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Achievable Rate Analysis and Phase Shift Optimization on Intelligent Reflecting Surface with Hardware Impairments

Zhe Xing,  Rui Wang,  Jun Wu,  and Erwu Liu The authors are with the College of Electronics and Information Engineering, Tongji University, Shanghai 201804, China (e-mail: [email protected]; [email protected]; [email protected]; [email protected]).
Abstract

Intelligent reflecting surface (IRS) is envisioned as a promising hardware solution to hardware cost and energy consumption in the fifth-generation (5G) mobile communication network. It exhibits great advantages in enhancing data transmission, but may suffer from performance degradation caused by inherent hardware impairment (HWI). For analysing the achievable rate (ACR) and optimizing the phase shifts in the IRS-aided wireless communication system with HWI, we consider that the HWI appears at both the IRS and the signal transceivers. On this foundation, first, we derive the closed-form expression of the average ACR and the IRS utility. Then, we formulate optimization problems to optimize the IRS phase shifts by maximizing the signal-to-noise ratio (SNR) at the receiver side, and obtain the solution by transforming non-convex problems into semidefinite programming (SDP) problems. Subsequently, we compare the IRS with the conventional decode-and-forward (DF) relay in terms of the ACR and the utility. Finally, we carry out simulations to verify the theoretical analysis, and evaluate the impact of the channel estimation errors and residual phase noises on the optimization performance. Our results reveal that the HWI reduces the ACR and the IRS utility, and begets more serious performance degradation with more reflecting elements. Although the HWI has an impact on the IRS, it still leaves opportunities for the IRS to surpass the conventional DF relay, when the number of reflecting elements is large enough or the transmitting power is sufficiently high.

Index Terms:
Intelligent reflecting surface (IRS), hardware impairment (HWI), achievable rate (ACR), phase shift optimization, decode-and-forward (DF) relay.

I Introduction

The rapid development of the worldwide mobile communication technologies has been witnessed in recent years. After the 4th generation (4G) mobile communications became universal around the world, the initial 5th generation (5G) standard was completed in 2018 and the 5G commercial networks were already employed in part in the first quarter of 2020. For supporting huge mobile data traffic and high-speed communications required by a growing number of the mobile devices accessed to the wireless networks, a variety of innovative techniques including millimeter wave (mmWave), ultra-dense network (UDN) and massive multiple-input multiple-output (MIMO) are implemented in 5G wireless transmission systems [1]. These techniques exhibit great advantages in helping the communication systems improve spectral efficiency (SE) [2], but face challenging problems such as: 1) the mmWave is susceptible to blockage and suffers from severe power attenuation during the long-distance propagation in the atmosphere [3], so that the wireless communication system will bear poor reliability when the received signals are substantially weak; 2) the UDN is composed of numerous intensively distributed base stations (BS) [4] while the massive MIMO requests the signal transceivers to be equipped with large-scale antenna arrays [5], which lead to high hardware cost (HWC).

One mature technological solution to these problems is utilizing relays to establish a multi-hop transmission mode. Conventional wireless cooperative communication systems mostly employ relays [6, 7, 8, 9] to process on the signals received halfway and retransmit the signals to the destination terminals actively through an uncontrollable propagation environment. Relays are validated to be effective on improving system reliability [7], but are still active retransmitting facilities that require high energy consumption (EC) and HWC. Recently, another state of the art approach, which is named Intelligent Reflecting Surface (IRS) [10, 11], Large Intelligent Surface (LIS) [2] or Large Intelligent Metasurface (LIM) [12], has attracted considerable attention from wireless communication researchers. An IRS is a planar array composed of a large number of low-cost passive reconfigurable reflecting elements, each of which induces an adjustable phase shift on the coming signal wave and reflects the signal to the destination terminal [13, 15, 16, 14]. It is distinct from the ordinary physical reflecting surfaces which simply reflect the signal waves without any parameter adjustment, and also different from the traditional relays which actively retransmit the received signals. As a passive reflecting apparatus, the IRS is envisioned as a promising hardware solution to EC and HWC in the future communication networks.

There have already been studies that focused on the achievable rate (ACR) maximization, energy efficiency improvement, modulation scheme, secure communication realization, phase shift optimization, channel estimation and capacity analysis for the IRS-aided wireless communication systems [19, 20, 21, 2, 22, 23, 17, 18]. For instance, C. Huang, et al. [17, 18] employed the IRS to maximize the ACR [17] and the energy efficiency [18] of the wireless communication systems. E. Basar [19] proposed an IRS-based index modulation scheme which enabled high data rate and low bit-error-rate (BER). M. Cui, et al. [20] and H. Shen, et al. [21] developed IRS-aided secure wireless communication systems where the IRS was employed to maximize the rate gap (secrecy rate) between the desired transmission path from the source to the legitimate user and the undesired one from the source to the eavesdropper. W. Yan, et al. [2] developed a passive beamforming and information transferring method and optimized the phase shifts with different state values to improve the average signal-to-noise ratio (SNR). Q. Nadeem, et al. [22] outlined an IRS-aided multiple-user MIMO communication system and estimated the cascaded channel matrix within each time interval. E. Björnson, et al. [23] analysed and compared the channel capacities of the IRS-supported, the decode-and-forward (DF) relay assisted and the single-input-single-output (SISO) communication systems, and derived the least required number of the IRS reflecting elements which allowed the IRS to outperform the DF relay and SISO.

