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Maximum Likelihood Timing and Carrier Frequency

Offset Estimation for OFDM Systems

With Periodic Preambles

Hung-Tao Hsieh, Student Member, IEEE, and Wen-Rong Wu, Member, IEEE

Abstract—Symbol timing offset (STO) and carrier frequency

offset (CFO) estimation are two main synchronization opera-tions in packet-based orthogonal frequency division multiplexing (OFDM) systems. To facilitate these operations, a periodic pream-ble is often placed at the beginning of a packet. CFO estimation has been extensively studied for the case of two-period preambles. In some applications, however, a preamble with more than two pe-riods is available. A typical example is the IEEE802.11a/g wireless local area network system, which features a ten-period preamble. Recently, researchers have proposed a maximum likelihood (ML) CFO estimation method for such systems. This approach first estimates the received preamble using a least squares method and then maximizes the corresponding likelihood function. In addi-tion to the standard calculaaddi-tions, this method requires an extra procedure to solve the roots of a polynomial function, which is disadvantageous for real-world implementations. In this paper, we propose a new ML method to solve the likelihood function directly and thereby perform CFO estimation. Our method can obtain a closed-form ML solution, without the need for the root-finding step. We further extend the proposed method to address the STO estimation problem as well as derive a lower bound on the estimation performance. Our simulations show that while the performance of the proposed method is either equal to or better than the existing method, the computational complexity is lower.

Index Terms—Frequency offset, maximum likelihood (ML), orthogonal frequency division multiplexing (OFDM), synchronization.

I. INTRODUCTION

O

RTHOGONAL frequency division multiplexing (OFDM) is known as an efficient modulation technique [21], [22]. However, the performance of OFDM systems is sensitive to both symbol timing offset (STO) [19], [20] and carrier fre-quency offset (CFO). STO will reduce the effective cyclic prefix (CP) length and induce intersymbol interference, while CFO will damage the orthogonality among subcarriers and thereby induce intercarrier interference. For typical OFDM receivers, STO and CFO have to be estimated and compensated before data detection can be conducted.

Manuscript received April 23, 2008; revised October 25, 2008, January 7, 2009, and March 4, 2009. First published April 3, 2009; current version published October 2, 2009. The review of this paper was coordinated by Dr. C. Cozzo.

The authors are with the Department of Communication Engineering, National Chiao Tung University, Hsinchu 300, Taiwan (e-mail: dow.cm93g@ nctu.edu.tw; wrwu@faculty.nctu.edu.tw).

Digital Object Identifier 10.1109/TVT.2009.2019820

Estimation methods for CFO and STO in OFDM systems can be classified into the following two categories: 1) data aided and 2) blind. The former is more suitable for packet-based transmission, while the latter is appropriate for continuous transmission such as broadcasting. Blind methods exploit the periodic structure of CPs to accomplish the estimation task [1]–[7]. Data-aided methods insert a known preamble, or pilot symbol, in front of each data packet such that it can easily be used by the receiver to achieve synchronization [9]–[18]. In this paper, we consider only the data-aided method.

CFO estimation usually consists of a fractional part and an integer part. Most researchers focus on how to estimate the fractional part, which is also the focus of this paper. For integer part estimation, see [9] and [10]. It has been shown that the performance of OFDM systems is greatly affected by CFO [30], and an accurate CFO estimation is required for real-world applications. A maximum likelihood (ML) CFO estimator using a preamble with two identical pilot symbols was first proposed in [11]. Using the same periodic preamble and taking null subcarriers into consideration, Huang and Letaief [12] propose a method that is able to estimate both fractional and integer CFOs. To avoid the extra overhead required in [12], Schmidl and Cox [13] introduce a preamble composed of two OFDM symbols: The first one has two identical periods (to estimate the fractional CFO and STO), and the second one has a special correlation with the first one (to estimate the integer CFO). To improve the performance, Morelli and Mengali [14] extend this area of research to treat preambles with periodicities of greater than two. Using the approach in [14], one can remove the second pilot symbol as required in [13]. As an improved version, Minn et al. [15] propose a CFO estimation based on the best linear unbiased estimation principle. Note that Morelli and Mengali [14] and Minn et al. [15] still use the same STO estimator as that in [13]. When the number of periods is greater than two, the method in [11] is no longer optimal. An ML CFO estimator for this problem was proposed in [16]. However, the required computational complexity is high. To alleviate this problem, a low-complexity approach was then proposed in [17]. Another simplified algorithm was also proposed in [18]. However, due to excessive approximation in the likelihood function, the performance of the CFO estimation in [18] does not approach the Cramér–Rao lower bound (CRLB) [25].

In this paper, we focus on CFO and STO estimation in the OFDM system with a periodic preamble. Specifically, we consider a preamble with more than two periods. The ML CFO

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estimation for the system has been considered in [17]. The method in [17] is essentially a two-step approach: it first es-timates the received preamble with a least squares (LS) method and then maximizes the corresponding likelihood function. In addition to regular computations, this method requires an extra procedure to solve for the roots of the derivative of the like-lihood function. Thus, its computational complexity is higher, and the cost for real-world implementations is also increased.

In this paper, we develop a new ML method that solves the likelihood function directly for the CFO-estimation problem. Our method generates a closed-form ML solution, and the root-finding procedure is not required. As a result, the computational complexity and the implementation cost are lower than those in [17], while the performance of the proposed method is either equal to or better than that in [17]. The proposed method is further extended to STO estimation, and a theoretical lower performance bound is derived. Note that the performance bound for STO estimation has not previously been addressed in the literature. This paper is organized as follows. In Section II, the CFO-estimation method in [17] is briefly reviewed. The proposed CFO- and STO-estimation procedures are described in Sections III and IV. A lower bound on STO estimation performance is presented in Section V. Our simulation results are reported and discussed in Section VI. Our conclusions are presented in Section VII.

