The concurrent process for blind deconvolution of digital signals described herein is intended to reduce and, possibly, eliminate the problem of intersymbol interference in digital signals, which is a result of the dispersive effect of any practical transmission channel. The process has the following working principle: The deconvolution is done by two filters, denominated herein V and W, whose two signals which results respectively from the filtering action of each filter jointly define the output signal y of the deconvolution process.

The coefficients of filter V are adjusted by gradient methods, or equivalent, based on a cost function that measures a statistic dispersion of y. The coefficients of filter W are adjusted by gradient methods, or equivalent, based on a cost function that measures a distance from y to the nearest digital alphabet symbol. The updating of the coefficients of filters W and V is such that the updating of the coefficients of W depends on the updating of the coefficients of V by means of a non-linear function. The results obtained demonstrate that the process described herein presents a performance comparatively superior to the processes usually adopted for the solution of this type of problem, and the range of possible applications and/or devices to be protected. Applications and/or devices subject to have their performance improved by the use of the Concurrent Process for Blind Deconvolution of Digital Signals includes but is not limited to: Spatial-Temporal processing (used, for example, in Smart Antennas or Smart Sensors, etc...), any digital telecommunication systems (cellular telephony, digital television, digital radio, etc...), telemetry systems; remote sensing systems; geodesic localization/measurement systems (GPS, etc..); navigation aid systems; seismic survey systems by wave refraction/reflection, magnetic media storage systems, RADAR systems, SONAR systems.

The Concurrent Process for Blind Deconvolution of Digital Signals, implemented by means of the Concurrent Equalizer, presents the capability to efficiently reach, under the same operational situation, a condition much closer to the zero-forcing condition, or equivalent, than the other equalizers used in the current scenario. This scenario includes the universally used-and renowned-CMA Equalizer. This allows the Concurrent Equalizer to be used to deconvolve channels with denser symbol constellation than the current technologic state permits. This way, the use of the Concurrent Equalizer for Blind Deconvolution of Digital Signals will allow for an increase in the transmission rate for those

digital systems that have their maximum speed limited by the operation of the equalizer (for example, see [21]).

Definition of the Problem whose Solution is Obtained by means of the Concurrent Process for Blind Deconvolution of Digital Signals.

The solution for the problem of superposition of propagation rays and the dynamic variation in the transmission channel of a digital system will be one of the hardest challenges for the technological advancement in this area for the next few years. In mobile communications, this undesirable phenomena is characterized by the parameters delay spread, angle spread and Doppler spread, which determine the level and dynamics of superposition between the symbols of the system. Such symbol superposition occurs as a consequence of the transmission of information through the channel.

Particularly, the superposition of symbols occurs due to the dispersive nature of the transmission channel of any practical digital system, which implies in the impulsive response c (n) of the channel to assume non-null values along many sample intervals [1]. A non-dispersive channel presents a response c (n) to the impulse d (n), characterized by a single W (n-nd) impulse that occurs in nd 2 0 sample instants after the initial instant.

The dispersion of the channel may be better understood from the point of view of the convolution [2] between the sequence of symbols s (77) sent by the digital transmitter and the impulsive response c (M) of the channel. If the channel is non-dispersive (which is the ideal situation desired in practice, due to the high speed of transmission of the digital symbols of the current systems), then the symbol sequence u (n) received by the digital receiver will be a equal to s (n), except for a gain constant G and a delay nd # 0, i.e., u(n) = G s(n - nd). If the channel is dispersive, each sample of u (n) will be a weighted sum of the previous samples, which is defined by c (n) &num , 5 (n-nd)- This way, the channel dispersion may be associated with the concept of reverberation, since the value of each sample is interfered by"echoes"from previously occurred samples. From this fact we have the concept of the quantity denominated Inter Symbol Interference or ISI, whose value measures how much the symbols of a digital transmission system overlap each other due to the channel dispersion [1] [3].

As the reverberation is a natural an inevitable phenomena to all and any practical transmission channel, the scientific community has circumvented the problem by means of dispersion compensation systems denominated Equalizers. Equalizers are usually placed between the digital receiver and the channel, so that the combined impulsive response h (ri) of the Equalizer in series with the channel tends to #(n - nd), and then avoiding the channel dispersion [1]. Figure 1 shows the simplified diagram of the dispersion compensation process accomplished by the Equalizer. ---------- i Transmission Y (17) Digital l 1 1 | Transmission > rinJ X | | | yfn} | Digital Transmission Channel X Equalizer /I I e_ _ _ _ _ Transmission Media: Any media liable to transport information by means of a group of Process: The u (n) signal received from the channel is digital symbols belonging to a digital alphabet. corrupted due to dispersion and/or echoes in the For example, electro-magnetic, acoustic, optical Equalizer input. The Equalizer processes the u (n) channels, etc... signal and delivers the y (n) signal in its output, which presents contents of dispersion and/or echoes lower than the u (n) signal, due to the deconvolution process performed by the Equalizer.

Figure 1: Baseband [1] representation of the removal process of the ISI by the Equalizer in a digital transmission system.