It is noted that the aforementioned works are carried out under the assumption of perfect hardware. However, in most practical situations, the inherent hardware impairment (HWI), e.g. phase noise, quantization error, amplifier non-linearity, et al., which will generally limit the system performance, cannot be neglected due to the non-ideality of the communication devices in the real world [24, 25, 8]. Although the effect of the HWI on the system performance can be mitigated by compensation algorithms [26], there will still exist residual HWI due to the imprecisely estimated time-variant hardware characteristic and the random noise. As a result, it is of great significance to probe into the system performance in the presence of HWI. Some researchers [27, 29, 28] analysed the channel capacity of the massive MIMO communication systems with HWI, which they modelled as additive Gaussian distributed distortion noise. But to the best of our knowledge, there were only a few studies that analysed the IRS-aided communication systems with the HWI at the IRS [31, 32, 33]. Among these studies, the researchers performed some important initial works by modelling the HWI at the IRS as an additive variable with respect to the distance between the reflecting point and the reflecting surface center [31], or as the uniformly distributed phase noise generated by the reflecting units [32, 33]. However, these works still left several research gaps to be filled. First, the HWI of the transmitting devices and receiving terminals was not simultaneously taken into consideration, which would jointly influence the performance of the IRS-aided communication systems as well. Second, the phase shift optimization was not implemented when there existed HWI, which was indispensable for one to acquire the optimal IRS configuration with hardware imperfections. Third, the performance comparisons between the IRS and the conventional approaches, e.g. DF relay, which also contributed to the wireless data transmission enhancement, needed to be further explored in the presence of HWI. Up to now, we have not found the related works that inquired into the above three aspects. Therefore, in this article, we will provide the ACR analysis and phase shift optimization on the IRS-aided communication system in consideration of the HWI at both the IRS and transceivers, and present performance comparisons with the existing multiple-antenna DF relay assisted communication system with the HWI at the DF relay and transceivers. Our contributions are summarized as follows.

  • By referring to [32], we model the HWI at the IRS as a phase error matrix, in which the random phase errors generated by the IRS reflecting units are uniformly distributed. By referring to [27, 30], we model the transceiver HWI as the additive distortion noise as well as the phase drift and the thermal noise. When the IRS phase shifts are adjusted to compensate for the phase shifts in the source-IRS channel and the IRS-destination channel, we mathematically derive the closed-form expression of the average ACR and the IRS utility with respect to the number of the reflecting elements, denoted by NN. From the theoretical and the numerical results, we confirm that the HWI decreases the average ACR and the IRS utility, and imposes more severe impact on the ACR performance as NN becomes larger.

  • In order to optimize the IRS phase shifts and obtain the maximum average ACR with HWI, we formulate the optimization problems and transform the non-convex problems into convex semidefinite programming (SDP) problems, then obtain the solution numerically by exploiting CVX toolbox with SDPT3 solver in the MATLAB simulation. Besides, we evaluate the impact of the channel estimation errors and the residual phase noises on the optimization performance, after which we conclude that both of the two unavoidable factors result in performance degradation to some extent.

  • When the HWI appears at the IRS, the DF relay and the transceivers, we compare the performance of the IRS with that of the multiple-antenna DF relay in terms of the ACR and the utility, and derive the condition where the IRS can always surpass the DF relay for all N>0N>0. The results illustrate that if NN is large enough or the transmitting power is sufficiently high, the IRS with NN passive reflecting elements is able to outperform the DF relay with the same number of antennas in the presence of HWI.

The rest of this article is organized as follows. In Section II, we introduce the IRS-aided wireless communication system with HWI by showing the system model. In Section III, we analyse the ACR and the IRS utility in the considered wireless communication system. In Section IV, we narrate the problem formulation and transformation when optimizing the IRS phase shifts in the presence of HWI. In Section V, we compare the performance of the IRS with that of the multiple-antenna DF relay in terms of the ACR and the utility. In Section VI, we provide numerical results to verify the theoretical analysis and present discussions on the channel estimation errors and the residual phase noises. In Section VII, we draw the overall conclusions.

Notations: Italics denote the variables or constants, while boldfaces denote the vectors or matrices. 𝐀\mathbf{A}^{*}, 𝐀T\mathbf{A}^{T}, 𝐀H\mathbf{A}^{H} and 𝐀1\mathbf{A}^{-1} symbolize the conjugate, transpose, conjugate-transpose and inverse of matrix 𝐀\mathbf{A}, respectively. tr(𝐀)tr(\mathbf{A}) and rank(𝐀)rank(\mathbf{A}) stand for the trace and the rank of 𝐀\mathbf{A}. diag(𝐚)diag(\mathbf{a}) represents an n×nn\times n sized diagonal matrix whose diagonal elements are (a1,a2,,an)(a_{1},a_{2},\ldots,a_{n}) in vector 𝐚\mathbf{a}. ||.||2||.||_{2} represents 2\ell_{2} norm. \odot symbolizes the Hadamard product. 𝐀m×n\mathbf{A}\in\mathbb{C}^{m\times n} or 𝐀m×n\mathbf{A}\in\mathbb{R}^{m\times n} means that 𝐀\mathbf{A} is an m×nm\times n sized complex or real-number matrix. 𝐀𝒞𝒩(𝟎,𝐕)\mathbf{A}\sim\mathcal{CN}(\mathbf{0},\mathbf{V}) or 𝐀𝒩(𝟎,𝐕)\mathbf{A}\sim\mathcal{N}(\mathbf{0},\mathbf{V}) illustrates that 𝐀\mathbf{A} obeys complex normal or normal distribution with mean of zero and covariance matrix of 𝐕\mathbf{V}. 𝐀𝟎\mathbf{A}\succeq\mathbf{0} means that 𝐀\mathbf{A} is positive semidefinite. 𝔼𝐱[𝐀]\mathbb{E}_{\mathbf{x}}[\mathbf{A}] denotes the expectation of 𝐀\mathbf{A} on the random variable 𝐱\mathbf{x} if 𝐀\mathbf{A} is a stochastic matrix in relation to 𝐱\mathbf{x}. 𝐈n\mathbf{I}_{n} and 𝚪n\mathbf{\Gamma}_{n} symbolize n×nn\times n sized identity matrix and n×nn\times n sized matrix with all elements of 1, respectively. 𝟏\mathbf{1} stands for the unit row vector with all elements of 1. Δ=b24ac\Delta=b^{2}-4ac represents the discriminant of the quadratic function f(x)=ax2+bx+cf\left(x\right)=ax^{2}+bx+c. g(x)=𝒪(f(x))g(x)=\mathcal{O}(f(x)) signifies that |g(x)/f(x)||g(x)/f(x)| is bounded when xx\rightarrow\infty. limxf(x)\lim_{x\to\infty}f(x) is represented by f(x)|xf(x)|_{x\rightarrow\infty} throughout the whole paper.

