Skip to content

Advertisement

  • Research
  • Open Access

SNR walls in eigenvalue-based spectrum sensing

  • 1Email author,
  • 1,
  • 1 and
  • 1
EURASIP Journal on Wireless Communications and Networking20172017:109

https://doi.org/10.1186/s13638-017-0899-y

Received: 12 October 2016

Accepted: 6 June 2017

Published: 19 June 2017

Abstract

Various spectrum sensing approaches have been shown to suffer from a so-called signal-to-noise ratio (SNR)-wall, an SNR value below which a detector cannot perform robustly no matter how many observations are used. Up to now, the eigenvalue-based maximum-minimum-eigenvalue (MME) detector has been a notable exception. For instance, the model uncertainty of imperfect knowledge of the receiver noise power, which is known to be responsible for the energy detector’s fundamental limits, does not adversely affect the maximum-minimum-eigenvalue (MME) detector’s performance. While additive white Gaussian noise (AWGN) is a standard assumption in wireless communications, it is not a reasonable one for the maximum-minimum-eigenvalue (MME) detector. In fact, in this work, we prove that uncertainty in the amount of noise coloring does lead to an SNR wall for the maximum-minimum-eigenvalue (MME) detector. We derive a lower bound on this SNR wall and evaluate it for example scenarios. The findings are supported by numerical simulations.

Keywords

  • Spectrum sensing
  • Eigenvalue-based
  • SNR wall

1 Introduction

The recent years have seen an ever-growing demand for wireless spectrum not least due to the rise of the smartphone in consumer markets. However, as a result of the licensing policies of the preceding decades, most of the radio spectrum can only be used by fixed licensees, many of which only make use of their spectral bands at certain places or times. To alleviate the need for spectrum and make better use of the given resources, opportunistic spectrum access (OSA) [1] has emerged as a sub-field of cognitive radio. In opportunistic spectrum access (OSA), a spectral band can be used by unlicensed transceivers, so-called secondary users (SUs), if they are certain that the licensee of the band, the so-called primary user (PU), is not using it.

To make sure the occupancy status of a band is reliably detected, the SU senses the spectrum before using it. The goal of spectrum sensing is to decide between two hypotheses, the first of which states that the band of interest is free (\(\mathcal {H}_{0}\)), such that the SU can make use of it. The second hypothesis states that the band is occupied (\(\mathcal {H}_{1}\)), in which case the SU should refrain from accessing the band. The requirements spectrum sensing algorithms have to meet are quite demanding, e.g., the IEEE 802.22 standard for cognitive wireless regional area networks [2] states that an SU receiver should be able to reliably detect a primary user (PU) signal at a signal-to-noise ratio (SNR) of −22 dB. There are good reasons for these demanding requirements, like, e.g., the hidden terminal problem ([3] Ch. 14.3.3).

A number of spectrum sensing algorithms have been proposed in the literature [46]. Under the ergodicity assumption, these algorithms are typically able to meet the above requirement, i.e., if enough samples are available, the probability density functions (PDFs) of the test statistics are well separable. However, due to model uncertainties caused by, e.g., colored or non-stationary background noise, non-ideal filters and imperfectly estimated parameters, detection algorithms can exhibit so-called SNR walls, i.e., SNR values, below which the detectors cannot robustly [7] decide between \(\mathcal {H}_{0}\) and \(\mathcal {H}_{1}\). The existence of SNR walls has been established for the energy detector, the matched filter detector, and the cyclostationarity detector [810]. A spectrum sensing algorithm that, to the best of our knowledge, has not been linked to the signal-to-noise ratio (SNR)-wall problem is the popular eigenvalue-based maximum-minimum-eigenvalue (MME) detector.

The contributions of this paper are manifold. We identify noise coloring as a model uncertainty adversely affecting the maximum-minimum-eigenvalue (MME) detector. Then, we show that uncertainty in the amount of noise coloring leads to an signal-to-noise ratio (SNR)-wall for the maximum-minimum-eigenvalue (MME) detector by using noise coloring to derive a lower bound on the signal-to-noise ratio (SNR)-wall of the maximum-minimum-eigenvalue (MME) detector. Finally, we support the analytical results with numerical simulations.

The rest of the paper is structured as follows. In Section 2, we introduce our signal model alongside the test statistic of the maximum-minimum-eigenvalue (MME) detector. Section 3 formally defines the term signal-to-noise ratio (SNR)-wall, while Section 4 explains why colored noise is a reasonable assumption in wireless communication. In Section 5, a lower bound on the signal-to-noise ratio (SNR)-wall for the maximum-minimum-eigenvalue (MME) detector is derived. Example scenarios with concrete values for the lower bound from Section 5 are given in Section 6. A numerical evaluation of our results can be found in Section 7, while Section 8 concludes the work.

2 Signal model and MME test statistic

Consider the discrete time complex baseband signal x(n) observed at a secondary system receiver, where n denotes the discrete time index. The task of a spectrum sensing algorithm is to decide between the following two hypotheses
$$ \begin{aligned} \mathcal{H}_{0} : x(n)&=\eta(n)\\ \mathcal{H}_{1} : x(n)&=s(n)+\eta(n), \end{aligned} $$
(1)

where s(n) represents a primary user (PU) signal, while η(n) stands for additive noise. For the sake of simplicity, no channel fading effects are taken into account.

Throughout this work, the primary user (PU) is assumed to transmit a linearly modulated signal with symbol length T symbol exhibiting a rectangular pulse shape. The signal is oversampled at the receiver with an integer oversampling rate given by \(M=\frac {T_{\text {symbol}}}{T_{\text {sample}}}\), where T sample denotes the sampling period. The decision whether the band under observation is free (\(\mathcal {H}_{0}\)) or occupied (\(\mathcal {H}_{1}\)) is based on a block of N samples. In the decision process, samples from p different receivers are considered. The samples available at the fusion center at time instant n are given by
$$ \begin{aligned} \mathbf{x}(n) = \left[\vphantom{\left. x_{2}(n),\ldots, x_{p}(n),\ldots, x_{p}(n-Q)\right]}x_{1}(n),x_{1}(n-1),\ldots, x_{1}(n-Q),\right.\\ \left. x_{2}(n),\ldots, x_{p}(n),\ldots, x_{p}(n-Q)\right]^{\mathrm{T}}, \end{aligned} $$
(2)
where the subscript indicates which receiver the samples are from. Each receiver contributes a consecutive set of Q+1 samples, where the quantity Q+1 is the so-called smoothing factor [11]. The inclusion of samples from different receivers as well as samples from different points in time allows the maximum-minimum-eigenvalue (MME) detector to exploit correlation from both domains in the detection process. For simplicity, all receivers are assumed to experience the same signal-to-noise ratio (SNR). The vectors s(n) and η(n) are defined analogous to x(n), leading to the concise representation
$$ \mathbf{x}(n) = \mathbf{s}(n) + \boldsymbol{\eta}(n). $$
(3)

We consider a scenario with a single primary user (PU) transmitter and multiple SU receivers. The receivers are assumed to be perfectly synchronized, i.e., \(s_{i}(n)|_{i=1}^{p} = s(n)\). Signal and noise are generated by mutually independent stationary random processes. The primary user (PU) signal s(n) is zero-mean, has variance \(\sigma _{s}^{2}\), and its symbols are independent, i.e., s(n) and s(n+M) are independent and identically distributed (i.i.d.). The receiver noise η i (n) is zero-mean and has variance \(\sigma _{\eta }^{2}\) for all i. The noise vector η(n) is distributed according to a circularly symmetric complex Gaussian distribution, i.e., \(\boldsymbol {\eta }(n) \sim \mathcal {CN}_{p(Q + 1)}(\boldsymbol {0}, \mathbf {R}_{\boldsymbol {\eta }})\).