In Figure 1, note that h (n) is the result of the convolution of the channel impulsive response c (ii) with the Equalizer impulsive response f (n), i. e., h (n) = c (72) * f(n) [2]. As the sequence of symbols y(n) received by the digital receiver is the result of the convolution of s (n) with h (), and since the Equalizer actuates in the process in order that h (n) # (M-), the process of channel deconvolution-also called process of channel equalization [2] [3]-results in y(n) # s(n - nd). That is, the deconvolution process performed by the Equalizer causes the y(n), contrary to the M ?) signal received from the channel, to be a reply of the s (7Z) sequence originally transmitted, except for a delay of nd

samples. Every time the deconvolution process reaches a stage in which h (n) o 6 (n-n]) it is said that the Equalizer has reached the ZF (zero forci71g) condition (or situation), when then, ISI-0 [1]. In many practical situations, due to several factors, such as noises and characteristics specific to the channel, the ZF condition is not fully accomplished, but only approximated by the Equalizer. One of these cases is that one in which the Equalizer operates in a situation of MMSE (Minimum Mean Squared Error), which is not exactly the ZF situation, but for practical and operational purposes of an Equalizer operating in this condition, it is a substitute situation.

Independently of the transmission channel media (electro-magnetic, acoustic, etc...), due to the tendency of digital systems to transmit digital symbols at faster and faster speeds to meet market demands, the dispersion, even at low levels, is enough to deteriorate the system performance, because the duration interval of the symbols is short if compared to the duration interval of the dispersion. Another additional factor has recently appeared, complicating even more the advancement of digital communications: The telecommunication market has presented a high growth rate of demand for more complexity (and, therefore, volume) of information to be transmitted. The Cellular Telephony System of 3rd Generation based on the"software radio"concept (under development by several manufacturers [4]) is a typical example of such demand. The fact is that this demand growth rate is a lot higher than the operation speed growth rate (clock) of the digital circuits that compose the digital system, and that speed is limited by the status of technological advance in the micro-electronics and semiconductors field. Also, it is important to point out that all these limiting factors occur in a context with little availability to allocate spectral bands, especially in low frequencies.

This way, in order to meet this higher demand for information volume, the solution found is to increase the"vocabulary"of digital symbols of a system (denominated constellation or system alphabet), so that the higher complexity of information may be offset by a better elaborated"vocabulary", capable to represent a maximum volume of information within the same time interval. That is, a denser constellation allows the transmission speed not to be reduced as a consequence of the higher complexity-i. e., entropy [1] [3]-of information, since the larger number of symbols available circumvents the need to issue

many symbols in a row, a situation that would occur for a lesser dense constellation.

However, for the same number of"letters"available, a forcibly long "vocabulary"presents a larger number of"words"or symbols that are similar to each other than a simpler"vocabulary". This increased similarity between the constellation symbols of a digital system that uses a denser constellation turns into a serious problem for the system performance when the channel is dispersive. This is due to the fact that the minimum ISI makes the symbols unintelligible from the digital point of view, due to the increased intrinsic similarity between them. In technical terms, the distance that differs the symbols from each other becomes shorter, which hampers the identification of the symbol effectively received.

This way, the performance of a channel Equalizer of a digital system becomes the critical factor in the performance of the system as a whole.

It is important to point out that the emerging cellular wideband communications systems, such as the 3rd Generation systems, involve the use of Smart Antennas in radio-bases and, possibly, in receiver terminals. These Smart Antennas are controlled by digital processing algorithms, denominated"Spatial-Temporal"algoritluns, which are essentially equivalent to the equalization algorithms referred to and/or described herein.

An equalizer is said to be blind when it performs the blind deconvolution of the channel, that is, when the equalizer totally discards the need of the receiver to recognize the s (n) sequence originally transmitted. On the opposite, non-blind equalizers need the s (fi) sequence to be recognized in the receiver as a reference-at best for a short interval of time -so that the ZF, MMSE or other equivalent condition may be accomplished. The advantage of a blind equalizer over a non-blind one is, therefore, obvious from the point of view of the reduction of spectral band required.

The Concurrent Process for Blind Deconvolution of Digital Signals, objective of this patent claim, is implemented by means of a blind equalizer system whose architecture is characterized for being concurrent. Therefore, hereinafter, we will refer to the equalizer that implements the Concurrent Process for Blind Deconvolution of Digital Signals as "Concurrent Equalizer", The new and inedited architecture of the Concurrent Equalizer- and the operation mode intrinsic to this architecture-permits the efficient deconvolution of

digital signals with much denser constellations than permitted by the types of blind equalizers usually employed in current digital systems. Furthermore, the Concurrent Equalizer permits the dynamic temporal variation in the channel, resulting, for example, from the relative displacement between digital transmitter and receiver, to be significantly higher than the maximum displacement speed usually permitted by other equalizers.

The ConcurrentEqualizer.