II Communication System Model

In this article, the considered wireless communication system (Figure 1) includes a signal-emitting source (e.g. the base station, BS), an IRS with NN passive reflecting elements, an IRS controller and a signal-receiving destination (e.g. the user equipment, UE). The signal-emitting source, assumed to be equipped with single antenna, transmits the modulated signals with an average signal power of P\sqrt{P}. The IRS induces reconfigurable phase shifts, which are adjusted by the IRS controller based on the channel state information (CSI), on the impinging signals, and reflects the coming signal waves to the destination. The signal-receiving destination, also equipped with single antenna, receives the directly arrived signals from the source and passively reflected signals from the IRS.

Refer to caption
Figure 1: The considered IRS-aided wireless communication system, including a single-antenna signal-emitting source, a single-antenna signal-receiving destination, an IRS with NN passive reflecting elements, and an IRS controller.

Generally, due to the non-ideality of the hardware, the received signal is disturbed by the HWI which universally exists in the real-world communication devices. In this considered system, the HWI appears at both the IRS and the signal transceivers. First, the HWI at the IRS is modelled as a random diagonal phase error matrix, which involves NN random phase errors induced by the intrinsic hardware imperfection of the passive reflectors, or by the imprecision of the channel estimation [32]. It is expressed as

𝚯E=diag(ejθE1,ejθE2,,ejθEN)\mathbf{\Theta}_{E}=diag\left(e^{j\theta_{E1}},e^{j\theta_{E2}},\ldots,e^{j\theta_{EN}}\right) (1)

where j2=1j^{2}=-1; θEi\theta_{Ei}, for i=1,2,,Ni=1,2,\ldots,N, are random phase errors uniformly distributed on [π/2,π/2]\left[-\pi/2,\pi/2\right]. Then, the HWIs at the signal transceivers primarily include the additive distortion noise, the multiplicative phase drift and the amplified thermal noise [28, 27, 30, 29], which create a mismatch between the intended signal and the practically generated signal, or create a distortion on the received signal during the reception processing. The distortion noises, generated by the transmitter and the receiver due to the insufficiency of the accurate modelling, the time-variant characteristics, et al., are modelled as ηt(t)𝒞𝒩(0,Υt)\eta_{t}(t)\sim\mathcal{CN}(0,\Upsilon_{t}) and ηr(t)𝒞𝒩(0,Vr)\eta_{r}(t)\sim\mathcal{CN}(0,V_{r}), respectively, where Υt\Upsilon_{t} and VrV_{r} will be given in (6) and (7). The multiplicative phase drift caused by the local oscillator at the receiver is modelled as ϕ(t)=ejψ(t)\phi(t)=e^{j\psi(t)}, with its expectation given by 𝔼[ϕ(t)]=e12δt\mathbb{E}[\phi(t)]=e^{-\frac{1}{2}\delta t} [29], where δ\delta denotes the oscillator quality, and ψ(t)\psi(t) follows a Wiener process:

ψ(t)𝒩(ψ(t1),δ)\psi(t)\sim\mathcal{N}(\psi(t-1),\delta) (2)

The amplified thermal noise, aroused by the mixers at the receiver and by the interference leakage from other frequency bands or wireless networks [30], is modelled as w(t)𝒞𝒩(0,σw2)w^{\prime}(t)\sim\mathcal{CN}(0,\sigma_{w^{\prime}}^{2}), with σw2\sigma_{w^{\prime}}^{2} being the thermal noise variance.

Therefore, referring to Eq. (2) in [27] and Eq. (3) in [30], the received signal disturbed by HWI is modelled as

y(t)=ϕ(t)(𝐡IUT𝚽𝚯E𝐡SI+hSU)[Ps(t)+ηt(t)]+ηr(t)+w(t)y(t)=\phi(t)\left(\mathbf{h}_{IU}^{T}\mathbf{\Phi}\mathbf{\Theta}_{E}\mathbf{h}_{SI}+h_{SU}\right)\left[\sqrt{P}s(t)+\eta_{t}(t)\right]+\eta_{r}(t)+w(t) (3)

where s(t)s(t) stands for the unit-power signal symbol at time tt with 𝔼[s(t)s(t)]=1\mathbb{E}\left[s(t)s^{*}(t)\right]=1; w(t)𝒞𝒩(0,σw2)w(t)\sim\mathcal{CN}\left(0,\sigma_{w}^{2}\right) denotes the receiver noise, whose variance σw2\sigma_{w}^{2}, according to [30], satisfies σw2=Fσw2\sigma_{w}^{2}=F\sigma_{w^{\prime}}^{2}, with F>1F>1 being the noise amplification factor; 𝚽=α×diag(ejθ1,ejθ2,,ejθN)\mathbf{\Phi}=\alpha\times diag\left(e^{j\theta_{1}},e^{j\theta_{2}},\ldots,e^{j\theta_{N}}\right) represents the phase shifting matrix of the IRS, where α(0,1]\alpha\in(0,1] is the fixed amplitude reflection coefficient and θi\theta_{i}, for i=1,2,,Ni=1,2,\ldots,N, are the adjustable phase-shift variables of the IRS; hSU=μSUejφSUh_{SU}=\sqrt{\mu_{SU}}e^{j\varphi_{SU}} represents the channel coefficient from the source to the destination, where μSU\sqrt{\mu_{SU}} and φSU\varphi_{SU} are the power attenuation coefficient and the phase shift of hSUh_{SU}; 𝐡IUN×1\mathbf{h}_{IU}\in\mathbb{C}^{N\times 1} and 𝐡SIN×1\mathbf{h}_{SI}\in\mathbb{C}^{N\times 1} are the channel coefficients from the IRS to the destination and from the source to the IRS, respectively, which are expressed as[23]