Considering the fact that both the signal and the noise are zero-mean, the statistical covariance matrices can be obtained as
$$ \begin{aligned} \mathbf{R}_{\mathbf{s}} &= \mathbb{E}\left[{\mathbf{s}(n) \mathbf{s}(n)^{\mathrm{H}}}\right]\\ \mathbf{R}_{\boldsymbol{\eta}} &= \mathbb{E}\left[{\boldsymbol{\eta}(n) \boldsymbol{\eta}(n)^{\mathrm{H}}}\right]\\ \mathbf{R}_{\mathbf{x}} &= \mathbb{E}\left[{\mathbf{x}(n) \mathbf{x}(n)^{\mathrm{H}}}\right]\\ &= \mathbf{R}_{\mathbf{s}} + \mathbf{R}_{\boldsymbol{\eta}}, \end{aligned} $$
(4)
where (·)H denotes the complex conjugate transpose. We assume that the received signal x(n) is covariance ergodic ([12], pp. 531), such that the sample covariance matrix
$$ \hat{\mathbf{R}}_{\mathbf{x}}(N) = \frac 1{N-Q} \sum\limits_{n=Q}^{N-1}\mathbf{x}(n)\mathbf{x}(n)^{\mathrm{H}} $$
(5)
asymptotically converges to the statistical covariance matrix, i.e.,
$$ \underset{N \rightarrow \infty}{\text{lim}} \hat{\mathbf{R}}_{\mathbf{x}}(N) = \mathbf{R}_{\mathbf{x}}. $$
(6)
The analytic derivations in this work target the well-known maximum-minimum-eigenvalue (MME) detector [11]. Its test statistic is composed of the eigenvalues of the received signal’s sample covariance matrix. The test statistic and its accompanying decision rule are given by
$$ \Gamma_{\text{MME}}(\mathbf{x}, N) = \frac{\lambda_{\text{max}}\left(\hat{\mathbf{R}}_{\mathbf{x}}(N)\right)}{\lambda_{\text{min}}\left(\hat{\mathbf{R}}_{\mathbf{x}}(N)\right)} \overset{\scriptscriptstyle{\mathcal{H}_0}}{\underset{\scriptscriptstyle{\mathcal{H}_{1}}}{\lessgtr}} \gamma, $$
(7)

where λ max(·) and λ min(·) denote the largest and smallest eigenvalue of a matrix respectively and γ stands for the predefined decision threshold. If Γ MME(x,N)<γ, we decide \(\mathcal {H}_{0}\), while for Γ MME(x,N)≥γ, we decide \(\mathcal {H}_{1}\). Since both sample and statistical covariance matrices are positive-semidefinite and thus all of their eigenvalues are ≥0, the test statistic Γ MME(x,N) is always ≥1.

3 SNR walls in spectrum sensing

Additive white Gaussian noise (AWGN) is a standard assumption in wireless communications research and for many problems in the field, it is a reasonable one. Indeed, a classical result from information theory states that additive Gaussian noise represents the worst case in point-to-point communication [13], which makes it a fair choice for performance evaluation. However, modeling the receiver noise as additive white Gaussian noise (AWGN) is only an approximation of reality and for eigenvalue-based spectrum sensing, where correlation in the received signal is the key to differentiability between the \(\mathcal {H}_{0}\) and the \(\mathcal {H}_{1}\) case, it does not embody the worst case. As will be shown in the subsequent sections, the assumption that the (Gaussian) noise samples are i.i.d. (and thus the noise is white) is a crucial prerequisite for the maximum-minimum-eigenvalue (MME) detector’s optimal operation. To take into consideration that different types of noise exist, we model η(n) as having any distribution W from a set of possible distributions \(\mathcal {W}\), all of which have the variance \(\sigma _{\eta }^{2}\). The maximum-minimum-eigenvalue (MME) detector is a general spectrum sensing algorithm in the sense that it is capable of detecting different kinds of signals. Thus, we do not assume a fixed signal type but instead only make the assumption that the primary user (PU) signal s(n) has any distribution S from the set of possible distributions \(\mathcal {S}\), all of which have the variance \(\sigma _{s}^{2}\).

Given the sets \(\mathcal {S}\) and \(\mathcal {W}\) with the variances \(\sigma _{s}^{2}\) and \(\sigma _{\eta }^{2}\) respectively, we can now define the signal-to-noise ratio (SNR) as
$$ \text{SNR} = \frac{\sigma_{s}^{2}}{\sigma_{\eta}^{2}}. $$
(8)
Further, we define the probability of false alarm and the probability of missed detection as
$$ \begin{aligned} P_{\text{fa}}(W, N) &= P\left(\Gamma_{\text{MME}}(\mathbf{x}, N) \ge \gamma\;|\;\mathcal{H}_{0}, W\right),\\ P_{\text{md}}(W, S, N) & = P(\Gamma_{\text{MME}}(\mathbf{x}, N) < \gamma\;|\;\mathcal{H}_{1}, W, S), \end{aligned} $$
(9)
respectively. In conformity with the definition in [9] (except that we do not consider a fading channel), we let a detector robustly achieve a pair (P fa,P md) consisting of a target false alarm probability P fa and a target missed detection probability P md if it satisfies
$$ \begin{aligned} \underset{W \in \mathcal{W}}{\text{sup}} P_{\text{fa}}(W,N) &\le P_{\text{fa}},\\ \underset{W \in \mathcal{W}, S \in \mathcal{S}}{\text{sup}} P_{\text{md}}(W,S,N) &\le P_{\text{md}}. \end{aligned} $$
(10)
The detector is called non-robust at a given SNR if at that SNR even with an arbitrarily high N, it cannot achieve any pair (P fa,P md) on the support P fa[0,0.5],P md[0,0.5]. The SNR wall is finally defined as
$${} \begin{aligned} \text{SNR}_{\text{wall}} = \text{sup}\{\text{SNR}_{t}, \;\text{s.t. the detector is non-robust}\\ \text{for all SNR} < \text{SNR}_{t}\}. \end{aligned} $$
(11)
For test statistics with symmetric probability density functions (PDFs), a definition of non-robustness equivalent to the above is that a detector is non-robust if the sets of means of the test statistic Γ(x,N) under the two hypotheses overlap [9]. This equivalence can be easily illustrated using Fig. 1. As can be seen, changing the threshold leads to a different pair (P fa,P md). The set of achievable pairs (P fa,P md) depends on the shape and the location of the test statistic probability density functions (PDFs). For symmetric probability density functions (PDFs), e.g., the ones illustrated in Fig. 1, achieving a pair (P fa,P md) on the support P fa[0,0.5],P md[0,0.5], i.e., being robust, means that the threshold cannot be above the mean of the \(\mathcal {H}_{1}\) PDF because this would result in a P md>0.5. Analogously, the threshold cannot be below the mean of the \(\mathcal {H}_{0}\) PDF because then P fa>0.5. Thus, if the sets of means overlap, i.e., if there is a \(\mathcal {H}_{1}\) mean that is below one of the \(\mathcal {H}_{0}\) means, no matter what value is chosen for the threshold, either P md or P fa is always >0.5 such that the detector is non-robust.
Figure 1
Fig. 1