II. EXISTINGAPPROACH

In this section, we briefly review the algorithm proposed in [17]. Let the preamble in the OFDM system be periodic with period N and length QN . Denote the preamble signal as s(k), where k = 0, 1, . . . , QN− 1. The preamble is placed at the beginning of a packet and is subsequently transmitted through a wireless channel. Denote the channel response as h(k) and the output signal as x(k). Then, we have x(k) = s(k)∗ h(k), where ∗ denotes the convolution operation. Assume that the maximum channel delay is N . Then, we can discard the first received N samples and retain the periodic property of the preamble x(k). Thus, the received preamble can be expressed as [1]

y(k) = ej2πεkN x(k) + w(k) (1)

where k = N, N + 1, . . . , QN− 1, ε is CFO, and w(k) repre-sents additive white Gaussian noise with a variance of σw2. We can perform an index transformation by letting k = mN + n, where m = 1, . . . , Q and n = 0, . . . , N− 1 such that x(k) =

x(mN + n). For notational simplicity, we further let xm(n) =

x(mN + n), denoting the nth sample of the mth period of x(k). Due to periodicity, we have xp(n) = xq(n) for p, q∈

{1, . . . , Q}. Similarly, we can define ym(n) = y(mN + n) =

y(k), and wm(n) = w(mN + n) = w(k). Let K = Q−1, and

y(n) = [ y1(n) y2(n) · · · yK(n) ]T

x(n) = [ x1(n) x2(n) · · · xK(n) ]T

w(n) = [ w1(n) w2(n) · · · wK(n) ]T. (2)

In addition, we define four matrices as follows:

Y = [ y(0) y(1) · · · y(N − 1) ]

X =x(0) x(1)ej2πεN · · · x(N − 1)ej2πε(N−1)N  W = [ w(0) w(1) · · · w(N − 1) ] A = ⎡ ⎢ ⎢ ⎣ ej2πε 0 · · · 0 0 ej2πε·2 · · · 0 .. . ... . .. ... 0 0 · · · ej2πε·K ⎤ ⎥ ⎥ ⎦ . (3)

The received preamble in (1) can then be rewritten as

Y = AX + W. (4)

The method in [17] uses a two-step approach: it first estimates

X using an LS method and then estimates CFO by maximizing

the likelihood function. Since the noise is a Gaussian random variable, y(n) is a Gaussian random vector with a covariance matrix of σ2wI, where I denotes the identity matrix. For a givenA, the LS estimate of X can be expressed as XLS= (1/K)AHY ≡ A+Y, where (·)H denotes the Hermitian operation. Substituting XLS back into (4), we can obtain the log-likelihood function as Λ(A) = N

n=1 y(n) − AA+y(n) 2 = N· trace((I − AA+)RY), where RY = E[YYH]. The (p, q)th entry of R

Y is (1/N )N −1n=0yp(n)yq∗(n), p, q∈ [1, K] [28]. The desired CFO estimation can then be derived as

ˆ ε = arg min ε trace (I − AA+)RY  = arg{max ε a HR Ya} (5)

where a is a vector consisting of the diagonal elements of A. It was shown in [26] that

aHR Ya =

K−1 m=−(K−1)

b(m)ej2πmε (6)

where b(m) =q−p=m(1/N )N −1n=0yp(n)yq∗(n). Taking the derivative of (6) with respect to ε and letting the result be zero, we obtain K−1 m=1 mb(m)zm= K−1 m=1 mb(−m)z−m (7)

where z = ej2πε. Equation (7) can be rewritten as

Im K−1  m=1 mb(m)zm  = 0 (8)

where Im(·) is an operator that isolates the imaginary part of a scalar value. Denote the set containing the roots of (8) by Ω. The CFO can then be estimated as follows [17]:

ˆ

ε = 1

j2πln(ˆz) (9)

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The procedure for CFO estimation in [17] can now be summarized as follows.

1) Construct the correlation matrixRY. 2) Calculate the coefficient of (8) usingRY. 3) Find the nonzero roots of (8).

4) Substitute the roots into (6), find the maximum root, and calculate ˆε using (9).

As we see, (8) requires a root-finding operation. Thus, a set of suboptimum algorithms to address this issue was proposed in [17]. Unfortunately, these suboptimum methods cannot effectively reduce the computational complexity while still maintaining good performance.

III. PROPOSEDML CFO ESTIMATION

In this section, we develop a new CFO estimation method that solves the likelihood function directly. The signal model we use is the same as that in (4). We assume that each data packet is transmitted through a slow-fading channel with an impulse response of h(k), k = 0, . . . , L− 1. Here, the h(k)s have Rayleigh distributions, and they are statisti-cally independent. Note that the time-domain preamble sig-nal is obtained from the discrete Fourier transform of the frequency-domain preamble signal, and the frequency-domain preamble signal is generally a white sequence. From the central limit theorem, the time-domain preamble signal can then be approximated as a white Gaussian sequence. Thus, the channel output x(k), which equals L−1l=0 h(l)s(k− l),

and the received preamble y(k) in (1) can be approxi-mated as Gaussian sequences. Let the variance of the time-domain preamble signal, i.e., s(k) be σs2. Then, the variance of x(n) equals σx2= E{L−1j=0L−1l=0 h(j)s(k− j)h(l)∗s(k− l)∗} = σs2L−1l=0 |h(l)|2= σ2sσh2, and that of y(k) equals σ2x+

σw2. Note that s(k) can be a psuedonoise sequence. In such a case, σs2indicates the averaged preamble power of s(k).

Let f (·) be a probability density function. Then, we explicitly write out the log-likelihood function of ε as follows [1]:

Λ(ε) = ln ⎧ ⎨ ⎩  n∈ ˜I f (y(n)) ⎫ ⎬ ⎭ = ln ⎧ ⎪ ⎨ ⎪ ⎩  n∈ ˜I f (y(n))  m∈[1,K]  n∈ ˜I f (ym(n)) ·  m∈[1,K]  n∈ ˜I f (ym(n)) ⎫ ⎪ ⎬ ⎪ ⎭ = ln ⎧ ⎨ ⎩  n∈ ˜I f (y(n)) f (y1(n))· · · f (yK(n)) ·  m∈[1,K]  n∈ ˜I f (ym(n)) ⎫ ⎬ ⎭. (10)

It is clear that the last term in (10), i.e., m∈[1,K],n∈ ˜I×

f (ym(n)), is independent of ε [1]. As a result, this term can be dropped. Let

u(n) = ej2πεnN [ x1(n)ej2πε · · · xK(n)ej2πε·K]T. (11) We then rewrite (4) as Y = U + W, where U = AX = [u(0), u(1), . . . , u(N − 1)]. Then, y(n) = u(n) + w(n). DefineRu= E[u(n)uH(n)] andRy= E[y(n)yH(n)]. Then, we have Ru= σ2x ⎡ ⎢ ⎢ ⎣ 1 e−j2πε · · · e−j2π(K−1)ε ej2πε 1 · · · e−j2π(K−2)ε .. . ... . .. ... ej2π(K−1)ε ej2π(K−2)ε · · · 1 ⎤ ⎥ ⎥ ⎦ (12)

andRy=Ru+ σw2I, where I is an identical matrix. Thus, we can express f (y(n)) as [23], [24]

f (y(n)) = πKdet(Ry) −1exp−y(n)HR−1y y(n). (13) According to the matrix inversion lemma [8], we derive the inverse ofRyas