𝐡IU=μIU(ejφIU,1,ejφIU,2,,ejφIU,N)T\mathbf{h}_{IU}=\sqrt{\mu_{IU}}\left(e^{j\varphi_{IU,1}},e^{j\varphi_{IU,2}},\ldots,e^{j\varphi_{IU,N}}\right)^{T} (4)
𝐡SI=μSI(ejφSI,1,ejφSI,2,,ejφSI,N)T\mathbf{h}_{SI}=\sqrt{\mu_{SI}}\left(e^{j\varphi_{SI,1}},e^{j\varphi_{SI,2}},\ldots,e^{j\varphi_{SI,N}}\right)^{T} (5)

where μIU\sqrt{\mu_{IU}} and μSI\sqrt{\mu_{SI}} are the power attenuation coefficients of 𝐡IU\mathbf{h}_{IU} and 𝐡SI\mathbf{h}_{SI}; φIU,i\varphi_{IU,i} and φSI,i\varphi_{SI,i}, for i=1,2,,Ni=1,2,\ldots,N, are the phase shifts of 𝐡IU\mathbf{h}_{IU} and 𝐡SI\mathbf{h}_{SI}. As the distortion noises are proportional to the signal power, we have

Υt=κtP𝔼[s(t)s(t)]\Upsilon_{t}=\kappa_{t}P\mathbb{E}\left[s(t)s^{*}(t)\right] (6)
Vr=κrP|ϕ(t)(𝐡IUT𝚽𝚯E𝐡SI+hSU)|2𝔼[s(t)s(t)]V_{r}=\kappa_{r}P\left|\phi(t)\left(\mathbf{h}_{IU}^{T}\mathbf{\Phi}\mathbf{\Theta}_{E}\mathbf{h}_{SI}+h_{SU}\right)\right|^{2}\mathbb{E}\left[s(t)s^{*}(t)\right] (7)

where κt\kappa_{t} and κr\kappa_{r} represent the proportionality coefficients which describe the severities of the distortion noises at the transmitter and the receiver, respectively.

For this communication system, we will derive the approximate closed-form ACR expression and the IRS utility in relation to NN in the presence of HWI, and analyse the ACR and utility degradations caused by HWI in the next section.

III ACR Analysis with HWI

Based on the signal model in (3), we will analyse the ACR and the IRS utility of the considered IRS-aided communication system in the presence of HWI. Here we assume that the phase information in the cascaded source-IRS-destination channel model [22] is already estimated before 𝚽\mathbf{\Phi} is adjusted, so that (φIU,i+φSI,i)\left(\varphi_{IU,i}+\varphi_{SI,i}\right), for i=1,2,,Ni=1,2,\ldots,N, are known for the IRS phase shift controller. This can be realized via some existing channel estimation techniques in e.g. [34, 22], which estimated the cascaded channel, and [35, 36], which designed robust and effective channel estimation frameworks based on the PARAllel FACtor (PARAFAC). In (3), 𝐡IUT𝚽𝚯E𝐡SI\mathbf{h}_{IU}^{T}\mathbf{\Phi}\mathbf{\Theta}_{E}\mathbf{h}_{SI} is maximized if each phase shift of the IRS is adjusted into θi=(φIU,i+φSI,i)\theta_{i}=-\left(\varphi_{IU,i}+\varphi_{SI,i}\right), for i=1,2,,Ni=1,2,\ldots,N, to compensate for the phase shifts in 𝐡IU\mathbf{h}_{IU} and 𝐡SI\mathbf{h}_{SI} [23]. As a result, when θi=(φIU,i+φSI,i)\theta_{i}=-\left(\varphi_{IU,i}+\varphi_{SI,i}\right), the received signal affected by HWI is expressed as

y(t)=ϕ(t)(α𝐠IUT𝚯E𝐠SI+hSU)[Ps(t)+ηt(t)]+ηr(t)+w(t)y(t)=\phi(t)\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\left[\sqrt{P}s(t)+\eta_{t}(t)\right]+\eta_{r}(t)+w(t) (8)

where 𝐠IU=μIU𝟏T\mathbf{g}_{IU}=\sqrt{\mu_{IU}}\mathbf{1}^{T} and 𝐠SI=μSI𝟏T\mathbf{g}_{SI}=\sqrt{\mu_{SI}}\mathbf{1}^{T}. Accordingly, the ACR with HWI is expressed as

RHWI(N)=log2{1+P|ϕ(t)(α𝐠IUT𝚯E𝐠SI+hSU)|2P(κt+κr)|ϕ(t)(α𝐠IUT𝚯E𝐠SI+hSU)|2+σw2}\begin{split}R_{HWI}\left(N\right)&=\log_{2}\left\{1+\frac{P\left|\phi(t)\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\right|^{2}}{P(\kappa_{t}+\kappa_{r})\left|\phi(t)\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\right|^{2}+\sigma_{w}^{2}}\right\}\end{split} (9)

Based on (9), we obtain the following theorem.

Theorem 1.

When θi=(φIU,i+φSI,i)\theta_{i}=-\left(\varphi_{IU,i}+\varphi_{SI,i}\right) and θEi\theta_{Ei} is uniformly distributed on [π/2,π/2]\left[-\pi/2,\pi/2\right], the approximate average ACR with HWI is expressed as

RHWI¯(N)=log2{1+βN2+λN+μSU(κt+κr)(βN2+λN+μSU)+σw2P}\overline{R_{HWI}}\left(N\right)=\log_{2}\left\{1+\frac{\beta N^{2}+\lambda N+\mu_{SU}}{\left(\kappa_{t}+\kappa_{r}\right)\left(\beta N^{2}+\lambda N+\mu_{SU}\right)+\frac{\sigma_{w}^{2}}{P}}\right\} (10)

where

β=4α2μIUμSIπ2\beta=\frac{4\alpha^{2}\mu_{IU}\mu_{SI}}{\pi^{2}} (11)
λ=(14π2)α2μIUμSI+4απμIU12μSI12μSU12cos(φSU)\lambda=\left(1-\frac{4}{\pi^{2}}\right)\alpha^{2}\mu_{IU}\mu_{SI}+\frac{4\alpha}{\pi}\mu_{IU}^{\frac{1}{2}}\mu_{SI}^{\frac{1}{2}}\mu_{SU}^{\frac{1}{2}}\cos{(\varphi_{SU})} (12)

The IRS utility with HWI, defined by γHWI(N)=RHWI¯(N)N\gamma_{HWI}(N)=\frac{\partial\overline{R_{HWI}}\left(N\right)}{\partial N} according to the Definition 1 in [31], is expressed as

γHWI(N)=σw2P(2βN+λ){[(κt+κr)(βN2+λN+μSU)+σw2P]×[(κt+κr+1)(βN2+λN+μSU)+σw2P]ln2}1\begin{split}\gamma_{HWI}(N)=\frac{\sigma_{w}^{2}}{P}(2\beta N+\lambda)\left\{\left[(\kappa_{t}+\kappa_{r})(\beta N^{2}+\lambda N+\mu_{SU})+\frac{\sigma_{w}^{2}}{P}\right]\times\right.\\ \left.\left[(\kappa_{t}+\kappa_{r}+1)(\beta N^{2}+\lambda N+\mu_{SU})+\frac{\sigma_{w}^{2}}{P}\right]\ln 2\right\}^{-1}\end{split} (13)
Proof.