Test statistic PDFs and error probabilities

Since the \(\mathcal {H}_{0}\) and \(\mathcal {H}_{1}\) test statistic probability density functions (PDFs) of the maximum-minimum-eigenvalue (MME) detector are not symmetric, we use a third definition of non-robustness, which states that a detector is non-robust if the sets of medians of the test statistic Γ(x,N) under the two hypotheses overlap. This definition is equivalent to the first one, even for non-symmetric distributions. For symmetric distributions, it coincides with the second definition. The reason we need to use the median instead of the mean is that for non-symmetric distributions, it does not hold that the probability above the mean as well as the probability below the mean is 0.5, while the same does by definition hold for the median.

We make use of the third version of the definition of an signal-to-noise ratio (SNR) wall when deriving a lower bound on the SNR wall for the maximum-minimum-eigenvalue (MME) detector, thus proving the existence of an SNR wall for that detector, in Section 5.

4 Sources of noise and noise coloring

As mentioned in Section 3, additive white Gaussian noise (AWGN) can only be considered an approximation of the actual noise experienced at a radio receiver. In this section, we make the case for considering colored receiver noise, which is an assumption used in the subsequent sections to prove the existence of an SNR wall for the maximum-minimum-eigenvalue (MME) detector.

In [11], it is assumed that the receiver noise before processing is white and that the only source of noise coloring is the use of a receive filter. The receive filter is assumed to be known in advance and to be invertible, such that a pre-whitening filter can be used to re-whiten the received samples before including them in the computation of the test statistic. On close inspection, it seems to be problematic to remove all coloring, since perfect filter design is hardly achievable, which makes employing an exact inverse of the receive filter seem impossible.

Even if the coloring caused by the receiver architecture was perfectly reversible, the assumption that the external noise is white represents an oversimplification, which in the case of the maximum-minimum-eigenvalue (MME) detector happens to be inappropriate, since for this detector uncorrelated noise is a requirement for proper functioning. In reality, the external noise is a superposition of different kinds of noise from various sources and although the impact of external noise decreases for higher frequencies [14], at moderate frequencies such as the ones used for television broadcasting, external noise is present and should be considered. Note that the television bands are of utmost interest for spectrum sensing, i.e., many spectrum sensing algorithms originated in the context of the IEEE 802.22 standard [2], which is concerned with communication in vacant television bands.

There are multiple different sources of realistic non-white external noise. One example is galactic radiation noise. The power spectral density (PSD) of such noise is proportional to \(\frac 1 {f^{2.7}}\) [15], where f denotes the frequency, which makes it non-white. Another example is man-made noise [16]. The reason this kind of noise leads to correlation in the received samples under \(\mathcal {H}_{0}\) is twofold. Firstly, it occurs in strong bursts that affect multiple receiver samples, which leads to time correlation. Secondly, when multiple receivers or multiple receive antennas are considered, the received noise is correlated in the case that multiple of them are in the range of the same man-made impulsive noise. The origin of man-made noise lies in, e.g., unintended radiation from electrical machinery or power transmission lines. Furthermore, nearly every electronic device creates it and thus, impulsive man-made noise is an effect that needs to be taken into account.

As pointed out above, expecting receiver noise to be white and uncorrelated is unrealistic due to imperfect filters, galactic radiation noise, and different sources of man-made noise. Thus, in the remainder, we investigate what effect non-white noise has on the performance of the maximum-minimum-eigenvalue (MME) detector.

5 SNR wall lower bound

In this section, we derive a lower bound on the SNR wall of the maximum-minimum-eigenvalue (MME) detector, thus proving its existence. More specifically, following the definition of the SNR wall from Section 3, we derive a lower bound on the SNR value below which the sets of medians of the test statistic Γ(x,N) under the two hypotheses (\(\mathcal {H}_{0}\) and \(\mathcal {H}_{1}\)) overlap even in the asymptotic case (\(N \rightarrow \infty \)). To determine the location of the overlap, we provide a lower bound on the test statistic under \(\mathcal {H}_{0}\) and an upper bound on the test statistic under \(\mathcal {H}_{1}\). The SNR below which the first of these two bounds has a higher value than the second one is the lower bound on the SNR wall. Due to the fact that for \(N \rightarrow \infty \), the probability density functions (PDFs) of the test statistic under the two hypotheses both become degenerate distributions, such that the probability density functions (PDFs) coincide with their medians, this is equivalent to the above definition of the SNR wall.

In our system model, the matrices R s and R η are no Toeplitz matrices. The reason can be found in the composition of the vector x(n), i.e., the covariance matrices contain two types of correlation, time, and receiver correlation (cf. (2)). Note, that this is the case despite the facts that firstly, due to our asymptotic approach, the matrices are statistical covariance matrices and secondly, the underlying noise processes are assumed to be stationary. The correlation coefficients associated with the entry in the i-th row and j-th column of R s and R η are denoted by \(\rho ^{s}_{ij}\) and \(\rho ^{\eta }_{ij}\), respectively. Bounds will be denoted by a bar above the respective symbol.