R−1

y = σw−2I −

σ−4w Ru

1 + σw−2E{uHu}. (14) Note that for n∈ ˜I, we have

Eyp(n)y∗q(n)  =  σx2+ σw2, if q− p = 0 σx2e−j2πε(q−p), if q− p = 0 (15) where p, q∈ [1, K]. As a result, R−1y = σw−2I − [Ru/(σw4 + 2wσ2x)], and f (yp(n)) = exp  −yp(n)y∗p(n) σ2x+σw2  π (σx2+ σ2w) (16) where p∈ [1, K]. Thus, the exponential term in (13) becomes

y(n)HR−1 y y(n)= σw−2 K  p=1 yp(n)yp∗(n) −C0 K  p=1 K  q=1 yp(n)y∗q(n)ej2π(q−p)ε = σ−2w−C0 K  p=1 yp(n)y∗p(n) −2C0Re K−1 p=1 K  q>p yp(n)yq∗(n)ej2π(q−p)ε ! (17)

where C0= σ2x/(σw4 + Kσw2σ2x), and Re{·} denotes the opera-tion that isolates the real part of the indicated complex variable.

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Dropping the superfluous terms and substituting (13)–(17) into (10), we finally express the log-likelihood function as

Λ(ε) = N −1 n=0 ln ⎧ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎨ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎩ σx2+ σ2w Kexp−y(n)HR−1 y y(n)  det(Ry) exp ⎡ ⎢ ⎢ ⎣− K p=1 yp(n)y∗p(n) σ2x+σ2w ⎤ ⎥ ⎥ ⎦ ⎫ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎬ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎭ (18) = C1+ C2φ + C3 K−1 p=1 K  q>p |γpq| cos(ψpq) (19) where γpq= N −1 n=0 yp(n)y∗q(n) (q≥ p and p ≥ 1) (20) ψpq= 2πε(q− p) + ∠γpq, φ = K  p=1 γpp (21) C1= N· ln  σx2+ σw2 K det(Ry)  (22) C2= (1− K) ρ 2 σw2(1 + (K− 1)ρ) (23) C3= 2C2 (1− K)ρ (24) ρ = σ 2 x σx2+ σw2. (25)

Note that φ is the received signal energy and that det(Ry) is a constant, independent of ε. The detailed derivation of (19) is provided in Appendix A. Ignoring unrelated terms, we obtain the log-likelihood as Λ(ε)∝ K−1 p=1 K  q>p |γpq| cos(ψpq). (26) To maximize the function, we first take a derivative of Λ(ε) with respect to ε and obtain

∂εΛ(ε) =− K−1 p=1 K  q>p 2π(q− p)|γpq| sin(ψpq). (27)

Thus, we have an alternative expression to that in (8). Now, the problem is how to solve (27). Since (27) involves a non-linear sine function, a closed-form solution will be difficult to

calculate. Here, we use a simple approximation method to overcome the problem. Using (20) and (1), we obtain

γpq= ej2πε(p−q) N −1 n=0 |x1(n)|2+ N −1 n=0 wp(n)w∗q(n) + ej2πε(pN +p) N −1 n=0 x1(n)w∗p(n) + ej2πε(pN −q) N −1 n=0 x∗1(n)wq(n). (28)

In (28), we have used the periodic property that x1(n) =

xp(n) = xq(n). Now, if the noise level is low, the noise related terms in (28) can be ignored. We then have

∠γpq≈ 2πε(p − q). (29)

From (29), we write

ψpq≈ 2πε(q − p) + 2πε(p − q) = 0. (30) From (30), we can then assume that sin(ψpq)≈ ψpq and ap-proximate the expression in (27) by

∂εΛ(ε) − K−1 p=1 K  q>p 2π(q− p)|γpq|(ψpq). (31) Setting the result in (31) to zero, we can estimate CFO as

ˆ ε =− K−1 p=1 K q>p|γpq|(q − p)∠γpq 2πK−1 p=1 K q>p |q − p|2pq| . (32)

Note that the approximation in (30) will become exact if noise is not present and if ε is the true CFO. In other words, (27) and (31) will have the same zero-crossing point although the two functions are different, indicating that (31) and (27) will yield the same optimum solution. If noise is present, however, (31) and (27) will not have the same optimum solution. The accuracy of the solution in (31) depends on the signal-to-noise ratio (SNR) in (28). We define the SNR in (28) as SNRγ and that in (1) as SNR. Then, SNR = σ2xw2, as typically defined. From (28), it is simple to see that

SNRγ =

N2σ4x

N σw4 + 2N σx2σw2 =

N· SNR2

1 + 2SNR. (33)

From (33), we can see that SNRγcan be much larger than SNR as long as N is reasonably large and SNR is not very low. Subsequently, the approximation in (31) will introduce only a small error for a wide SNR range. As a simple example, let N = 16 and SNR = 0 dB. From (33), we obtain SNRγ = 7.27 dB, which is much higher than SNR.

Note that the proposed estimate requires that we extract the phase from γpq. It is simple to see that the result is only unambiguous when |∠γpq| < π. For a particular combination of p and q, the estimation range for CFO is|ε| ≤ 1/[2(q − p)].

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TABLE I

COMPUTATIONALCOMPLEXITYCOMPARISON FOR THEALGORITHM IN[17]AND FOR THEPROPOSEDALGORITHMS

Since the maximum value for q− p is K − 1, the estimation range for CFO is |ε| ≤ 1/[2(K − 1)]. When K is large, the range becomes small. In the following, we propose a method to remedy this problem. The basic idea is to apply the phase-unwrapping procedure. We first calculate the phase angle for each γpq. Then, for each p, we calculate the phase difference of ∠γpq, q = p + 1, p + 2, . . . , K. Let dr,s denote the phase dif-ference, i.e., dr,s =∠γrs− ∠γr(s−1), r = 1, 2, . . . , K− 2 and

s = r + 2, r + 3, . . . , K. Since the maximum value of|dr,s| is π, whenever|dr,s| > π, the phase need to be unwrapped. This can be performed with the following operation:

dr,s= 

dr,s− 2π if dr,s> π

dr,s+ 2π if dr,s<−π. (34) For a value of r, the dr,svalues should have the same signs. We can use this property to further correct occasional errors. Let

g be the sum of all dr,s values, i.e., g = K−2

r=1 K

s=r+2dr,s. Then, we use the sign of g to determine the sign of dr,sand to evaluate∠γpk, k = p + 1, . . . , K. Finally, the unwrapped∠γpq can be written (with q≥ p + 2) as

∠γpq=∠γp(p+1)+ q  s=p+2

dp,s. (35)

Substituting (35) into (32), we can estimate CFO. Using our proposed procedure, the CFO estimation range can be greatly extended up to|ε| < 1/2.