The proof is given in Appendix A. ∎

Subsequently, for theoretically evaluating the impact that the HWI has on the ACR and the IRS utility, we further calculate the rate gap, defined by δR(N)=R(N)RHWI¯(N)\delta_{R}(N)=R(N)-\overline{R_{HWI}}\left(N\right), and the utility gap, defined by δγ(N)=γ(N)γHWI(N)\delta_{\gamma}(N)=\gamma(N)-\gamma_{HWI}(N) in the following Lemma 1, where R(N)R(N) and γ(N)\gamma(N), denoting the ACR and the IRS utility without HWI, will be given in the proof.

Lemma 1.

When θi=(φIU,i+φSI,i)\theta_{i}=-\left(\varphi_{IU,i}+\varphi_{SI,i}\right) and θEi\theta_{Ei} is uniformly distributed on [π/2,π/2]\left[-\pi/2,\pi/2\right], the rate gap δR(N)\delta_{R}\left(N\right) between the average ACRs with and without HWI is expressed as

δR(N)=log2{P(κt+κr)χ+σw2+P2χϖ(κtσw2+κrσw2)+PϖP(κt+κr+1)χ+σw2}\delta_{R}\left(N\right)\!=\!\log_{2}\left\{\frac{P\left(\kappa_{t}+\kappa_{r}\right)\chi+\sigma_{w}^{2}+P^{2}\chi\varpi\left(\frac{\kappa_{t}}{\sigma_{w}^{2}}+\frac{\kappa_{r}}{\sigma_{w}^{2}}\right)+P\varpi}{P(\kappa_{t}+\kappa_{r}+1)\chi+\sigma_{w}^{2}}\right\} (14)

where

ϖ=π24βN2+ρN+μSU\varpi=\frac{\pi^{2}}{4}\beta N^{2}+\rho N+\mu_{SU} (15)
χ=βN2+λN+μSU\chi=\beta N^{2}+\lambda N+\mu_{SU} (16)

with ρ\rho given by ρ=2αμIU12μSI12μSU12cos(φSU)\rho=2\alpha\mu_{IU}^{\frac{1}{2}}\mu_{SI}^{\frac{1}{2}}\mu_{SU}^{\frac{1}{2}}\cos{(\varphi_{SU})}.

The utility gap δγ(N)\delta_{\gamma}(N) between the IRS utilities with and without HWI is expressed as

δγ(N)=[P3χ2(κt+κr+1)(κtσw2+κrσw2)ϖN+P2(κt+κr+1)(ϖNχχNϖ)+P2(κt+κr)(ϖNχ+χNϖ)+Pσw2(ϖNχN)]×{[P(κt+κr)χ+σw2+P2ϖχ(κtσw2+κrσw2)+Pϖ][P(κt+κr+1)χ+σw2]ln2}1\begin{split}\delta_{\gamma}(N)=&\left[P^{3}\chi^{2}(\kappa_{t}+\kappa_{r}+1)\left(\frac{\kappa_{t}}{\sigma_{w}^{2}}+\frac{\kappa_{r}}{\sigma_{w}^{2}}\right)\frac{\partial\varpi}{\partial N}+P^{2}(\kappa_{t}+\kappa_{r}+1)\left(\frac{\partial\varpi}{\partial N}\chi-\frac{\partial\chi}{\partial N}\varpi\right)+\right.\\ &\left.P^{2}\left(\kappa_{t}+\kappa_{r}\right)\left(\frac{\partial\varpi}{\partial N}\chi+\frac{\partial\chi}{\partial N}\varpi\right)+P\sigma_{w}^{2}\left(\frac{\partial\varpi}{\partial N}-\frac{\partial\chi}{\partial N}\right)\right]\times\left\{\left[P(\kappa_{t}+\kappa_{r})\chi+\sigma_{w}^{2}+\right.\right.\\ &\left.\left.P^{2}\varpi\chi\left(\frac{\kappa_{t}}{\sigma_{w}^{2}}+\frac{\kappa_{r}}{\sigma_{w}^{2}}\right)+P\varpi\right]\left[P(\kappa_{t}+\kappa_{r}+1)\chi+\sigma_{w}^{2}\right]\ln 2\right\}^{-1}\end{split} (17)

where ϖN=π22βN+ρ\frac{\partial\varpi}{\partial N}=\frac{\pi^{2}}{2}\beta N+\rho and χN=2βN+λ\frac{\partial\chi}{\partial N}=2\beta N+\lambda are the partial derivatives of ϖ\varpi and χ\chi, respectively.

Proof.