5.1 Lower bound on the test statistic under \(\mathcal {H}_{0}\)

In the \(\mathcal {H}_{0}\) case, R x =R η , since no primary user (PU) signal exists. For this case, we aim at finding a lower bound \(\bar \Gamma ^{\text {asym, lo}}_{\text {MME}, \mathcal {H}_{0}}\) on the asymptotic test statistic, i.e.,
$$\begin{array}{*{20}l} \frac{\bar \lambda_{\text{max}}^{\text{lo}}\left(\mathbf{R}_{\boldsymbol{\eta}}\right)}{\bar \lambda_{\text{min}}^{\text{up}}\left(\mathbf{R}_{\boldsymbol{\eta}}\right)} = \bar \Gamma^{\text{asym, lo}}_{\text{MME}, \mathcal{H}_{0}} \le \Gamma^{\text{asym}}_{\text{MME}, \mathcal{H}_{0}} = \frac{\lambda_{\text{max}}\left(\mathbf{R}_{\boldsymbol{\eta}}\right)}{\lambda_{\text{min}}\left(\mathbf{R}_{\boldsymbol{\eta}}\right)}. \end{array} $$
(12)
To obtain the lower bound \(\bar \Gamma ^{\text {asym, lo}}_{\text {MME}, \mathcal {H}_{0}}\), we need to determine a lower bound on the largest eigenvalue (\(\bar \lambda _{\text {max}}^{\text {lo}}(\mathbf {R}_{\boldsymbol {\eta }})\)) and an upper bound on the smallest eigenvalue \(\left (\bar \lambda _{\text {min}}^{\text {up}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right)\right)\), i.e.,
$$ \begin{aligned} \bar \lambda_{\text{max}}^{\text{lo}}\left(\mathbf{R}_{\boldsymbol{\eta}}\right) &\le \lambda_{\text{max}}\left(\mathbf{R}_{\boldsymbol{\eta}}\right),\\ \bar \lambda_{\text{min}}^{\text{up}}\left(\mathbf{R}_{\boldsymbol{\eta}}\right) &\ge \lambda_{\text{min}}\left(\mathbf{R}_{\boldsymbol{\eta}}\right). \end{aligned} $$
(13)
According to the Courant-Fischer theorem, the maximum and minimum eigenvalues λ max(H) and λ min(H) of a Hermitian matrix H can be obtained by solving the following optimization problems [17]
$$ \begin{aligned} \lambda_{\text{max}}(\mathbf{H}) &= \underset{\mathbf{z} : \mathbf{z}^{\mathrm{H}} \mathbf{z} = 1}{\text{max}} \mathbf{z}^{\mathrm{H}} \mathbf{H} \mathbf{z},\\ \lambda_{\text{min}}(\mathbf{H}) &= \underset{\mathbf{z} : \mathbf{z}^{\mathrm{H}} \mathbf{z} = 1}{\text{min}} \mathbf{z}^{\mathrm{H}} \mathbf{H} \mathbf{z}. \end{aligned} $$
(14)
From (14), it directly follows that
$$ \lambda_{\text{min}}(\mathbf{H}) \le \mathbf{z}^{\mathrm{H}} \mathbf{H} \mathbf{z} \le \lambda_{\text{max}}(\mathbf{H}), $$
(15)

for an arbitrary normalized z. This means that we can obtain the bounds \(\bar \lambda _{\text {max}}^{\text {lo}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right)\) and \(\bar \lambda _{\text {min}}^{\text {up}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right)\) by simply evaluating \(\bar \lambda _{\text {max}}^{\text {lo}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right) = \mathbf {z}_{1}^{\mathrm {H}} \mathbf {R}_{\boldsymbol {\eta }}\mathbf {z}_{1}\) and \(\bar \lambda _{\text {min}}^{\text {up}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right) = \mathbf {z}_{2}^{\mathrm {H}} \mathbf {R}_{\boldsymbol {\eta }}\mathbf {z}_{2}\) using two arbitrary normalized vectors z 1 and z 2. However, an additional constraint we need to take care of when obtaining the bounds is that \(\bar \lambda _{\text {max}}^{\text {lo}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right) \ge \bar \lambda _{\text {min}}^{\text {up}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right)\) needs to hold. In the following, we construct a set of vectors z 1 and z 2 that guarantees that this property is satisfied.

Given a specific covariance matrix R η , the vectors are constructed as to extract its largest correlation coefficient \(\rho ^{\eta }_{\text {max}}\) with \(\left |\rho ^{\eta }_{\text {max}}\right | \ge \left |\rho ^{\eta }_{ij}\right |\,\forall \,i,j\) with ij. For the below example, we assume that the largest correlation coefficient is located at the k-th column of the first row of the matrix. Given the Hermitian structure of covariance matrices and the assumed stationarity of the noise processes, this assumption can be made without loss of generality. The considered covariance matrix has the following structure
$$ \mathbf{R}_{\boldsymbol{\eta}} = \sigma_{\eta}^{2} \left(\begin{array}{cccc} 1 &\cdots & |\rho_{\text{max}}^{\eta}|e^{j\phi} & \cdots \\ \vdots &\ddots & \cdots & \cdots \\ \ |\rho_{\text{max}}^{\eta}|e^{-j\phi} & \cdots & 1 & \cdots \\ \vdots &\vdots & \vdots & \ddots \\ \end{array}\right). $$
(16)
The accompanying vectors z 1 and z 2 are given by
$$ \begin{aligned} \mathbf{z}_{1}&=\frac{1}{\sqrt{2}}\left[1,0,\dots,0,+e^{-j\phi},0,\dots,0\right]^{\mathrm{T}},\\ \mathbf{z}_{2}&=\frac{1}{\sqrt{2}}\left[1,0,\dots,0,-e^{-j\phi},0,\dots,0\right]^{\mathrm{T}}, \end{aligned} $$
(17)
where ±e j ϕ is the k-th element of the respective vector, coinciding with the position of \(\left |\rho _{\text {max}}^{\eta }\right |e^{\pm j\phi }\) in R η . We can now obtain
$$ \begin{aligned} \bar \lambda_{\text{max}}^{\text{lo}}\left(\mathbf{R}_{\boldsymbol{\eta}}\right) = \mathbf{z}_{1}^{\mathrm{H}} \mathbf{R}_{\boldsymbol{\eta}} \mathbf{z}_{1} &= \sigma_{\eta}^{2}\left(1+ \left|\rho_{\text{max}}^{\eta}\right|\right),\\ \bar \lambda_{\text{min}}^{\text{up}}\left(\mathbf{R}_{\boldsymbol{\eta}}\right) = \mathbf{z}_{2}^{\mathrm{H}} \mathbf{R}_{\boldsymbol{\eta}} \mathbf{z}_{2} &= \sigma_{\eta}^{2}\left(1- \left|\rho_{\text{max}}^{\eta}\right|\right). \end{aligned} $$
(18)
Note that the above argument can be made for an arbitrary position of \(\rho _{\text {max}}^{\eta }\) by choosing z 1 and z 2 accordingly, leaving (18) unchanged. Note also that \(\bar \lambda _{\text {max}}^{\text {lo}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right) \ge \bar \lambda _{\text {min}}^{\text {up}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right)\) holds. The lower bound on the test statistic under \(\mathcal {H}_{0}\) is now given by
$$ \bar \Gamma^{\text{asym, lo}}_{\text{MME}, \mathcal{H}_{0}} = \frac{1+ \left|\rho_{\text{max}}^{\eta}\right|}{1- \left|\rho_{\text{max}}^{\eta}\right|}, $$
(19)

for \(0 \le \left |\rho _{\text {max}}^{\eta }\right | < 1\). For the case of complete noise correlation, i.e., \(\left |\rho _{\text {max}}^{\eta }\right | = 1\) we get \(0 \le \lambda _{\text {min}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right) \le \bar \lambda _{\text {min}}^{\text {up}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right) = 0\), where the first inequality is due to the general positive semidefiniteness of covariance matrices. Since for \(\lambda _{\text {min}}\left (\mathbf {R}_{\boldsymbol {\eta }}\right) = 0\) detection becomes impossible (cf. (7)), we exclude the case of complete noise correlation.