Figure 2 shows the diagram for the Concurrent Equalizer. From its initialization, the vector with weights V = [V0 V1 # VL-1]T is updated with some algorithm based on Gradient methods, such as, for example, Stochastic Gradient [3], RLS (Recursive Least Square) [3], or another equivalent, intending to minimize the cost function JD, of another cost function that measures dispersion. Likewise, from its initialization, the vector with weights W = [W0 W1 # WL-1]T is updated with some algorithm based on Gradient Methods, intending to minimize the cost function JQ, or another that measures an output distance y from the Equalizer to the nearest symbol in alphabet A, which is given by Q {y}. The operator Q {} represents the quantization operation with reference to the symbols of alphabet A.

2 Stochastic Gradient a 2 QtY} =ar9rninly-skl, Ske A StochasticGradient_|J= 4 E {(|yl-Y}} | su k = 0, 1, M-I Vo vu 1 up. received x vL 2 \ \ samples vu-9 channe E /W1. r ri L-2 L-1 _I L-1 i.. L-2 I WP.. 4 //wO.,! / ZU z,-*--, =' --- -.''- =T ! °M- Stochastic Gradient Figure 2: Schematic diagram of the Concurrent Equalizer, which implements the Concurrent Process for Blind Deconvolution of Digital Signals. Each z-'block introduces the delay of a sample.

In Figure 2 y = E VEti, statistic dispersion constant for a dispersion order of P=2. E {} is the operator that returns the statistic average of the argument. The {6} T operator results in the transposition of the vector/matrix argument and the-operator returns the Euclidean rule of the argument. The-operator was used as a distance metric, since the symbols s of alphabet A are usually complex numbers (when, for instance, the signalling is M-QAM, M-PSK, [1] etc...). Therefore, the computational cost of the-operation is reduced with | = s s, where the {} operator represents the conjugation of the argument.

However, any operator expressing the length-in the distance context-of the argument may be used. The Gradient method shown in Figure 2 is the Stochastic Gradient, but any equivalent method is liable to be employed.

Note that JD is a statistic dispersion of order P [5], which inherently uses higher order statistics from the equalizer output set y [6]. Although the Concurrent Equalizer can operate for any internal value of P, for the sake of simplification of the following

description, we will adopt P = 2.

Note that JQ measures the square of the Euclidian rule between the equalizer output and the nearest alphabet symbol. Also, by the definition of the cost functions, note that if JQ is minimized, JD will simultaneously be minimized too. However, the reciprocal is not true.

In order to the minimization process of JQ does not destroy the stability of the delicate dynamics of the minimization process of JD, for both share the same common variable y, a link is established between them, as demonstrated in Figure 2. This link permits the process of JD to inform how balanced it is to the process of JQ. The balance of the JD process must be understood not only associated with the stability concept, but also associated with the degree of the effect resulting from that stability, that is, the degree in which the minimization process of JD simultaneously minimizes JQ, since the equalizer was developed to operated concurrently. This criteria is critical, since the minimization of JD, for definition, not necessarily minimizes JQ. This link consists of a non-linear operator that inhibits the JQ process when the minimization process of JD does not minimize JQ simultaneously. Thus, although they share the common output variable y-which makes the processes concurrent due to the resulting architecture-the JQ process can only interfere cooperatively with the minimization process of JD.

Table 1 describes the general procedure adopted when the Concurrent Equalizer is applied to the equalization of a channel under T/2 fraction sampling [1]. Stage Procedure Initialize vectors W and l » : W=0+j0 and fO+7'0=OAZ-l, 1+ j0, k= where, j =, L is the dimension of vectors V and W (equalizer size) and 0< <L-1, is the index of the only weight of the V weight vectors to be initialized with the value 1+jO. Initialize the index counter for the received samples by fractional sampling from channel: i =1 Initialize the channel regressor index counter (or instant/iteration index counter): nô Obtain the nth channel regressor r (n) [6] [1] [7]: rk(n) = u(L-1-k+i), k = 0,1,#,L-1, where, u is the sequence of samples received by fractional sampling T/2 from the channel, with i =1, 3, A, Na-1, varying as n = 0, 1, A, Nr-1, and Na is the total number of samples to be received by fractional sampling from the channel, is the total number of regressors to be obtained from the channel and T is the interval between the symbols generated in the transmitter. L j is the operator that results in the closest whole number minor than the argument.

Obtains the equalizer output at the instant n : y(n) = WT (n)#r(n)+V(n)#r(n) Update V weight vector: V(n+1)=V(n)+#v#y(n)(γ-#y(n)#2)#r*(n), where, 77, is the adaptation step of vector V, 0 < 7v « 1.0.

Update W weight vector: W(n+1)=W(n)+#w[1-DQ(n)][Q{y(n)}-y(n)]r*(n), where, 7Zw is the adaptation step of vector W, 0 < #w # 1.0. controls the non-linear link of Figure 2, where Y (n) = VT (n+1)#r(n) + WT (n)#r(n) Increment index counters: <BR> <BR> <BR> <BR> i=i+2<BR> <BR> <BR> <BR> <BR> n=n+ 1 Test loop end: If L +i > Nα#END Otherwise, repeat steps 4 to 9.

Table 1: General summary of operations performed by the Concurrent Equalizer to implement the Concurrent Process for Blind Deconvolution of Digital Signals when applied to the channel equalization, for P = 2. Note that, in a continuous communication, the value of Na may be considered infinite.