According to [23], R(N)R\left(N\right) is expressed as

R(N)=log2{1+P[α2N2μIUμSI+2αNμIUμSIμSUcos(φSU)+μSU]σw2}R\left(N\right)=\log_{2}\left\{1+\frac{P\left[\alpha^{2}N^{2}\mu_{IU}\mu_{SI}+2\alpha N\sqrt{\mu_{IU}\mu_{SI}\mu_{SU}}\cos{\left(\varphi_{SU}\right)}+\mu_{SU}\right]}{\sigma_{w}^{2}}\right\} (18)

Then, the corresponding γ(N)\gamma(N), defined by γ(N)=R(N)N\gamma(N)=\frac{\partial R(N)}{\partial N}, is given by

γ(N)=Pσw2[2α2μIUμSIN+2αμIUμSIμSUcos(φSU)]{1+Pσw2[α2N2μIUμSI+2αNμIUμSIμSUcos(φSU)+μSU]}ln2\begin{split}\gamma(N)&=\frac{\frac{P}{\sigma_{w}^{2}}\left[2\alpha^{2}\mu_{IU}\mu_{SI}N+2\alpha\sqrt{\mu_{IU}\mu_{SI}\mu_{SU}}\cos{\left(\varphi_{SU}\right)}\right]}{\left\{1+\frac{P}{\sigma_{w}^{2}}\left[\alpha^{2}N^{2}\mu_{IU}\mu_{SI}+2\alpha N\sqrt{\mu_{IU}\mu_{SI}\mu_{SU}}\cos{\left(\varphi_{SU}\right)}+\mu_{SU}\right]\right\}\ln 2}\end{split} (19)

Thereupon, by calculating δR(N)=R(N)RHWI¯(N)\delta_{R}(N)=R(N)-\overline{R_{HWI}}\left(N\right) and δγ(N)=γ(N)γHWI(N)=R(N)NRHWI¯(N)N=δR(N)N\delta_{\gamma}(N)=\gamma(N)-\gamma_{HWI}(N)=\frac{\partial R(N)}{\partial N}-\frac{\partial\overline{R_{HWI}}(N)}{\partial N}=\frac{\partial\delta_{R}(N)}{\partial N}, we derive the above (14) and (17). ∎

Theorem 1 demonstrates that: 1) although the RHWI¯(N)\overline{R_{HWI}}\left(N\right) increases with NN, the proportionality coefficient β\beta on N2N^{2} in RHWI¯(N)\overline{R_{HWI}}\left(N\right) is smaller than α2μIUμSI\alpha^{2}\mu_{IU}\mu_{SI} in R(N)R(N), hinting that RHWI¯(N)\overline{R_{HWI}}\left(N\right) rises more slowly than R(N)R(N). 2) When NN\rightarrow\infty, the RHWI¯(N)\overline{R_{HWI}}\left(N\right) is limited by

RHWI¯(N)|N=log2(1+1κt+κr)\left.\overline{R_{HWI}}\left(N\right)\right|_{N\rightarrow\infty}=\log_{2}\left(1+\frac{1}{\kappa_{t}+\kappa_{r}}\right) (20)

which signifies that even if NN becomes significantly large or tends to be infinite, the potential growth of RHWI¯(N)\overline{R_{HWI}}\left(N\right) will be primarily restricted by κt\kappa_{t} and κr\kappa_{r} of the HWI at the signal transceivers. On the contrary, R(N)R(N) continuously ascends without bound as NN grows. 3) The γHWI(N)\gamma_{HWI}(N) is inversely proportional to 𝒪(N3)\mathcal{O}(N^{3}), which indicates that the IRS utility with HWI descends as NN grows, and is close to zero when NN\rightarrow\infty. This implies that if NN is extremely large or nearly infinite, adding more passive reflecting elements will contribute to little ACR improvement when there exists HWI.

Lemma 1 illustrates that: 1) the rate gap δR(N)>0\delta_{R}(N)>0 for N>0N>0, which indicates that the ACR is degraded by HWI. 2) The δR(N)\delta_{R}(N) increases with NN, because the numerator inside log2(.)\log_{2}(.) contains χϖ\chi\varpi which is proportional to 𝒪(N4)\mathcal{O}(N^{4}), while the denominator inside log2(.)\log_{2}(.) merely involves χ\chi which is proportional to 𝒪(N2)\mathcal{O}(N^{2}). This implies that as NN grows, the IRS-aided wireless communication system will suffer from more serious ACR degradation. 3) The utility gap δγ(N)>0\delta_{\gamma}(N)>0, because by expanding (ϖNχχNϖ)\left(\frac{\partial\varpi}{\partial N}\chi-\frac{\partial\chi}{\partial N}\varpi\right) and (ϖNχN)\left(\frac{\partial\varpi}{\partial N}-\frac{\partial\chi}{\partial N}\right) in (17), we have

(ϖNχχNϖ)=4α2μIUμSIN2π2[(π241)α2μIUμSI+(π2)αμIU12μSI12μSU12cos(φSU)]+[(28π2)N+4π21]α2μIUμSIμSU+(24π)αμIU12μSI12μSU32cos(φSU)>0\begin{split}&\left(\frac{\partial\varpi}{\partial N}\chi-\frac{\partial\chi}{\partial N}\varpi\right)=\frac{4\alpha^{2}\mu_{IU}\mu_{SI}N^{2}}{\pi^{2}}\left[\left(\frac{\pi^{2}}{4}-1\right)\alpha^{2}\mu_{IU}\mu_{SI}+(\pi-2)\alpha\mu_{IU}^{\frac{1}{2}}\mu_{SI}^{\frac{1}{2}}\mu_{SU}^{\frac{1}{2}}\cos{(\varphi_{SU})}\right]+\\ &\left[\left(2-\frac{8}{\pi^{2}}\right)N+\frac{4}{\pi^{2}}-1\right]\alpha^{2}\mu_{IU}\mu_{SI}\mu_{SU}+\left(2-\frac{4}{\pi}\right)\alpha\mu_{IU}^{\frac{1}{2}}\mu_{SI}^{\frac{1}{2}}\mu_{SU}^{\frac{3}{2}}\cos{(\varphi_{SU})}>0\end{split} (21)
(ϖNχN)=(2N1)(14π2)α2μIUμSI+(24π)αμIU12μSI12μSU12cos(φSU)>0\begin{split}\left(\frac{\partial\varpi}{\partial N}-\frac{\partial\chi}{\partial N}\right)=(2N-1)\left(1-\frac{4}{\pi^{2}}\right)\alpha^{2}\mu_{IU}\mu_{SI}+\left(2-\frac{4}{\pi}\right)\alpha\mu_{IU}^{\frac{1}{2}}\mu_{SI}^{\frac{1}{2}}\mu_{SU}^{\frac{1}{2}}\cos{(\varphi_{SU})}>0\end{split} (22)

This reveals that the IRS utility will be also degraded by HWI to some extent.