5.2 Upper bound on the test statistic under \(\mathcal {H}_{1}\)

In the \(\mathcal {H}_{1}\) case, R x =R s +R η . For this case, we aim at finding an upper bound \(\bar \Gamma ^{\text {asym, up}}_{\text {MME}, \mathcal {H}_{1}}\) on the asymptotic test statistic, i.e.,
$$\begin{array}{*{20}l} \frac{\bar \lambda_{\text{max}}^{\text{up}}\left(\mathbf{R}_{\mathbf{x}}\right)}{\bar \lambda_{\text{min}}^{\text{lo}}(\mathbf{R}_{\mathbf{x}})} = \bar \Gamma^{\text{asym, up}}_{\text{MME}, \mathcal{H}_{1}} \ge \Gamma^{\text{asym}}_{\text{MME}, \mathcal{H}_{1}} = \frac{\lambda_{\text{max}}(\mathbf{R}_{\mathbf{x}})}{\lambda_{\text{min}}(\mathbf{R}_{\mathbf{x}})}. \end{array} $$
(20)
To obtain the upper bound \(\bar \Gamma ^{\text {asym, up}}_{\text {MME}, \mathcal {H}_{1}}\), we need to determine an upper bound on the largest eigenvalue \(\left (\bar \lambda _{\text {max}}^{\text {up}}\left (\mathbf {R}_{\mathbf {x}}\right)\right)\) and a lower bound on the smallest eigenvalue \(\left (\bar \lambda _{\text {min}}^{\text {lo}}\left (\mathbf {R}_{\mathbf {x}}\right)\right)\), i.e.,
$$ \begin{aligned} \bar \lambda_{\text{max}}^{\text{up}}(\mathbf{R}_{\mathbf{x}}) &\ge \lambda_{\text{max}}(\mathbf{R}_{\mathbf{x}}),\\ \bar \lambda_{\text{min}}^{\text{lo}}(\mathbf{R}_{\mathbf{x}}) &\le \lambda_{\text{min}}(\mathrm{R}_{\mathbf{x}}). \end{aligned} $$
(21)
Let r ij denote the entry of R x in the i-th row and j-th column. Given our assumptions from Section 2, we get
$$ \begin{aligned} r_{ii}&=\sigma_{\eta}^{2}+\sigma_{s}^{2}=(1+\text{SNR})\sigma_{\eta}^{2},\\ r_{ij}&=\sigma_{\eta}^{2} \rho_{ij}^{\eta} +\sigma_{s}^{2} \rho_{ij}^{s}=\left(\rho_{ij}^{\eta}+\text{SNR} \rho_{ij}^{s}\right)\sigma_{\eta}^{2}. \end{aligned} $$
(22)
According to the Gershgorin circle theorem [18], all eigenvalues \(\lambda _{k}|_{k=1}^{g}\) of a matrix \( \mathbf {A} \in \mathbb {C}^{g\times g}\), with g=p(Q+1), lie within the union of the circular disks
$$ \left\{z \in \mathbb{C}: \left|z-a_{ii}\right|\le R_{i}\right\}, $$
(23)
where
$$ R_{i}=\sum_{\substack{j=1\\j\neq i}}^{g}{\left|a_{ij}\right|}. $$
(24)
Since R x is Hermitian, all of its eigenvalues are real and thus the disks from (23) become intervals on the real axis. The value of r ii is independent of i. Thus, an upper bound on the maximum eigenvalue of R x can be obtained as
$${} \begin{aligned} \bar \lambda_{\text{max}}^{\text{up}}(\mathrm{R}_{\mathbf{x}}) &= \left|r_{ii}\right| + \underset{i}{\text{max}}\; R_{i}\\ &=\sigma_{\eta}^{2}\left(\text{SNR}+1+\underset{i}{\text{max}} \sum_{\substack{j=1\\ j\neq i}}^{g}\left|\left(\rho_{ij}^{\eta}+\text{SNR} \rho_{ij}^{s}\right)\right|\right)\\&\geq \lambda_{\text{max}}(\mathrm{R}_{\mathbf{x}}). \end{aligned} $$
(25)
In analogy to (25), a lower bound on the minimum eigenvalue of R x can be obtained as
$${} \begin{aligned} \bar \lambda_{\text{min}}^{\text{lo}}(\mathrm{R}_{\mathbf{x}}) &= \left|r_{ii}\right| - \underset{i}{\text{max}}\; R_{i}\\ &=\sigma_{\eta}^{2}\left(\text{SNR}+1-\underset{i}{\text{max}} \sum_{\substack{j=1\\j\neq i}}^{g} \left|\left(\rho_{ij}^{\eta}+\text{SNR} \rho_{ij}^{s}\right)\right|\right)\\&\le \lambda_{\text{min}}(\mathrm{R}_{\mathbf{x}}). \end{aligned} $$
(26)
However, for (26) to be a valid bound in terms of the test statistic, we need to introduce an extra constraint. We need to make sure that \(\bar \lambda _{\text {min}}^{\text {lo}}(\mathrm {R}_{\mathbf {x}}) > 0\), i.e., \(\left |r_{ii}\right |-\underset {i}{\text {max}}~R_{i}>0\), which leads to the constraint
$$\begin{array}{*{20}l} 1+\text{SNR}>\underset{i}{\text{max}}\sum_{\substack{j=1\\j\neq i}}^{g} \left|\left(\rho_{ij}^{\eta}+\text{SNR} \rho_{ij}^{s}\right)\right|. \end{array} $$
(27)
Combining (25) and (26) finally provides the upper bound on the asymptotic test statistic under \(\mathcal {H}_{1}\) given by
$$\begin{array}{*{20}l} \bar{\Gamma}_{\text{MME},\mathcal{H}_{1}}^{\text{asym, up}}=\frac{\text{SNR}+1+\underset{i}{\text{max}} \sum\limits_{\substack{j=1\\j\neq i}}^{g} \left|\left(\rho_{ij}^{\eta}+\text{SNR} \rho_{ij}^{s}\right)\right|}{\text{SNR}+1-\underset{i}{\text{max}} \sum\limits_{\substack{j=1\\j\neq i}}^{g}\left|\left(\rho_{ij}^{\eta}+\text{SNR} \rho_{ij}^{s}\right)\right|}. \end{array} $$
(28)

5.3 Lower bound on the SNR wall

Combining (19) and (28), we can say that the maximum-minimum-eigenvalue (MME) detector is non-robust under the condition given by (27) and given that \(\rho ^{\eta }_{\text {max}} <1\) when \(\bar {\Gamma }_{\text {MME},\mathcal {H}_{1}}^{\text {asym, up}} \le \bar \Gamma ^{\text {asym, lo}}_{\text {MME}, \mathcal {H}_{0}}\), i.e.,
$$\begin{array}{*{20}l} \frac{\text{SNR}+1+\underset{i}{\text{max}} \sum\limits_{\substack{j=1\\j\neq i}}^{g}\left|\left(\rho_{ij}^{\eta}+\text{SNR} \rho_{ij}^{s}\right)\right|}{\text{SNR}+1-\underset{i}{\text{max}} \sum\limits_{\substack{j=1\\j\neq i}}^{g}\left|\left(\rho_{ij}^{\eta}+\text{\text{SNR}} \rho_{ij}^{s}\right)\right|} \le \frac{1+\left|\varrho_{\text{max}}^{\eta}\right|}{1-\left|\varrho_{\text{max}}^{\eta}\right|}. \end{array} $$
(29)

Note that the correlation coefficients in the \(\mathcal {H}_{0}\) case are now denoted by ϱ instead of ρ to facilitate the distinction between the noise correlation in the \(\mathcal {H}_{0}\) and the \(\mathcal {H}_{1}\) case. For the interpretation of (29), it is important to note that \(\rho _{ij}^{s} \ge 0 \;\forall \; i,j\), i.e., the signal correlation coefficients never become negative. This follows from (2), (4), and the assumption that consecutive symbols are independent.