From Table 1, note that factor [1-DQ] generates the following behavior during the operation of the Concurrent Equalizer: W can only be updated if, when updating Il, the output variable y remains in the same quantization level Q {y}. A quantization in V that does not change the quantization level Q implicitly means a probably correct updating, since this is the expected condition after the equalizer convergence. Therefore, factor [1-D Q] controls the updating of bY pursuantly to the concurrent operation of the system: The minimization process of JQ is only activated when the minimization process of JD simultaneously minimizes JQ. As the W and V filters jointly influence the output y, factor [1-DQ] avoids any non-cooperative interference of the minimization process of JQ that might unbalance the minimization process of JD.

Comparative Tests under Static Channel-Results Obtained.

With the objective of testing the Concurrent Equalizer in situations as real as possible, we will use in this description models of channels available in the database of Rice University, in Houston, Texas, USA. This database is known as Signal Processing Infor7nation Base (SPIB) [8] and can be accessed at http ://spib. rice. edu/. The SPIB has been widely used as a reference in many recent works that intend to avoid an exclusively academic focus. Additional information, including studies and articles based on SPIB can be found in the site of the Blind Equalizatiofz Research Group (BERG) [9] at http ://backhoe. ee. cornell. edu/BERG/, which belongs to the Cornell University, in Ithaca, New York, USA. The operation of the Concurrent Equalizer under dynamic channel is described in Section 4.

The microwave channel models to be used may be accessed at http ://spib. rice. edu/spib/microwave. html. These models constitute the impulse response of several real microwave channels obtained from field measurements. Although it is herein presented the complete characterization of each channel in time domain and also in

frequency domain, additional information may be obtained in [10], [11] and [12].

The impulse response of the SPIB microwave channels is obtained under a high sampling rate, at the magnitude of tens of megabauds per second, resulting in impulsive responses with hundreds of samples. This allows each researcher to decimate the resulting sequence by a factor appropriate to its particular interest, without losing significant information. The great majority of the works rarely uses an impulsive response of channel with more than some tens of samples. In this description, in order to maintain a comparison term with recent works in the field [6] [7] [13], the SPIB microwave channels will be decimated to 16 samples. Table 2 identifies the SPIB channels used and establishes the respective designation to be adopted hereinafter. For example, references to channel M4 in this description must be understood as: the channel whose impulse response results in the decimation to 16 samples from the sample sequence of the file chan4. mat from the SPIB database, concerning microwave channels. SPIB File : Sampling rate 1/T of Number of samples in the Designation, in this (microwaves) transmitter in Mbauds/s SPIB file, resulting from the description, of the respective (according to fractional sampling T/2 of impulsive response generated http://spib. rice. edu/spib/mic impulsive response received by decimation of the SPIB file rowave. html) : from the channel : to 16 samples: chan4. mat 30 300 M4 chan9. mat 30 300 M9 chanl4. mat 30 600 M14 Table 2: Microwave channel models in the SPIB database.

In order not to change the location of the zeros of the FIR transfer function of a SPIB channel, the decimation is applied to the frequency domain [2] [7]. Specifically, the number of samples in a SPIB file is extended to the next whole power of 2 plus the addition of null samples in sequence. Then, the FFT (FFT-Fasí Fourier TrM/o) is applied on the extended sequence and the resulting sequence in the frequency domain is decimated to 16 samples. Next, the IFFT (IFFT-Inverse Fast Fourier Transforiii) [2] is applied over the decimated sequence in the frequency domain, resulting in a sequence of 16 samples in the time domain, corresponding to the decimated impulsive response. If the decimation in the time domain were used, aliasing effects would be generated [2], changing, particularly, the position of reflected roods and roots close to the unitary circle in the frequency domain z, and then distorting the characteristics of the SPIB channels.

Another channel model used in this description is the representative of cable TV channels, which may be accessed at http://spib. rice. edu/spib/cable. html. The sampling rate used for these SPIB channels is the usually employed in practical cable TV decoders. This way, in order to maintain a comparison term with the works in the field, these channels will not be decimated. Table 3 identifies the cable TV channel SPIB to be used and establishes the respective designation to be adopted hereinafter. For example, references to channel Cl in this description must be understood as: the channel whose impulse response is given by the sequence of samples of the chanl. mat file of the SPIB database concerning cable TV channels. SPIB File: Number of sample sin the SPIB file, Designation in this resulting from the fractional sampling T/2 description of the (cable TV) of the impulsive response received from the respective impulsive channel: response associated: (according to http ://spib. rice. edu/spib/cable. html.) Chanl. mat 128 Cl

Table 3: Model of cable TV channel from the SPIB database.

In this description, the channels M4, M9, M14 and Cl are characterized by: 1-Module |c (n) | and phase Zc (n) (in degrees) of the impulsive response c (n) resulting from the fractional sampling T/2 of the impulse response c (t) of the channel.

2-The location in plane z of the zeros of the transfer function C (z) of the channel.