It is notable that the results in Theorem 1 and Lemma 1 are derived on the basis of θi=(φIU,i+φSI,i)\theta_{i}=-\left(\varphi_{IU,i}+\varphi_{SI,i}\right), which is configured to compensate for the phase shifts in 𝐡IU\mathbf{h}_{IU} and 𝐡SI\mathbf{h}_{SI} [23]. However, θi=(φIU,i+φSI,i)\theta_{i}=-\left(\varphi_{IU,i}+\varphi_{SI,i}\right) might not be optimal in this considered wireless propagation environment, as it does not take the phase shift in hSUh_{SU} into account. Thus, in Section IV, we will optimize the IRS phase shifts and reconfigure the phase shifting matrix to obtain the maximum ACR in the presence of HWI.

IV Phase Shift Optimization

Instead of configuring θi=(φIU,i+φSI,i)\theta_{i}=-\left(\varphi_{IU,i}+\varphi_{SI,i}\right) to evaluate the ACR, we will formulate the optimization problem to optimize the IRS phase shifts with HWI in this section.

IV-A Problem Formulation and Transformation

Here, we retrospect (3), from which we obtain the ACR with HWI:

R𝚽,HWI(N)=log2{1+P|ϕ(t)(𝐡IUT𝚽𝚯E𝐡SI+hSU)|2P(κt+κr)|ϕ(t)(𝐡IUT𝚽𝚯E𝐡SI+hSU)|2+σw2}\begin{split}R_{\mathbf{\Phi},HWI}\left(N\right)&=\log_{2}\left\{1+\frac{P\left|\phi(t)\left(\mathbf{h}_{IU}^{T}\mathbf{\Phi}\mathbf{\Theta}_{E}\mathbf{h}_{SI}+h_{SU}\right)\right|^{2}}{P(\kappa_{t}+\kappa_{r})\left|\phi(t)\left(\mathbf{h}_{IU}^{T}\mathbf{\Phi}\mathbf{\Theta}_{E}\mathbf{h}_{SI}+h_{SU}\right)\right|^{2}+\sigma_{w}^{2}}\right\}\end{split} (23)

Therefore, aiming at maximizing the received SNR, we can formulate the phase shift optimization problem as

(P1):max𝚽\displaystyle(\mathrm{P1}):\ \mathop{\max}\limits_{\mathbf{\Phi}} P|ϕ(t)(𝐡IUT𝚽𝚯E𝐡SI+hSU)|2P(κt+κr)|ϕ(t)(𝐡IUT𝚽𝚯E𝐡SI+hSU)|2+σw2\displaystyle\frac{P\left|\phi(t)\left(\mathbf{h}_{IU}^{T}\mathbf{\Phi}\mathbf{\Theta}_{E}\mathbf{h}_{SI}+h_{SU}\right)\right|^{2}}{P(\kappa_{t}+\kappa_{r})\left|\phi(t)\left(\mathbf{h}_{IU}^{T}\mathbf{\Phi}\mathbf{\Theta}_{E}\mathbf{h}_{SI}+h_{SU}\right)\right|^{2}+\sigma_{w}^{2}} (24a)
s.t.\displaystyle s.t.\ |[𝚽](n,n)|=α,n=1,2N\displaystyle\left|\left[\mathbf{\Phi}\right]_{(n,n)}\right|=\alpha,\ n=1,2\ldots N (24b)

However, the objective function (OBF) in (24a) is non-concave with respect to 𝚽\mathbf{\Phi}, and the constraint in (24b) is non-convex. Thus, inspired by [20], we will convert (P1) into another solvable form.

Let 𝐃IU\mathbf{D}_{IU} denote a diagonal matrix expressed as 𝐃IU=diag(𝐡IU)\mathbf{D}_{IU}=diag\left(\mathbf{h}_{IU}\right), and 𝜽\bm{\theta} denote a column vector expressed as 𝜽=α(ejθ1,ejθ2,,ejθN)T\bm{\theta}=\alpha\left(e^{j\theta_{1}},e^{j\theta_{2}},\ldots,e^{j\theta_{N}}\right)^{T}. Then, we have 𝜽T𝐃IU=𝐡IUT𝚽\bm{\theta}^{T}\mathbf{D}_{IU}=\mathbf{h}_{IU}^{T}\mathbf{\Phi}. By replacing 𝐡IUT𝚽\mathbf{h}_{IU}^{T}\mathbf{\Phi} with 𝜽T𝐃IU\bm{\theta}^{T}\mathbf{D}_{IU}, we expand (23) into

R𝜽,HWI(N)=log2{1+P(Z+hSU22)P(κt+κr)(Z+hSU22)+σw2}R_{\bm{\theta},HWI}\left(N\right)=\log_{2}{\left\{1+\frac{P\left(Z+||h_{SU}||_{2}^{2}\right)}{P(\kappa_{t}+\kappa_{r})\left(Z+||h_{SU}||_{2}^{2}\right)+\sigma_{w}^{2}}\right\}} (25)

where Z=𝐡SIH𝚯EH𝐃IUH𝜽𝜽T𝐃IU𝚯E𝐡SI+𝐡SIH𝚯EH𝐃IUH𝜽hSU+hSU𝜽T𝐃IU𝚯E𝐡SIZ=\mathbf{h}_{SI}^{H}\mathbf{\Theta}_{E}^{H}\mathbf{D}_{IU}^{H}\bm{\theta}^{*}\bm{\theta}^{T}\mathbf{D}_{IU}\mathbf{\Theta}_{E}\mathbf{h}_{SI}+\mathbf{h}_{SI}^{H}\mathbf{\Theta}_{E}^{H}\mathbf{D}_{IU}^{H}\bm{\theta}^{*}h_{SU}+h_{SU}^{*}\bm{\theta}^{T}\mathbf{D}_{IU}\mathbf{\Theta}_{E}\mathbf{h}_{SI}.