6 Examples of the lower bound on the SNR wall

Inequality (29) is quite involved and does not allow for easy interpretation. Since our goal is to prove the existence of an signal-to-noise ratio (SNR) wall, we continue our investigation with examples that simplify (29), facilitating interpretation. We consider the case, where under \(\mathcal {H}_{1}\) no noise correlation exists, i.e., \(\rho _{ij}^{\eta } = 0\;\forall \;i,j\) except i=j, while under \(\mathcal {H}_{0}\), the noise is correlated, i.e., (i,j) with ij for which \(\varrho _{ij}^{\eta } \ne 0\). This case occurs when the sources of noise coloring in the vicinity of the sensor are only present at certain times or if the sensor is used at different locations. Considering uncorrelated noise under \(\mathcal {H}_{1}\), (27) can be simplified as follows
$$ \begin{aligned} &1+\text{SNR}>\underset{i}{\text{max}}\sum_{\substack{j=1\\j\neq i}}^{g} \left|\left(\rho_{ij}^{\eta}+\text{SNR} \rho_{ij}^{s}\right)\right|\\ \Leftrightarrow &1+\text{SNR}>\text{SNR}\cdot \underset{i}{\text{max}}\sum_{\substack{j=1\\j\neq i}}^{g} \left|\rho_{ij}^{s}\right|\\ \Leftrightarrow &\text{SNR}<\frac{1}{\kappa_{\text{max}}-1}, \end{aligned} $$
(30)
where
$$ \kappa_{\text{max}}=\underset{i}{\text{max}}\sum_{\substack{j=1\\j\neq i}}^{g}\left|\rho_{ij}^{s}\right|. $$
(31)
This means that the higher the correlation in the signal samples, the lower the signal-to-noise ratio (SNR) for which our lower bound is defined. For κ max<1, the condition is never satisfied. In this case, we have to fall back to zero as a lower bound for λ min, which is guaranteed by the properties of covariance matrices. This however leads to the test statistic under \(\mathcal {H}_{0}\) taking the value infinity, which again rules out the possibility of giving a lower bound for an signal-to-noise ratio (SNR) wall. For a more concise notation, let
$$ \alpha_{\text{max}} = \bar \Gamma^{\text{asym, lo}}_{\text{MME}, \mathcal{H}_{0}} = \frac{1+\left|\varrho_{\text{max}}^{\eta}\right|}{1-\left|\varrho_{\text{max}}^{\eta}\right|}. $$
(32)
By assuming a minimal amount of noise coloring under \(\mathcal {H}_{0}\) and excluding the case of complete noise correlation, we restricted the support of the largest noise correlation coefficient, such that ϱ max(0,1). As a consequence, it holds that α max>1. Using the definitions of κ max and α max, as well as the assumption that under \(\mathcal {H}_{1}\) the noise is uncorrelated, (29) becomes
$$\begin{array}{*{20}l} \frac{\text{SNR}+1+\kappa_{\text{max}}\text{SNR}}{\text{SNR}+1-\kappa_{\text{max}}\text{SNR}}\le \alpha_{\text{max}}, \end{array} $$
(33)
or equivalently
$$\begin{array}{*{20}l} \text{SNR} \le \frac{\alpha_{\text{max}}-1}{1+\kappa_{\text{max}}+\alpha_{\text{max}}\left(\kappa_{\text{max}}-1\right)}. \end{array} $$
(34)

In order to obtain concrete numbers for the bound, we will look at more specific examples in the following.

6.1 Receiver correlation (Q=0, p≥2)

In this example, we consider a p-receiver setup with perfect signal correlation, i.e., \(\rho _{ij}^{s} = 1\;\forall \;i, j\). The maximum signal correlation in this case is κ max=p−1 and thus the condition (30) becomes \(\text {SNR} < \frac 1 {p-2}\). If the condition is satisfied, we can say that the maximum-minimum-eigenvalue (MME) detector becomes non-robust for
$$ \text{SNR} \le \frac{\alpha_{\text{max}}-1}{p+\alpha_{\text{max}}(p-2)}. $$
(35)
For p=2 and a maximum noise correlation of \(\varrho _{\text {max}}^{\eta } = 0.05\), which we consider to be moderate noise coloring, we arrive at a lower bound of SNR=0.052632=−12.788 dB, which is considerably far away from −22 dB (cf. Section 1). This example is simple enough for us to obtain the actual statistical covariance matrices for an evaluation of the bound’s tightness. They are given by
$$ \begin{aligned} \mathbf{R}_{\mathbf{x}}^{\mathcal{H}_{0}}&=\mathbf{R}_{\boldsymbol{\eta}}^{\mathcal{H}_{0}}=\sigma_{\eta}^{2} \left(\begin{array}{cc} 1 &0.05\\ 0.05 &1 \end{array}\right), \\ \mathbf{R}_{\mathbf{x}}^{\mathcal{H}_{1}}&= \left(\begin{array}{cc} \sigma_{\eta}^{2}+\sigma_{s}^{2} &\sigma_{s}^{2}\\ \sigma_{s}^{2} &\sigma_{\eta}^{2}+\sigma_{s}^{2} \end{array}\right) \\ &=\sigma_{\eta}^{2} \left(\begin{array}{cc} 1+\text{SNR} &\text{SNR}\\ \text{SNR} &1+\text{SNR} \end{array}\right). \end{aligned} $$
(36)

With the above covariance matrices, the asymptotic test statistics evaluate to \(\Gamma _{\mathcal {H}_{0}}^{\text {asym}}=1.10503\) and \(\Gamma _{\mathcal {H}_{1}}^{\text {asym}}=1+2\text {SNR}\). This means that for an signal-to-noise ratio (SNR) below 0.052632=−12.788 dB, \(\Gamma _{\mathcal {H}_{1}}^{\text {asym}} < \Gamma _{\mathcal {H}_{0}}^{\text {asym}}\), such that the detector becomes non-robust, i.e., in this special case the bound is tight.

6.2 Time correlation (p=1, Q≥1)

To complement the receiver correlation example, we next investigate a case with only one receiver that examines the correlation of the received samples over time. In order to again obtain a bound via (34), the value of κ max needs to be determined. Given an oversampling factor M and the independence of consecutive symbols, the autocorrelation function of the primary user (PU) signal can be obtained as
$$ \mathbb{E}\left[{s^{*}(n)s(n\pm k)}\right]=\begin{cases} \sigma_{s}^{2}\left(1-\frac{k}{M}\right) &\text{if}~ |k|<M \\ 0 & \text{else.}\end{cases} $$
(37)
In our case, the row with the maximum off-diagonal correlation sum in R s is the \(\left \lfloor \frac {g + 1} 2 \right \rfloor \)-th one, where g=Q+1 is the number of rows of R s and · denotes the floor operation. This is illustrated in the following example for Q=3 (assuming M≥3)
$$\begin{array}{*{20}l} \mathbf{R}_{\mathbf{s}}= \sigma_{s}^{2} \left(\begin{array}{cccc} 1 &1-\frac{1}{M} &1-\frac{2}{M} &1-\frac{3}{M}\\ 1-\frac{1}{M} &1 &1-\frac{1}{M} &1-\frac{2}{M}\\ 1-\frac{2}{M} &1-\frac{1}{M} &1 &1-\frac{1}{M}\\ 1-\frac{3}{M} &1-\frac{2}{M} &1-\frac{1}{M} &1 \end{array}\right). \end{array} $$
(38)

The further away from the diagonal, the smaller the value. Thus, the middle row has the highest sum.