3-Theplaceinplanezofthezerosofthetransferfunctions CEVEN (z) and C°DD (z) of the sub-channels (fractional sampling/2 implies odd and even sub-channels [6] [7]). Fig. 3a: #c(n)#. Fig. 3b : #c(n). 1.5 1 o,- 1- t õ |' o ; 0. 5 P \ ° a ; g b -0. 5 o j,'o \s |" ° o -1 o s o o 0 - 1.5-1-0.5 0 . 5 1 1.5 F^l Deri teal Part parte Imaginria parte Real Fig. 3d: Zeros of CEVEN(z) - # and CODD(z) - *. Figure 3: Characterization of channel M4. and Fig. 4a: #c(n)#. Fig. 4b: Zc (ii) in degrees. 1 s S s o 0. 5 0. 5. ' ; 0 ____________ ______________. ; __________ I ? . JE a -0. 5 \/0 0 q , 'o 1 b so o, t o -l-0. 5 0 0. 5 1 1.5 fReal Part Fig. 4c: Zeros of C (z). parte Imaginaria parte Real Fig. 4d: Zeros of CEVEN(z) - # and CODD(z) - *. Figure 4: Characterization of channel M9. Fig. 5a : c (n)#. Fig. 5b : Zc (n) in degrees. 1 w ''- 0. 5 c _ ? 1 1 t :'', c i 5', (CH2 in _ O \ Réai part Fig. 5c : Zeros of C (z). parte Imaginaria parte Real Fig. 5d: Zeros of CEVEN(z) - # and CODD(z) - *. Figure 5: Characterization of channel M14. Fig. 6a: le (n) l. Fig. 6b : Zc (H) in degrees. 2- 2. 1. 5' a i o00 ca CL po au - . 5 "0 E ç) $oooooo -2-1. 5-1. 0. 6 0 0.5 1 1.5 2 ireal Part Fig. 6c : Zeros of C (z). parte Imaginaria parteReal Fig. 6d: Zeros of (zea and CODD(z) - *. Figure 6: Characterization of channel C 1.

The Concurrent Equalizer performance evaluation will be done in reference with an equalizer type CMA (Corastarat Modulus Algorithm) [1] [7]. The CMA FIR transversal Equalizer is perhaps the most widely used and tested in the implementation of the current blind equalizers [14], because, in practical systems, its performance has been reported to be superior to other blind equalizers currently in use [6] [7]. The performance criteria adopted are based on the following simulation results: 1-Graph of the constellation 1 at the output y of the CMA Equalizer after convergence, having the constellation of the source alphabet A as reference, with A represented in the graph by the symbols"+".

2-Graph of the T constellation in the output y of the Concurrent Equalizer after convergence, having the constellation of the source alphabet A as reference, with A represented in the graph by the symbols"+".

3-Comparative graph of ISI (i) curves for the two equalizers, i = 0,2, A, Na-1, where Na is the total number of samples received by fractional sampling T/2 from the channel, and ISI (ì) is the"reverberation"measure in the equalized signal y in instant i, obtained from <BR> <BR> <BR> <BR> ISI = [##Hk# - max#Hk#]/max#Hk# calculated for this instant. H, represents the vh component of<BR> <BR> <BR> i vector H, which contains the coefficients of the impulse response h (7Z), combined with the equalizer and the channel.

4-Comparative graph of MSE (i) curves for the two equalizers, i = 0, 2, A, Na-1, where, MSE (i) is the mean square error between the equalized output y and the original sequence transmitted s, taking into consideration for the average the interval of samples that includes the instant i and the L+L-1 samples previous to it. La is the dimension of channel dispersion defined by the number of non-null samples in the impulse response C (7Z) of the channel. Additionally, this graph demonstrates the horizontal line NT, which defines the maximum permitted MSE level, so that the transference to the renowned DD Equalizer (Direcl Deci, sion) [1] [6] [7] be done. The DD Equalizer acts after the convergence of the CMA Equalizer, intending to reduce its residual MSE (steady state MSE). However, the DD Equalizer can only converge if the steady state MSE of the CMA Equalizer has reached a value inferior to the indicated by the horizontal line NT [7].

The sequence representing the information source s to be transmitted through the channel has average zero, unit variance, uniform distribution, and presents statistic independence between samples.

The noise added to the equalizer input is Gaussian, with zero average, spectrally white and with variance defined by SNR (Signal To Noise Ratio) [1].

Some authors suggest that the dimension of equalizer L be done larger than the dimension of the channel dispersion Lc, so that the extra degrees of freedom so obtained allow the minimization of the equalizer noise gain [15]. However, in order to minimize the haroare cost for implementation purposes, we will adopt L = L, in the following simulations.

The initialization of the vector that defines the filter of the CMA Equalizer and the vector V of the Concurrent Equalizer follows the strategy denominated sigle spike [7], which consists of initializing the vectors with 1 + jO in position , 0 < < L-1, maintaining the elements in other positions null. In [7] it is demonstrated that the optimal value of depends on the position of the sample with maximum absolute value in the channel impulse response #c(n)"# sequence, denominated channel cursor. However, as c (ra) is not known at first, the universally accepted practice is to make = L/2. If the equalizer does not converge with = L/2, it is normal that the receiver system tries to make a few attempts around = L/2 until the equalizer converges, that is, # = L/2~#, # = 1,2,# [16]. We will adopt such heuristic in case of initial convergence failure. The cases for which it was necessary to apply it can be identified by L12.