Now, the procedure for our proposed ML CFO estimation can be summarized as follows.

1) Construct all γpq’s, where p∈ [1, K − 1] and q ∈ [p + 1, K], and calculate their amplitude.

2) Use the phase unwrapping scheme to estimate the phase of γpq.

3) Substitute the results into (32), and calculate the ML estimate.

Clearly, the proposed estimate does not require the root-finding procedure, and this, in turn, effectively reduces the computa-tional complexity. Step 1) above is similar to the calculation of

R in Section II. However, our method is easier since we only

have to compute γpqfor q > p.

In this paragraph, we compare the computational complexity of the proposed ML estimate with that of the algorithm in [17]. Three algorithms are proposed in [17], which are referred to as algorithms A, A , and B. While algorithm A is optimal,

algorithms A and B are suboptimal. Table I summarizes this result. In Table I, MUL, ADD, LN, ABS, PH, and DIV denote the multiplication, addition, natural logarithm, absolute value, phase derivation, and division operations, respectively. In ad-dition, the algorithm proposed in this section is referred to as proposed algorithm I, and the one in Section IV is termed pro-posed algorithm II. For the propro-posed algorithms, we consider the worst case in which all the phase differences dr,s need to be unwrapped. Fig. 1 shows several examples of how Q and N affect the complexity. Note that the computational complexity for the root-finding procedure in [17] is not included here. For convenience, we treat all operations other than addition as multiplications. As we can see, the computational complexity for the proposed algorithm is slightly lower than that for algorithms A and B in [17], and algorithm A in [17] is the lowest. However, algorithm A truncates the polynomials with order higher than two in (6), i.e., Λ(z) =2m=−2b(m)zm. This impacts the estimation accuracy. Note that we can always truncate the summation terms in (32) and thereby reduce the computational complexity of proposed algorithm I. Since sub-optimum approaches are not our focus, we will not consider the details here. We will now discuss the computational complexity of the root-finding procedure. As shown in [27] and [29], the root-finding procedure requires O(K3) multiplications. Table I shows that the computational complexity of algorithm A is

O(N K2). Thus, the computational complexity of the root-finding procedure will be high when K is large. Furthermore, its implementation cost will also be higher, since we may need dedicated electronic circuitry to implement this function.

It is well known that the performance of an unbiased estima-tor is bounded by the CRLB [25]. If the variance of an unbiased estimator reaches the CRLB, we consider the estimator effi-cient. Following the procedure to derive performance bounds in [25], we can calculate the CRLB for our CFO estimation procedure. Let ˆε be an estimate of ε. The CRLB for our CFO

estimation is then CRLB(ˆε) =− 1 E " 2 ∂ε2Λ(ε) # = (8π 2ρ)−1σ2 w(1 + (K− 1)ρ) E $ K−1 p=1 K q>p (q− p)2Reγpqej2πε(q−p) %

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Fig. 1. Computational complexity comparison for the algorithm in [17] and proposed algorithm I. Note that the complexity of the root-finding procedure is not considered in [17]. = σw2(1 + (K− 1)ρ) 2ρN σx2K−1 p=1 K q>p (q− p)2 = 1 + K· SNR 2N· SNR2 1 K−1 p=1 K q>p (q− p)2 (36)

where E[·] denotes the expectation.

IV. PROPOSEDJOINTML STOANDCFO ESTIMATION

In this section, we extend the method developed in Section III to solve the STO-estimation problem. The core idea is to apply a sliding data window for the received (Q + 1)N samples; each window covers the preamble in the context of a particular timing offset. We perform the ML CFO estimation for data in each window and store the estimated CFO and the corre-sponding maximum log-likelihood. Thereafter, the estimated CFO with the largest log-likelihood is selected as the ML CFO estimate. The corresponding window position is taken as the ML STO estimate. Let the window size be QN , and define the set Vi={y(i), y(i + 1), . . . , y(i + QN − 1)} to be the received data in window i. Since the maximum delay is shorter than N , it is clear that 0≤ i ≤ N − 1. If we let the STO be θ, Vθwill cover the complete preamble. In Appendix B,

we show that the log-likelihood function for Vi can be ex-pressed by Λi(ε) = C1i+ C2iφi+ C3i Q−2 p=0 Q−1 q>p &&γi pq&&cos ψipq (37) where the superscript i indicates that all the variables are calculated within Vi, and C1i, C2i, and C3i can be treated as window independent. Thus, we can simplify the above log-likelihood function using

Λi(ε)≈ C2φi+ C3 Q−2  p=0 Q−1  q>p

&&γpqi &&cos ψipq (38) where C2and C3are the same as those in (23) and (24). Since the received signal power φi is independent of CFO, we can estimate CFO using (32) as

ˆ εi= Q−2 p=0 Q−1 q>p &&γi pq&&(q− p)∠γpqi Q−2 p=0 Q−1 q>p|q − p| 2&&γi pq&& . (39)

Note that the upper bound in the summation terms of (39) is Q instead of K. The estimated STO is then

ˆ θ = arg max i  Λi( ˆεi)= iopt. (40)

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Now, the procedure for the proposed joint ML STO and CFO estimation can be summarized as follows.

1) Calculate γipq and its amplitude, where i∈ [1, N], p ∈ [0, Q− 2], and q ∈ [p + 1, Q − 1].

2) Use the phase unwrapping procedure outlined above to calculate∠γi

pq.

3) Substitute the results into (38) and (39), and calculate Λiεi) and ˆεi.

4) Find ioptsuch that Λioptεiopt) > Λiεi), i= i opt. 5) The ML STO estimate is iopt, and the ML CFO estimate

is then ˆεiopt.

As we can see from the above procedure, the computational complexity of the algorithm will be N times higher than that in Section III. Note also that the upper limit of p is Q− 2 instead of K− 2. In other words, we have an extra period for CFO estimation. By leveraging the sliding window structure, we can effectively reduce the computational complexity in calculating γi

pq. Similar to the definition of γpq, we obtain

γpqi =i+N −1n=i yp(n)[yq(n)]∗. Then, it is simple to show that

γpqi = γpqi−1+ yp(i + N− 1) [yq(i + N− 1)]∗

−yp(i− 1) [yq(i− 1)]∗. (41) From (41), we can see that except for i = 0, the calculation of

γi

pqrequires only two complex multiplications and two complex additions. This will greatly reduce the required computational complexity in the scenario of joint STO and CFO estimation. The required computational complexity has been summarized in Table I.