In order to obtain κ max, three cases have to be distinguished. For \(\left \lceil \frac Q 2\right \rceil < M\) and Q even, we get
$$ \begin{aligned} \kappa_{\text{max}} &=2\sum_{j=1}^{\frac{Q}{2}}{\left(1-\frac j M\right)}\\ &=Q-\frac{Q^{2} + 2Q}{4M}, \end{aligned} $$
(39)
for \(\left \lceil \frac Q 2\right \rceil < M\) and Q odd, we get
$$ \begin{aligned} \kappa_{\text{max}}&=2 \sum_{j=1}^{\frac{Q-1}{2}}{\left(1-\frac j M\right)}+\left(1-\frac{Q+1}{2M}\right)\\ &=Q-\frac{(Q+1)^{2}}{4M}, \end{aligned} $$
(40)
and for \(\left \lceil \frac Q 2\right \rceil \ge M\), we get
$$ \kappa_{\text{max}}=2 \sum_{j=1}^{M-1}{\left(1-\frac j M\right)}=M-1, $$
(41)
where · denotes the ceiling operation. In this example, we model the noise as a stationary auto-regressive process of order one (AR(1)). It is supposed to mimic white external noise that has undergone filtering by a low-pass receive filter. The noise process is given by
$$ \eta(n) = 0.1 \eta(n - 1) + \epsilon(n), $$
(42)
where ε(n) denotes an i.i.d. complex Gaussian random process with mean zero and variance 0.99. It is independent of η(n−1) and has independent real and imaginary parts and \(\mathbb {E}\left [ {\left |\eta \left [n\right ]\right |^{2}}\right ]=1\). Figure 2 shows the noise process’s power spectral density (PSD) to illustrate its characteristics. We consider the case of Q=3 and M=4, where the choice of Q leads to the noise covariance matrix
$$ \mathbf{R}_{\boldsymbol{\eta}}= \left(\begin{array}{cccc} 1 &0.1 &0.1^{2} &0.1^{3}\\ 0.1 &1 &0.1 &0.1^{2}\\ 0.1^{2} &0.1 &1 &0.1\\ 0.1^{3} &0.1^{2} &0.1 &1 \end{array}\right) $$
(43)
Figure 2
Fig. 2

PSD of AR(1) process, which follows η[n]=0.1η[n−1]+ε[n]. The frequency is normalized to f samples=2π

and κ max=2 (cf. (40)). Using (34), we again get a lower bound for the signal-to-noise ratio (SNR)-wall of −12.788 dB.

6.3 Time and receiver correlation (p>1,Q>0)

As a final example, we consider the case where both, time and receiver correlation, are exploited. Given our model assumption that the signal strength is equal for all receivers, we can combine the κ max terms derived in the preceding subsections to obtain
$$ \kappa_{\text{max}}=p-1+p\cdot\kappa_{\text{max,time}}, $$
(44)

where κ max,time denotes the κ max term for time correlation.

7 Numerical evaluation

In this section, we provide numerical results corresponding to the examples given in Section 6.1 and Section 6.2. The parameters used in the simulations can be found in Table 1.
Table 1

System parameters

Parameter

Symbol

Value(s)

Modulation type

 

BPSK

Oversampling factor

M

4

Number of samples

N

{999,9999,999999}

No. of Monte Carlo instances

 

2000

No. of histogram bins

 

12

For the \(\mathcal {H}_{1}\) case, we generate white Gaussian noise and an oversampled binary phase shift keying (BPSK) signal with a rectangular pulse shape and symbols that are independent of each other. For the \(\mathcal {H}_{0}\) case, we generate colored noise. The different noise types used for \(\mathcal {H}_{0}\) and \(\mathcal {H}_{1}\) represent the model uncertainty that has to be taken into account when designing spectrum sensing algorithms. When generating colored noise, our aim is to create a stationary, sampled Gaussian process with a predefined covariance matrix.

7.1 Receiver correlation

In the receiver correlation case, we use a matrix multiplication approach for generating colored noise. We start by generating the p-dimensional white Gaussian noise sample vector \(\mathbf {w}(n) \sim \mathcal N\left (\boldsymbol {0}, \mathbf {R}_{\mathbf {w}}\right)\) for all time instances n, where R w =I p×p , while p is the number of receivers. That is, the vector w(n) is generated according to a p-dimensional zero-mean Gaussian distribution with the identity matrix as its covariance matrix. The colored noise vector η(n), which is experienced at the receiver in the \(\mathcal {H}_{0}\) case, is subsequently obtained as η(n)=A w(n), where the matrix \(\mathbf {A} \in \mathbb {C}^{p\times p}\) needs to be chosen such that the covariance matrix of η(n) equals the predefined R η . This approach leads to the desired result due to the fact that linear combinations of Gaussian random variables are again distributed according to a Gaussian distribution. It is well known that the covariance matrix of A w(n) is given by \(\mathbf {A} ^{\mathrm {H}} \mathbf {R}_{\mathbf {w}} \mathbf {A}\). Thus, the matrix A can be easily obtained by computing the Cholesky decomposition \(\mathbf {R}_{\boldsymbol {\eta }} = \mathbf {A}^{\mathrm {H}}\mathbf {A}\).

Figure 3 shows the histograms for the maximum-minimum-eigenvalue (MME) test statistic Γ MME in the \(\mathcal {H}_{0}\) case (black) and the \(\mathcal {H}_{1}\) case (colored). For the \(\mathcal {H}_{1}\) case, the test statistic histograms for different SNRs are shown. It can be observed that the estimation variance of the test statistic decreases with an increasing number of samples N, which is to be expected since asymptotically the sample covariance matrix converges to the statistical covariance matrix. What we can also see is that the mean of the estimated test statistic changes for an increasing N. This is a testimony to the biasedness of the estimator (7). Recall, that the lower bound on the signal-to-noise ratio (SNR) wall for this scenario has been derived to be −12.788 dB. The simulation results confirm this bound. Indeed, when the signal-to-noise ratio (SNR) drops below the derived bound, the medians of the test statistics under \(\mathcal {H}_{1}\) are below the median of the test statistic under \(\mathcal {H}_{0}\) for all inspected N, making the detector non-robust by definition.
Figure 3
Fig. 3

Estimated probability density function for receiver correlation (p=2, Q=0) and different N. Noise correlation factor \(\varrho _{\text {max}}^{\eta }=0.05\). Solid lines represent the histograms, while dashed lines depict the means. The \(\mathcal {H}_{0}\) case result is shown in black, while the \(\mathcal {H}_{1}\) case results are colored, where the SNR from right to left is given by {−10,−11,…,−15} dB

7.2 Time correlation

Since in the previous example, the noise correlation only exists between the noise processes of different receivers but not between noise samples taken at a single receiver at different times, the matrix A, which is used to color the noise, has a small dimension. This makes the matrix multiplication approach feasible for the receiver correlation example. To use the same method in the time correlation example, a coloring matrix of size N×N would be necessary, where in our simulations, N takes on values of up to 106. This renders the matrix multiplication approach infeasible for the current example. Thus, a different approach for generating colored noise has to be taken. First, we generate an autocorrelation with a real-valued power spectral density (PSD) from an autoregressive model of order one. We then generate an N-dimensional vector distributed according to a zero-mean, unit-variance, complex, white Gaussian distribution, which serves as a frequency-domain noise basis. Its power spectral density (PSD) is subsequently scaled by the power spectral density (PSD) of the autocorrelation, after which it is transformed to the time-domain via the inverse discrete Fourier transform (IDFT) and scaled to variance \(\sigma _{\eta }^{2}\). Here again, we use the fact that a linear combination of Gaussian random variables is also distributed according to a Gaussian distribution.