The adaptation step of the CMA Equalizer filter is 7Z, and the adaptation steps of the Concurrent Equalizer filters are 77,, and 77,,. These parameters are experimentally adjusted in order to meet the tradeoff between fast convergence and low steady state MSE.

With unitary variance in the information source s, for 16-QAM and 64-QAM, 7 presents better results in the neighborhood of value lxl0-3, and for 256-QAM, in the neighborhood of 1 x 10-4. These results agree with the experiments involving 16-QAM and 256-QAM modulation in [7].

In the following graphs, the following events are considered indication of good performance : 1-The degree in which the points of the output constellation y of the equalizer (r or t) concentrate around the + symbols of alphabet A. Under ideal performance, this graph would show all of the output points y projected in the intersection of the lines that define the + symbols and the alphabet A.

2-The rate at which the curve ISI (i) decreases with i and how low and invariable is the value of ISI (i) after convergence (steady state ISI).

3-The rate at which the curve MSE (i) decreases with i and how low and invariable is the value of MSE (i) after convergence (steady state MSE).

Below are the results of the simulations which assess the comparative performance between the CMA Equalizer and the Concurrent Equalizer.

Modulation 16-QAM SNR=35dB-Channel M14 Fig. 7a: F (CMA) Fig. 7b: T (CONC)

Fig. 7c : ISI (i) Fig. 7d: MSE (i) Figure 7: Comparative results between the CMA Equalizer and the Concurrent Equalizer (CONC) for channel M14, modulation 16-QAM (γ - 1. 32), SNR=35dB.

Parameters: Na = 100000, # = 1#10-3, #v = 1#10-3, #w = 1#10-2, L = Lc = 16 and # = 6.

Modulation 64-QAM SNR=35dB-Channel M9 Fig. 8a: F (CMA) Fig. 8b : T (CONC) Fig. 8C : ISI (i) Fig. 8d: MSE (i) Figure 8: Comparative results between the CMA Equalizer and the Concurrent Equalizer (CONC) for channel M9, modulation 64-QAM (y=1. 380953), SNR=35dB.

Parameters: Na = 100000, # = 1#10-3, #v = 1#10-3, #w = 1#10-2, L = Lc =16 and =2.

Modulation 256-QAM SNR=35dB-Channel Cl Fig. 9a : r (CMA) Fig. 9b: # (CONC) Fig. 9c : ISI (j) Fig. 9d: MSE (i) Figure 9: Comparative results between the CMA Equalizer and the Concurrent Equalizer (CONC) for channel Cl, modulation 256-QAM (y=1. 395295), SNR=35dB.

Parameters: Na = 100000, # = 1#10-4, #v = 1#10-4, #w = 1#10-3, L = Lc = 128 and # = 63.

Modulation 16-QAM SNR=35dB-Channel M4 Fig. 10a : r (CMA) Fig. lOb : T (CONC) Fig. 10c : ISI () Fig. lOd : MSE (i)

Figure 10: Comparative results between the CMA Equalizer and the Concurrent Equalizer (CONC) for channel M4, modulation 16-QAM (γ = 1. 32), SNR=35dB.

Parameters: Na = 30000, # = 1#10-3, #v = 1#10-3, #w = 1#10-2, L = Lc = 16 and # = 8.

Modulation 64-QAM SNR=35dB-Channel M4 Fig. 11 a : F (CMA) Fig. lib : T (CONC) Fig. lie : ISI (i) Fig. lid : MSE (i) Figure 11: Comparative results between the CMA Equalizer and the Concurrent Equalizer (CONC) for channel M4, modulation 64-QAM (γ = 1. 380953), SNR=35dB.

Parameters: Na = 30000, # = 1#10-3, #v = 1#10-3, #w = 1#10-2, L = Lc = 16 and # = 6.

Note that, in none of the first three examples shown (Figures 7,8 and 9), the CMA Equalizer reaches a MSE low enough so that the transference to the DD Equalizer is successfully accomplished. These are typical cases in which the popular and renowned CMA-DD Equalizer would fail in meeting its objective. For the three examples, the Concurrent Equalizer not only has surpassed the MSE level for transference, but also reached a MSE level much inferior and less variable than the CMA Equalizer. The same

observation is valid for the comparative ISI between the equalizers.

The Concurrent Equalizer outperforms the CMA Equalizer, even in those situations in which the CMA reaches the transference MSE, such as demonstrated, for example, in Figure 10 for modulation 16-QAM. Note also that for the same channel and modulation 64-QAM, the CMA Equalizer reaches only a marginal steady state MSE, as shown in Figure 11.