We can also obtain the CRLB for the CFO estimate. All we have to do is to replace K with Q in (36). Since Q = K + 1, the CRLB is lower than that in (36). Note that the STO is a discrete value. No performance lower bounds have been reported to date in the literature. In Section V, we will derive a lower bound to address this omission.

V. PERFORMANCEANALYSIS OFSTO ESTIMATION

In this section, we analyze the performance of the proposed STO estimation method. We first redefine (38) as Λi(ε) =

C2φi+ C 3ξi, where φi= K  p=0 i+N −1 n=i yp(n)yp∗(n) = K  p=0 N −1 n=0 xp(n)x∗p(n) + wp(n)w∗p(n) + 2Re  xp(n)wp∗(n) exp ' j2πεpN + n N () (42) ξi= K−1 p=0 K  q>p

&&γpqi &&cos ψpqi

= K−1 p=0 K  q>p N −1 n=0 xp(n)w∗q(n) exp ' j2πεqN + n N ( + wp(n)x∗q(n) exp ' −j2πεpN + n N ( + wp(n)w∗q(n) exp (j2πε(q− p)) + xp(n)x∗q(n). (43)

Note here that φiand ξiare random variables. The mean value of Λi(ε), which is denoted by μi

Λ, is equal to C2μiφ+ C3μiξ, where μi

φ and μiξ are the mean of φi and ξi, respectively. The variance of Λican be expressed by νi

Λ= C22νφi + C32νξi+ 2C2C3κi

φξ, where νφi and νξi denote the variance of φi and ξi, respectively, and κiφξ the covariance between φi and ξi. The whole set of Vi, 0≤ i ≤ N − 1, has (Q + 1)N samples, and it may cover three regions. The first region consists of the noise samples, the second region the periodic preamble samples, and the third region the data samples. We denote these regions by IN, IP, and ID. Thus, the signal variance in IN is σw2, that in IP is σx2+ σw2, and that in ID is σ2d+ σ2w, where σ2d represents the variance of data samples. Recall that θ is the actual STO in the system. Using θ as a reference, we can have the following three cases for the value of i: 1) i = θ; 2) i < θ; and 3) i > θ (0≤ i ≤ N − 1). The statistics of φi and ξi are different across these three cases. In Appendix C, we provide a detailed derivation of μiφ, μiξ, νφi, νξi, and κiφξ.

For the proposed STO-estimation algorithm, an error occurs when iopt= θ. Thus, we can define the error probability of STO estimation as P (∪i,i=θ{Λθ< Λi}), where P (·) denotes the probability of a certain event. Note that the evaluation of P (Λθ< Λi) only requires 1-D integration. If the log-likelihood functions for all i’s are independent and identically distributed, we have P (∪i,i=θ{Λθ< Λi}) =

i,i=θP (Λθ< Λi). Unfortunately, the log-likelihood functions are not inde-pendent. As a result, we have to conduct multidimensional integration, which is both complex and difficult. Therefore, we propose a simple alternative to overcome the problem. Instead of the exact error probability, we attempt to derive a lower bound.

As shown in [13], the likelihood function is approximately Gaussian. We denote the distribution of Λi using G(μi

Λ, νΛi), where G(·) denotes the Gaussian distribution. Consider the joint density function of Λi and Λj. Using the Gaussian as-sumption, we write the bivariate Gaussian distribution as

P (Λi, Λj) = 1 2π· νi Λ· νΛj · * 1− Cc(i, j) · exp ' zij 2 (1− Cc(i, j)) ( (44) where 1≤ i, j ≤ N, and zij = Λi− μi Λ 2 νi Λ +  Λj− μjΛ 2 νΛj −2Cc(i, j) Λi− μiΛj− μjΛ  + νi Λ· νΛj (45) Cc(i, j) = Eij)− μi Λμj Λ + νi Λ· νΛj . (46)

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Fig. 2. Comparison of simulated and theoreticalP (Λθ> Λj).

Note that Cc(i, j) is the corresponding correlation coefficient. The numerator of Cc(i, j) is expressed as

Eij)= μiΛμΛj∗+ C22κijφφ+ C32κijξξ

+ C2C3κijφξ+ C2C3κijξφ (47) where κijabdenotes the covariance of ai and bj∗ (ai, bj ∈ {φi, φj, ξi, ξj}). The main idea here is only to calculate P (Λθ>

Λi) for all i’s (except for i = θ) and then use the result to derive a lower bound. Thus, we only have to consider Cc(i, θ) as

κiθφφ= 2σx2σw2(QN− |i − θ|) (48) κiθξξ= Q(Q− 1)σ2xσ2w , N 3(2Q− 1) − 1 2|i − θ| -+1 2QN (Q− 1)σ 4 w (49) κiθφξ= κiθξφ= (Q− 1)2N σ2xσ2w + (Q− 1) (N − |i − θ|) σx2σw2. (50) Substituting (45)–(50) into (44), we can then evaluate

P (Λθ> Λi). Given this definition, we have P (Λθ> Λi) = .

−∞ .Λθ

−∞P (Λi, Λθ)dΛidΛθ. Simulations have been conducted to evaluate the validity of our theoretical results. Using the scenario depicted in Section VI, we compare the theoretical and simulated P (Λθ> Λi) in Fig. 2. In the figure, we see that the theoretical P (Λθ> Λi) is close to the simulated result. If we let Pmin= min

i=θ P (Λ

θ> Λi), we can then treat P

minas an upper bound for the correct probability of STO estimation (i.e.,

iopt= θ). Thus, we can then have a lower bound for the error probability of STO estimation (LBSTO) as 1− Pmin.

VI. SIMULATIONS ANDDISCUSSIONS

In this section, we report our simulation results, which eval-uate the performance of the proposed algorithms. We adopt a Rayleigh multipath channel with an exponential power decay and five channel taps. The preamble, which is generated from a

Fig. 3. Performance comparison of CFO estimation, the algorithm in [17], and proposed algorithm I; SNR= 10 dB.

