teachings are applied to a 15 slot frame, other data formats wherein a synchronization channel is located in a frame or comparable data format which is divided into an odd number of portions may benefit from the present inventive teachings. Consequently, while the present embodiments have been described in detail, various substitutions, modifications or alterations could be made to the descriptions set forth above without departing from the inventive scope which is defined by the following claims.