Note that in the examples for which the channel rotates the received constellation, the Concurrent Equalizer is capable to correct this undesirable effect, while the CMA Equalizer does not have this capability. This is a particularity of the Concurrent Equalizer, which allows the simplification of the synchronism system. It is important to point out that, upon performing joint equalization with carrier phase retrieval and/or symbol sampling instant retrieval, the Concurrent Equalizer presents an inertia and a response time shorter than those of the CMA Equalizer followed by a phase corrector (de-spinner). This is a decisive characteristic for the good performance of the Concurrent Equalizer in time varying channels.

It is important to reaffirm that the Concurrent Equalizer surpasses the performance of the CMA Equalizer, not only regarding the MSE, but also the ISI. In all cases, the Concurrent Equalizer quickly reached a much lower and more stable ISI level than CMA Equalizer. This behavior of the Concurrent Equalizer demonstrates that its best performance compared to the CMA Equalizer does not depend on the phase rotation imposed by the channel to the constellation received, since the ISI is defined from the module of the impulse response h (M). If, in the examples above, a system to correct the phase rotation on the received constellation were previously added to both equalizers, the performance of CMA Equalizer would not be changed regarding the ISI due to the phase invariance of this equalizer [7], while, on the other hand, the performance of the Concurrent Equalizer would tend to improve.

Comparative Tests under Dynamic Channel- Results Obtained.

In the following simulation set, the performance of the Concurrent Equalizer is evaluated against the CMA Equalizer, both operating under temporal variation in the channel, situation which characterizes the operation under dynamic channel.

The objective is to determine the sensibility of both equalizers to the speed of

variation in the channel. To do so, the following analysis is based on the channels suggested by M. Gosh [17], whose work referred to herein studies the digital television system ATSC 8-VSB proposed by the Advanced Television Systems Committee [18] for the equalization performance.

The ATSC 8-VSB digital system was proposed in the USA in 1993, with the objective to substitute the veteran NTSC analog system for television broadcast. Using the same channel with the 6MHz bandwidth of the NTSC system, the ATSC 8-VSB was conceived to present a superior performance, even under high levels of interference, noise and multi-path effects [19].

Since this description considers all signals as baseband signals [l], for the sake of this simulation, it is enough to use as information source s the 8-VSB alphabet generator A= {-1. 53,-1. 09,-0. 66,-0.22,0.22,0.66,1.09,1.53} to represent the eight possible signal amplitudes (8-PAM) baseband generated by a 8-VSB transmitter. Since the Channel Encoder of a ATSC 8-VSB transmitter"randomizes"with uniform distribution the baseband signal for transmission efficiency purposes [20], the source s presents a uniform probabilistic distribution with statistic independence between samples. Note also, from the definition of alphabet A, that the variance of s is unitary. The unitary variance is assumed for s as partial representation of the CAG system effect present in any digital system.

The dynamic channel model adopted in this study is the one suggested in [17] and is specified in Table 4. Components of the Amplitude Delay s] Delay [samples] Signal Received Principal Ray: 1.000 0.00 39 Echo 1 : 0.100-1.80 0 Echo 2: 0.100 0.15 42 Echo 3 : 0. 316 sinf2. 0 77 FI J 0.316, f = 0 Echo 4: 0.200 5.70 161 Echo 5: 0.126 18.0 426

Table 4: Specification of the dynamic channel mode adopted. The column"Delay [samples]"is obtained by dividing the values in column"Delay [, Us]" by the fractional sampling interval T/2 of the receiver, where 11T = F, 10. 76MHz is the sampling rate of the symbols in the ATSC 8-VSB transmitter [19] [18], considering as a sample of index 0 the one with lower delay. The integer variable n represents the index of the nth channel regressor received, or the index of the n symbol sent by the transmitter and, therefore, presents temporal spacing T associated to the interval between the indexed samples. The real constant f represents the speed of temporal variation for each type of dynamic channel to be considered. For example, 0. 05Hz< f <0. 5Hz models dynamic channels resulting from the reflection of signals by a tall building whose structure is swaying in its natural frequency of mechanical oscillation (due to the wind, etc...), and 2Hz < f < 5Hz models channels with rapid and periodic fading Cutter) generated by the reflection of the signal by aircraft flying in low altitude [17].

Therefore, from Table 4, the impulsive response obtained by fractional sampling T/2 of the dynamic channel in question has its representation in the z domain given by The ATSC 8-VSB system includes a baseband filter (Nyquist filter) of the raised-cosiyie type, with a roll-off of 11.5% [18] [17]. As this filter affects the baseband signal, the channel model to be considered must include the effect of this filter in the performance evaluation of the equalizer. The raised-cosine filter of the ATSC 8-VSB system is an analog filter that presents a transfer function H (f), according to Figure 12.

Figure 12: Graphic representation of the transference function H (f) of the raised-cosine filter of the ATSC 8-VSB system.

The discrete impulsive response obtained by fractional sampling T/2 of the continuous impulsive response of the analog filter defined by the graph of Figure 12 is given by Equation (2) and is graphically represented in Figure 13.

In the Equation (2) N = 64 is the number of samples considered in this study for the impulsive response h,, (i), and a = 0. 115 is the parameter that defines the 11.5% zoll-off of the filter in the frequency domain. The integer variable i represents the index of the ith sample received from the channel and, therefore, presents temporal spacing T/2 associated with the interval between the indexed samples.