Fig. 4. BER comparison for systems with and without CFO.

frequency-domain binary-phase-shift-keying-modulated signal, has ten periods, and each period has 16 samples. The data following the preamble are transmitted using a 16-quadratic-amplitude-modulation scheme. The mean square error (MSE) of the estimated CFO is used as a performance measure. We first consider the CFO-only estimation problem. In this case, the first received N samples are discarded. As previously mentioned, we term the proposed approach for this scenario as algorithm I (as described in Section III). We compare the proposed ML estimator with that in [17]. One optimum algorithm (algorithm A) and two suboptimum algorithms (algorithm A and B) in [17] are simulated. Fig. 3 shows the simulation result for SNR at 10 dB. In the figure, we can see that the performances of algorithms A and B are poorer. Algorithm A and the proposed algorithm offer a similar level of performance that is very close to the CRLB. To evaluate the impact of CFO on system perfor-mance, we conduct simulations for systems with and without CFO. For the system with CFO, we first use the proposed method to estimate CFO and then conduct CFO compensation. Fig. 4 shows the BER comparison for ε = 0.2. As we can see in

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Fig. 5. Performance comparison for CFO estimation, the algorithm in [17], and proposed algorithm II; SNR= 10 dB.

Fig. 6. Performance comparison for CFO estimation, the algorithm in [17], and proposed algorithms I and II;N = 16, and Q = 10.

the figure, the BER performance degrades slightly when CFO is present.

We then consider the case of the joint STO and CFO esti-mation process. In this case, discarding the first received N samples is not necessary. As a result, one additional pream-ble is availapream-ble. This means that the proposed method may offer better performance compared with the previous scenario. However, the price we pay for the additional STO estimation is the increase in computational complexity. As mentioned, we name this approach proposed algorithm II (as explained in Section IV). Using a similar approach, the method in [17] can also be used to estimate STO. However, its computational com-plexity increases much more than our method. Fig. 5 shows the simulation result for the CFO estimate. The proposed method offers good performance. Only when CFO is very close to

±0.5 does the performance of the proposed algorithms degrade.

Fig. 6 shows the CFO estimation result for various SNRs. In the figure, we see that the proposed method still works well for SNRs as low as −5 dB. The algorithms in [17] perform

Fig. 7. Error probability of STO estimation (proposed algorithm II).

Fig. 8. Performance comparison for STO estimation (SNR= 2 and 10 dB).

well until SNR reaches −7 dB, which is somewhat better than the proposed algorithms. However, when SNR falls below

−8 dB, the proposed algorithms again outperform those in

[17]. This may be because the correlation matrix in (6) is very noisy, and the roots therefore cannot be solved reliably. Fig. 7 shows the error probability for the STO estimation. We observe that the derived lower bound for the STO estimation is tight when the SNR is high. Note that the error probability we de-fined is only relevant to performance evaluation. If the channel response is shorter than the CP (which is the typical case), we can always has some tolerance for the STO estimation. Thus, there is no need to calculate the exact channel delay. In real-world applications, it is a common practice to reduce the estimated STO by a couple of samples when conducting STO compensation. Another property is that STO estimation performance is not particularly impacted when CFO is close to 0.5. In the literature, there exist a number of STO estimation methods. We select the two algorithms proposed in [13] and [18] for comparison. Fig. 8 shows the MSE curves for these approaches and for the proposed algorithms (θ = 8). The figure confirms that the proposed method performs best.

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VII. CONCLUSION

In this paper, we have developed new algorithms for ML STO and CFO estimation in OFDM systems with periodic pream-bles. The proposed algorithms do not have to calculate the roots of the derivative of the likelihood function. The operations are simple, and the computational complexity is low. With the proposed method, we can simultaneously solve the STO and CFO estimation problems. We also derive a lower bound for the STO estimation error. Simulations show that the proposed methods offer good performance, and the derived lower bound is tight when the SNR is high.

APPENDIXA DERIVATION OF(19)

The likelihood function in (18) can be rewritten as

Λ(ε) = N −1 n=0 ln ⎧ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎨ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎩ σx2+ σ2w Kexp−y(n)HR−1 y y(n)  det(Ry) exp ⎡ ⎢ ⎢ ⎣− K p=1 yp(n)y∗p(n) σ2x+σ2w ⎤ ⎥ ⎥ ⎦ ⎫ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎬ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎪ ⎭ = N −1 n=0 ln" σ2x+ σw2 K(det(Ry))−1 # + K p=1 yp(n)yp∗(n) σ2x+ σ2w − y(n) HR−1 y y(n) ! . (51)

Then, by substituting (17) into (51), we derive the log-likelihood function as Λ(ε) = N −1 n=0 ln $ σx2+ σ2w K det(Ry) % + K p=1 yp(n)yp∗(n) σx2+ σ2w σw−2− C0 K  p=1 yp(n)yp∗(n) + 2C0Re K−1 p=1 K  q>p yp(n)y∗q(n)ej2π(q−p)ε ! ! = N −1 n=0 ln" σx2+ σw2 K(det(Ry))−1 # + , 1 σx2+ σ2w σ−2w − C0 -K  p=1 yp(n)yp∗(n) + 2C0Re K−1 p=1 K  q>p yp(n)y∗q(n)ej2π(q−p)ε ! ! = (1− K)σ 4 x σw22x+ σw2) (Kσx2+ σ2w) K  p=1 N −1 n=0 yp(n)y∗p(n) + 2C0Re K−1 p=1 K  q>p N −1 n=0 yp(n)y∗q(n)ej2π(q−p)ε ! + N ln" σx2+ σ2w K(det(Ry))−1 # (52)

where C0= σx2/(σ4w+ Kσ2wσx2). By substituting (21) and (25) into (52), we can express (52) as

Λ(ε) = C1+ C2 K  p=1 γpp + C3Re K−1 p=1 K  q>p γpqej2π(q−p)ε ! = C1+ C2 K  p=1 γpp + C3Re K−1 p=1 K  q>p |γpq|ej∠γpq ej2π(q−p)ε ! = C1+ C2φ + C3 K−1 p=1 K  q>p |γpq| cos(ψpq) (53) where ψpq, φ, C1, C2, and C3are defined as (22)–(24).