Recall that the lower bound on the signal-to-noise ratio (SNR) wall for this scenario has been derived to be −12.788 dB. According to the numerical results, in this scenario, the maximum-minimum-eigenvalue (MME) detector exhibits an signal-to-noise ratio (SNR) wall between −8 and −9 dB (Fig. 4). While the lower bound cannot be called very tight for this example, it nevertheless proves the existence of an signal-to-noise ratio (SNR) wall, which is guaranteed to be much higher than the desired −22 dB.
Figure 4
Fig. 4

Estimated probability density function for time correlation (p=1, Q=4) and different N. Solid lines represent the histograms, while dashed lines depict the means. The \(\mathcal {H}_{0}\) case result is shown in black, while the \(\mathcal {H}_{1}\) case results are colored, where the SNR from right to left is given by {−6,−7,…,−10} dB.

8 Conclusions

In this work, we have proven the existence of an signal-to-noise ratio (SNR) wall for the eigenvalue-based maximum-minimum-eigenvalue (MME) spectrum sensing algorithm. The signal-to-noise ratio (SNR) wall is caused by uncertainty about the coloring of the receiver noise. A lower bound on the signal-to-noise ratio (SNR) wall is derived and is complemented by time and receiver correlation examples. For the example, we give concrete signal-to-noise ratio (SNR) values, below which the maximum-minimum-eigenvalue (MME) detector is non-robust. Finally, numerical results supporting the analytical results are provided.

One possible direction for future work is the derivation of tighter bounds on the signal-to-noise ratio (SNR) wall. Also, it would be of great value if the results could be generalized to arbitrary eigenvalue-based spectrum sensing algorithms.

Declarations

Funding

This work was partly supported by the Deutsche Forschungsgemeinschaft (DFG) project CoCoSa (grant MA 1184/26-1).

Competing interests

The authors declare that they have no competing interests.

Publisher’s Note

Springer Nature remains neutral with regard to jurisdictional claims in published maps and institutional affiliations.

Open Access This article is distributed under the terms of the Creative Commons Attribution 4.0 International License (http://creativecommons.org/licenses/by/4.0/), which permits unrestricted use, distribution, and reproduction in any medium, provided you give appropriate credit to the original author(s) and the source, provide a link to the Creative Commons license, and indicate if changes were made.

Authors’ Affiliations

(1)
Institute for Theoretical Information Technology, RWTH Aachen University, Aachen, Germany

References

  1. Q Zhao, BM Sadler, A survey of dynamic spectrum access. IEEE Signal Proc. Mag.24(3), 79–89 (2007).View ArticleGoogle Scholar
  2. IEEE, IEEE Standard for Information Technlogy-Telecommunications and information exchange between systems; Wireless Regional Area Networks (WRAN)-Specific requirements Part 22: Cognitive Wireless RAN Medium Access Control (MAC) and Physical Layer (PHY) Specifications: Policies and Procedures for Operation in the TV Bands. IEEE Std 802.22-2011 (2011). https://www.ieee.org/documents/ieeecitationref.pdf.
  3. A Goldsmith, Wireless communications (Cambridge University Press, Cambridge, 2005).View ArticleGoogle Scholar
  4. E Axell, G Leus, EG Larsson, HV Poor, Spectrum sensing for cognitive radio: state-of-the-art and recent advances. IEEE Signal Proc. Mag. 29(3), 101–116 (2012).View ArticleGoogle Scholar
  5. T Yücek, H Arslan, A survey of spectrum sensing algorithms for cognitive radio applications. IEEE Commun. Surv. Tutorials. 11(1), 116–130 (2009).View ArticleGoogle Scholar
  6. Y Zeng, Y-C Liang, AT Hoang, R Zhang, A review on spectrum sensing for cognitive radio: challenges and solutions. EURASIP J. Adv. Signal Process. 2010: (2010). https://link.springer.com/article/10.1155/2010/381465.
  7. PJ Huber, Robust statistics (Springer, Berlin, 2011).View ArticleGoogle Scholar
  8. A Sonnenschein, PM Fishman, Radiometric detection of spread-spectrum signals in noise of uncertain power. IEEE Trans. Aerosp. Electron. Syst. 28(3), 654–660 (1992).View ArticleGoogle Scholar
  9. R Tandra, A Sahai, SNR walls for signal detection. IEEE J. Selected Topics Signal Process.2(1), 4–17 (2008).View ArticleGoogle Scholar
  10. R Tandra, A Sahai, in IEEE International Symposium on New Frontiers in Dynamic Spectrum Access Networks (DySPAN). SNR Walls for Feature Detectors, (2007), pp. 559–570.Google Scholar
  11. Y Zeng, Y-C Liang, Eigenvalue-based spectrum sensing algorithms for cognitive radio. IEEE Trans. Commun. 57(6), 1784–1793 (2009).View ArticleGoogle Scholar
  12. A Papoulis, SU Pillai, Probability, random variables, and stochastic processes, 4th edn (McGraw-Hill, New York City, 2002).Google Scholar
  13. I Shomorony, AS Avestimehr, Worst-Case Additive Noise in Wireless Networks. IEEE Trans. Inf. Theory. 59(6), 3833–3847 (2013).MathSciNetView ArticleMATHGoogle Scholar
  14. International Telecommunication Union, Recommendation P.372-12: Radio noise. Technical report (2015). https://www.itu.int/rec/R-REC-P.372/en. Accessed 23 Nov 2015.
  15. CD Motchenbacher, JA Connelly, Low noise electronic system design (Wiley, Hoboken, 1993).Google Scholar
  16. A Wagstaff, N Merricks, Man-made noise measurement programme (AY4119) - final Report. Technical Report Issue 2, Mass Consultants Limited (2003).Google Scholar
  17. RM Gray, Toeplitz and circulant matrices: a review (Now Publishers, Boston, Delft, 2006).MATHGoogle Scholar
  18. S Gerschgorin, Über die Abgrenzung der Eigenwerte einer Matrix. Bulletin de l’Académie des Sciences de l’URSS. 6:, 749–754 (1931).MATHGoogle Scholar

Copyright

© The Author(s) 2017

Advertisement