Figure 13: Graph of hrc (i) for N = 64 and a = 0. 115.

In the following simulation set, the effect of the raised-cosine filter is included by effecting the convolution of the impulsive response of the channel defined by (1) with the impulsive response of the raised-cosine filter given by (2). Therefore, the dimension Le of the global channel dispersion? including the effect of the raised-cosine filter? is given by the sum of the dimension of channel dispersion with the dimension N of the filter dispersion, that is, Lc = 427+64 = 491.

The performance criteria adopted are based on the following simulation results: 1-Graph of the CMA Equalizer output yCMA(n), where ru is the index of the n th channel regressor received, having the source alphabet constellation A as reference. A is represented in the graph by the set of dashed lines.

2-Graph of the Concurrent Equalizer output ycoNc (n) having the source alphabet constellation A as reference. A is represented in the graph by the set of dashed lines.

3-Graph of the MSEoM) curve of the CMA Equalizer, with MSECMA(n) being the mean square error between the yCMM(n) output and 6 (n)}, Q{#} is the operator that represents the 8-VSB quantizer. The averaging interval for the MSECMAW(n) includes the instant n and the previous Lu-l samples. Additionally, this graph shows the horizontal line NT that defines the maximum permitted MSE level, so that the transference to the DD Equalizer be possible.

4-Graph of the MSEcoNc (Z2) curve of the Concurrent Equalizer, with MSEcoNc (n) being the mean square error between the yoN, (n0 output and Q{yCONC(n)}. The averaging interval for the MSECONC(n) includes the instant n and the previous L,-I samples. Additionally,

this graph shows the horizontal line NT that defines the maximum permitted MSE level, so that the transference to the DD Equalizer be possible.

A SNR= lOOdB was adopted, since the objective is to measure the sensibility of the equalizer to the channel variations, and not the sensibility to the noise. As the channel varies, it was considered reasonable to adopt a dimension of the equalizer L that exceeds in 50% the dimension Lu = 491 of the global channel dispersion, that is, it was adopted L = 738. The initialization of vector V, both for the CMA Equalizer and the Concurrent Equalizer, follows the usual technique single spike, which, in this simulation, consists of initializing V with the value 1.0 in position = 65, maintaining null the elements in the other positions.

The adaptation steps were fixed in 7 = 2x 10-4 for the CMA Equalizer and razz = 2 x 10-4 and 77,, = 2 x 10-3 for the Concurrent Equalizer.

Below are the simulations of the comparative performance between the CMA Equalizer and the Concurrent Equalizer, both operating under dynamic channel for variation speeds f = 0Hz (static channel), f = 10Hz, f = 20Hz, f = 50Hz and f = 100Hz.

Fig. 14a: yc (n) Fig. 14b: YCONC (n) Fig. 14c: MSECMA (n) Fig. 14d: MSECONC (n) Figure 14: Comparative results between the CMA Equalizer and the Concurrent Equalizer (CONC) for the channel specified in Table 4 with f = OHz, including the effect of raised-cosine filter.

Fig. 15a: y. (n) Fig. 15b: yCONC (n) Fig. 15c: MSECMA(n) Fig. 15d: MSECONC(n) Figure 15: Comparative results between the CMA Equalizer and the Concurrent Equalizer (CONC) for the channel specified in Table 4 with f = 10Hz, including the effect of raised-cosine filter.

Fig. 16' : y. (n) Fig. 16b: YCONC (n) Fig. 16c: MSECMA (n) Fig. 16d: MSE... (n) Figure 16: Comparative results between the CMA Equalizer and the Concurrent Equalizer (CONC) for the channel specified in Table 4 with f = 20Hz, including the effect of raised-cosi7ie filter.

Fig. 17a : yCMA(n) Fig. 17b : yCONC(n) Fig. 17c: MSEc., (fez) Fig. 17d : MSECONC(n) Figure 17: Comparative results between the CMA Equalizer and the Concurrent Equalizer (CONC) for the channel specified in Table 4 with f = 50Hz, including the effect of raised-cosine filter.

Fig. 18a: yCMA (n) Fig. 18b: YCONC (n) Fig. 18c: MSE,,, « (n) Fig. 18d: MSEcoNc (n) Figure 18: Comparative results between the CMA Equalizer and the Concurrent Equalizer (CONC) for the channel specified in Table 4 with f = 100Hz, including the effect of raised-cosine filter.

The experimental results under dynamic channel operation demonstrate that the Concurrent Equalizer presents a performance superior to the CMA Equalizer in the task to deconvolve channels that present rapid temporal variations.

Note that, opposite to the Concurrent Equalizer, for f = 50Hz and f = 100Hz the CMA Equalizer cannot reach and maintain the MSE lever required for the transference to the DD Equalizer. Note also that, for all cases, the MSE regime level reached by the Concurrent Equalizer is much lower and more invariable when compared to the level accomplished by the CMA Equalizer.

These results suggest that the Concurrent Equalizer will be able to largely contribute for the performance improvement of mobile digital systems.

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