APPENDIXB DERIVATION OF(38)

We assume that the channel noise, the received preamble, and the received data are statistically uncorrelated with one another. We define three column vectorsy1(n) = [y0(n), . . . ,

yQ−1(n)]T, y

2(n) = [y1(n), . . . , yQ−1(n)]T, and y3(n) = [y0(n), . . . , yQ−2(n)]T and their autocorrelation matrix asRyk for k = 1, 2, and 3. Note that i is the window index of (37), and θ is the real STO. Therefore, (19) can be derived for the following two cases: 1) i≤ θ and 2) i > θ. Using the approach taken to derive (18), we obtain the log-likelihood function for the first case as

Λi≤θ(ε) = ln ⎧ ⎪ ⎪ ⎪ ⎨ ⎪ ⎪ ⎪ ⎩ n=i+N −1 n=i f (y(n)) Q  k=1 f (yk−1(n)) ⎫ ⎪ ⎪ ⎪ ⎬ ⎪ ⎪ ⎪ ⎭ = θ−1  n=i ln  f (y2(n)) f (y1(n))· · · f (yQ−1(n)) ) + i+N −1 n=θ ln  f (y1(n)) f (y0(n))· · · f (yQ−1(n)) ) (54) =θ− i N C12+ i + N − θ N C 1 + θ−1  n=i C2 Q−1 p=1 yp(n)yp∗(n)

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+ θ−1  n=i C3Re Q−2 p=1 Q−1 q>p yp(n)yq∗(n)ej2π(q−p)ε ! + i+N −1 n=θ C3 Re Q−2 p=0 Q−1 q>p yp(n)y∗q(n)ej2π(q−p)ε ! + i+N −1 n=θ C2 Q−1 p=0 yp(n)yp∗(n) (55) where C12= N· ln  σx2+ σ2w K det(Ry2)  (56) C1 = N· ln  σx2+ σ2w Q det(Ry1)  (57) C2 = (1− Q) ρ 2 σw2 (1 + (Q− 1)ρ) (58) C3 = =, 2C 2 (1− Q)ρ. (59)

Similarly, we can derive the log-likelihood function for

i > θ as Λi>θ(ε) = i+N −1 n=θ+N ln  f (y3(n)) f (y0(n))· · · f (yQ−2(n)) ) + θ+N −1 n=i ln  f (y1(n)) f (y0(n))· · · f (yQ−1(n)) ) (60) =i− θ N C13+ θ + N− i N C 1 + i+N −1 n=θ+N C2 Q−2 p=0 yp(n)y∗p(n) + i+N −1 n=θ+N C3Re Q−3 p=0 Q−2 q>p yp(n)yq∗(n)ej2π(q−p)ε ! + θ+N −1 n=i C2 Q−1 p=0 yp(n)yp∗(n) + θ+N −1 n=i C3 Re Q−2 p=0 Q−1 q>p yp(n)yq∗(n)ej2π(q−p)ε ! (61) where C13= N· ln  σ2x+ σ2w K det(Ry3)  . Sincey2(n), i≤ n ≤ θ − 1 in (54) and y3(n), θ + N ≤ n ≤

i + N− 1 in (60) contain Q − 1 periods of the preamble,

det(Ry2) and det(Ry3) will be the same as det(Ry) [see (22)]. Consequently, C12= C13= C1. From (22)–(24), we see that

C1, C2, and C3can be calculated by replacing Q andRy1with

K andRy, respectively, in (57)–(59). When Q is reasonably large, we obtain C1 ≈ C1, C2 ≈ C2, and C3 ≈ C3. Thus, we rewrite (55) and (61) as Λi≤θ(ε) θ−1  n=i C3Re Q−2 p=1 Q−1 q>p yp(n)y∗q(n)ej2π(q−p)ε ! + i+N −1 n=θ C3Re Q−2 p=0 Q−1 q>p yp(n)y∗q(n)ej2π(q−p)ε ! + C1+ θ−1  n=i C2 Q−1 p=1 yp(n)yp∗(n) + i+N −1 n=θ C2 Q−1 p=0 yp(n)yp∗(n) (62) Λi>θ(ε) θ+N −1 n=i C3Re Q−2 p=0 Q−1 q>p yp(n)yq∗(n)ej2π(q−p)ε ! + i+N −1 n=θ+N C3Re Q−3 p=0 Q−2 q>p yp(n)y∗q(n)ej2π(q−p)ε ! + C1+ i+N −1 n=θ+N C2 Q−2 p=0 yp(n)y∗p(n) + θ+N −1 n=i C2 Q−1 p=0 yp(n)y∗p(n). (63)

We now approximate Q−1p=1yp(n)yp∗(n) and Q−2

p=1 Q−1

q>p ×

yp(n)yq∗(n)ej2π(q−p)ε in (62) with

Q−1

p=0 yp(n)yp∗(n) and Q−2p=0 Q−1q>p yp(n)yq∗(n)ej2π(q−p)ε, respectively. Similarly, we also approximate Q−2p=0 yp(n)yp∗(n) and Q−3p=0Q−2q>p yp(n)y∗q(n)ej2π(q−p)ε in (63) with Q−1 p=0 yp(n)y∗p(n) and Q−2 p=0 Q−1 q>p yp(n)yq∗(n)ej2π(q−p)ε, respectively. Given these approximations, Λi≤θ(ε) and Λi>θ(ε) can be identically written as

Λi(ε) C1+ C2 i+N −1 n=i Q−1 p=0 yp(n)yp∗(n) +C3 i+N −1 n=i Re Q−2 p=0 Q−1 q>p yp(n)yq∗(n)ej2π(q−p)ε ! . (64)

Using the approach that is similar to that in Appendix A, we finally obtain Λi(ε) C1+ C2φi+ C3Re Q−2 p=0 Q−1 q>p &&γi pq&&cos ψpqi ! (65) where γi pq= i+N −1 n=i yp(n)yq∗(n), φi= Q−1 p=0 γppi , and ψi

pq= 2πε(q− p) + ∠γipq. Note that the approximations we made are equivalent to adding|θ − i| samples (noise or data)

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in calculating the likelihood functions. Since the number of samples in the ith sliding data window QN is usually much larger than the number of added samples |θ − i|, the added samples will not change the likelihood functions too much. The approximation errors also depend on the distance between the window position and the actual STO, i.e.,|θ − i|. When the distance is larger, the error is also larger. However, if the distance is larger, the likelihood function tends to be smaller, and a larger error is then tolerable. Finally, we note that the added samples, either noise or data, are uncorrelated with the preamble samples.

APPENDIXC DERIVATIONS OFμi

φ, μiξ, νφi, νξi,ANDκiφξ

We first note that θ is the real STO in the system. Using θ as a reference, we have the following three cases for the value of i: 1) i = θ; 2) i < θ; and 3) i > θ (0≤ i ≤ N − 1). For the first case, the window covers the preamble data only (IP). Thus, (42) and (43) can be simplified to

φθ= Q−1 p=0 θ+N −1 n=θ xp(n)x∗p(n) + wp(n)w∗p(n) + 2Re  xp(n)wp∗(n) exp ' j2πεpN + n N () (66) ξθ= Q−2 p=0 Q−1 q>p θ+N −1 n=θ xp(n)x∗q(n) + xp(n)wq∗(n) exp ' j2πεqN + n N ( + wp(n)x∗q(n) exp ' −j2πεpN + n N ( + wp(n)w∗q(n) exp (j2πε(q− p)) . (67) The mean values of φiand ξifor the first case are then

μθφ,1= QN σ2x+ σw2 (68)

μθξ,1=QN (Q− 1)

2 σ

2

x. (69)

The corresponding variance values are

νφ,1θ = 2QN σx2σw2 (70) νξ,1θ =QN (Q− 1) 2 σ 4 w + σ2xσ2wQN (Q− 1)(2Q − 1) 3 . (71)

The corresponding covariance value is

κθφξ,1= QN (Q− 1) σ2xσ2w . (72) Here, κi

φξ,j denotes κiφξ in the jth case discussed. For the second case, the window covers the sets IN and IP. Thus, φi

and ξican be expressed as

φi= θ−1  n=i w0(n)w∗0(n) + i+N −1 n=θ x0(n)x∗0(n) + w0(n)w∗0(n) + 2Re x0(n)w0∗(n) exp  j2πεn N  + Q−1 p=1 i+N −1 n=i xp(n)x∗p(n) + wp(n)wp∗(n) + 2Re  xp(n)w∗p(n) exp ' j2πεpN + n N () (73) ξi= Q−1 q>0 θ−1  n=i w0(n)x∗q(n) exp  −j2πεn N  + w0(n)w∗q(n) exp(j2πεq) + Q−1 q>0 N +i−1 n=θ x0(n)x∗q(n) + x0(n)w∗q(n) exp ' j2πεqN + n N ( + w0(n)x∗q(n) exp  −j2πεn N  + w0(n)w∗q(n) exp(j2πεq) + Q−2 p=1 Q−1 q>p i+N −1 n=i xp(n)x∗q(n) + xp(n)w∗q(n) exp ' j2πεqN + n N ( + wp(n)x∗q(n) exp ' −j2πεpN + n N ( + wp(n)wq∗(n) exp (j2πε(q− p)) . (74) Their mean values are

μiφ,2= (QN + i− θ) σx2+ σ2w + (i− θ)σx2 (75) μiξ,2= (Q− 1)(N + i − θ)σx2 +(Q− 1)(Q − 2) 2 N σ 2 x (76)

the corresponding variance values are

νφ,2i = 2σx2σ2w[QN + i− θ] (77) νξ,2i =QN (Q− 1) 2 σ 4 w+ σ22wN (Q− 1) · , (Q− 1) ' 2 + i− θ N ( +(Q− 2)(2Q − 3) 3 -(78)

and the covariance value is

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For the third case, the window covers sets IP and ID, and we write φiand ξias φi= Q−2 p=0 i+N −1 n=i xp(n)x∗p(n) + wp(n)w∗p(n) + 2Re × , xp(n)wp∗(n) exp ' j2πεpN + n N (- ! + θ+N −1 n=i xQ−1(n)x∗Q−1(n) + wQ−1(n)w∗Q−1(n) + 2Re $ xQ−1(n)wQ−1∗ (n) × exp ' j2πε(Q− 1)N + n N ( %! + i+N −1 n=θ+N xQ−1(n)x∗Q−1(n) + wQ−1(n)wQ−1 (n) + 2Re $ xQ−1(n)wQ−1 (n) × exp ' j2πε(Q− 1)N + n N ( %! (80) ξi= Q−3 p=0 Q−2 q>p i+N −1 n=i xp(n)x∗q(n) + xp(n)w∗q(n) exp ' j2πεqN + n N ( + wp(n)x∗q(n) exp ' −j2πεpN + n N ( + wp(n)w∗q(n) exp (j2πε(q− p)) + Q−2 p=0 θ+N −1 n=i xp(n)x∗Q−1(n) + xp(n)w∗Q−1(n) exp ' j2πε(Q− 1)N + n N ( + wp(n)x∗Q−1(n) exp ' −j2πεpN + n N ( + wp(n)w∗Q−1(n) exp (j2πε(Q− p − 1)) + Q−2 p=0 i+N −1 n=θ+N xp(n)x∗Q−1(n) + xp(n)w∗Q−1(n) exp ' j2πε(Q− 1)N + n N ( + wp(n)x∗Q−1(n) exp ' −j2πεpN + n N ( + wp(n)w∗Q−1(n) exp (j2πε(Q− p − 1)) . (81)

Thus, the mean values are

μiφ,3= (QN + θ− i) σx2+ σ2w + (i− θ) σ2d+ σ2w (82)

μiξ,3= (Q− 1)(N − i + θ)σx2+(Q− 1)(Q − 2)

2 N σ

2 x (83)

the variance values are

νφ,3i = 2σ2xσw2(QN− i + θ) + 2(i − θ)σ2dσw2 (84) νξ,3i = σx2σ2wN (Q− 1) × , (2Q− 3) ' 1 +θ− i N ( +(Q− 2)(2Q − 3) 3 + 1 -+QN (Q− 1) 2 σ 4 w+ (Q− 1)2(i− θ)(σd2+ σw2) (85) and the covariance value is

κiφξ,3= (Q− 1)σ2xσ2w[QN + 2(θ− i)] . (86)

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Hung-Tao Hsieh (S’08) received the B.S. degree

in physics in 2000 from the National Central Uni-versity, Taoyuan, Taiwan, and the M.S. degree in electro-physics in 2002 from the National Chiao Tung University (NCTU), Hsinchu, Taiwan, where he is currently working toward the Ph.D. degree with the Department of Communication Engineering.

His research interests include detection/estimation theories and communication signal processing.

Wen-Rong Wu (M’89) received the B.S. degree

in mechanical engineering from Tatung Institute of Technology, Taipei, Taiwan, in 1980 and the M.S. degrees in mechanical and electrical engineer-ing and the Ph.D. degree in electrical engineerengineer-ing from the State University of New York, Buffalo, in 1985, 1986, and 1989, respectively.

Since August 1989, he has been a faculty member with the Department of Communication Engineer-ing, National Chiao Tung University, Hsinchu, Taiwan. His research interests include statistical signal processing and digital communication.

數據

Fig. 1. Computational complexity comparison for the algorithm in [17] and proposed algorithm I
Fig. 3. Performance comparison of CFO estimation, the algorithm in [17], and proposed algorithm I; SNR = 10 dB.
Fig. 5. Performance comparison for CFO estimation, the algorithm in [17], and proposed algorithm II; SNR = 10 dB.

參考文獻

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