Let 𝐚\mathbf{a} be defined by 𝐚=(𝜽T,1)H\mathbf{a}=\left(\bm{\theta}^{T},1\right)^{H}. We can rewrite ZZ as Z=𝐚H𝚵𝐚Z=\mathbf{a}^{H}\mathbf{\Xi}\mathbf{a}, where

𝚵=(𝐃IU𝚯E𝐡SI𝐡SIH𝚯EH𝐃IUHhSU𝐃IU𝚯E𝐡SI𝐡SIH𝚯EH𝐃IUHhSU0)\mathbf{\Xi}=\left(\begin{matrix}\mathbf{D}_{IU}\mathbf{\Theta}_{E}\mathbf{h}_{SI}\mathbf{h}_{SI}^{H}\mathbf{\Theta}_{E}^{H}\mathbf{D}_{IU}^{H}&h_{SU}^{*}\mathbf{D}_{IU}\mathbf{\Theta}_{E}\mathbf{h}_{SI}\\ \mathbf{h}_{SI}^{H}\mathbf{\Theta}_{E}^{H}\mathbf{D}_{IU}^{H}h_{SU}&0\\ \end{matrix}\right) (26)

Therefore, R𝜽,HWI(N)R_{\bm{\theta},HWI}\left(N\right) can be simplified into

R𝜽,HWI(N)=log2{1+P(𝐚H𝚵𝐚+hSU22)P(κt+κr)(𝐚H𝚵𝐚+hSU22)+σw2}=log2{1+P[tr(𝚵𝐗)+hSU22]P(κt+κr)[tr(𝚵𝐗)+hSU22]+σw2}\begin{split}R_{\bm{\theta},HWI}\left(N\right)=&\log_{2}{\left\{1+\frac{P\left(\mathbf{a}^{H}\mathbf{\Xi}\mathbf{a}+||h_{SU}||_{2}^{2}\right)}{P(\kappa_{t}+\kappa_{r})\left(\mathbf{a}^{H}\mathbf{\Xi}\mathbf{a}+||h_{SU}||_{2}^{2}\right)+\sigma_{w}^{2}}\right\}}\\ =&\log_{2}{\left\{1+\frac{P\left[tr(\mathbf{\Xi}\mathbf{X})+||h_{SU}||_{2}^{2}\right]}{P(\kappa_{t}+\kappa_{r})\left[tr(\mathbf{\Xi}\mathbf{X})+||h_{SU}||_{2}^{2}\right]+\sigma_{w}^{2}}\right\}}\end{split} (27)

where

𝐗=𝐚𝐚H=(𝜽𝜽T𝜽𝜽T1)(N+1)×(N+1)\mathbf{X}=\mathbf{a}\mathbf{a}^{H}=\left(\begin{matrix}\bm{\theta}^{*}\bm{\theta}^{T}&\bm{\theta}^{*}\\ \bm{\theta}^{T}&1\\ \end{matrix}\right)\in\mathbb{C}^{\left(N+1\right)\times\left(N+1\right)} (28)

Then, the optimization problem is formulated as

(P2):max𝜽\displaystyle(\mathrm{P2}):\ \mathop{\max}\limits_{\bm{\theta}} P[tr(𝚵𝐗)+hSU22]P(κt+κr)[tr(𝚵𝐗)+hSU22]+σw2\displaystyle\frac{P\left[tr(\mathbf{\Xi}\mathbf{X})+||h_{SU}||_{2}^{2}\right]}{P(\kappa_{t}+\kappa_{r})\left[tr(\mathbf{\Xi}\mathbf{X})+||h_{SU}||_{2}^{2}\right]+\sigma_{w}^{2}} (29a)
s.t.\displaystyle s.t.\ |[𝜽]n|=α,n=1,2N\displaystyle\left|\left[\bm{\theta}\right]_{n}\right|=\alpha,\ n=1,2\ldots N (29b)

which is still non-convex due to the complicated non-concave OBF in (29a) and the non-convex module constraint in (29b).

Here, from 𝜽𝜽T\bm{\theta}^{*}\bm{\theta}^{T} in (28), it can be realized that the diagonal entries in 𝐗\mathbf{X} embody the modules of the elements in 𝜽\bm{\theta}. Thus, we define a simple matrix 𝐄n\mathbf{E}_{n}, whose (i,j)(i,j)-th element is given by

[𝐄n](i,j)={1,i=j=n0,otherwise\left[\mathbf{E}_{n}\right]_{(i,j)}=\left\{\begin{matrix}1,\ \ \ \ \ i=j=n\\ 0,\ \ \ \ otherwise\\ \end{matrix}\right. (30)

As a result, the optimization problem is converted into

(P3):max𝐗𝟎\displaystyle(\mathrm{P3}):\ \mathop{\max}\limits_{\mathbf{X}\succeq\mathbf{0}} P[tr(𝚵𝐗)+hSU22]P(κt+κr)[tr(𝚵𝐗)+hSU22]+σw2\displaystyle\frac{P\left[tr(\mathbf{\Xi}\mathbf{X})+||h_{SU}||_{2}^{2}\right]}{P(\kappa_{t}+\kappa_{r})\left[tr(\mathbf{\Xi}\mathbf{X})+||h_{SU}||_{2}^{2}\right]+\sigma_{w}^{2}} (31a)
s.t.\displaystyle s.t.\ tr(𝐄n𝐗)=α2,n=1,2N\displaystyle tr\left(\mathbf{E}_{n}\mathbf{X}\right)=\alpha^{2},\ n=1,2\ldots N (31b)
tr(𝐄N+1𝐗)=1\displaystyle tr\left(\mathbf{E}_{N+1}\mathbf{X}\right)=1 (31c)
rank(𝐗)=1\displaystyle rank(\mathbf{X})=1 (31d)

where the constraint in (31b) is transformed from the module constraint of |[𝜽]n|2=[𝜽𝜽T](n,n)=𝐚H𝐄n𝐚=tr(𝐄n𝐗)=α2\left|\left[\bm{\theta}\right]_{n}\right|^{2}=\left[\bm{\theta}^{*}\bm{\theta}^{T}\right]_{(n,n)}=\mathbf{a}^{H}\mathbf{E}_{n}\mathbf{a}=tr\left(\mathbf{E}_{n}\mathbf{X}\right)=\alpha^{2}, for n=1,2Nn=1,2\ldots N; the constraint in (31c) is transformed from [𝐗](N+1,N+1)=1\left[\mathbf{X}\right]_{(N+1,N+1)}=1; the constraint in (31d) is responsible for strictly guaranteeing that 1) the resolved 𝐗\mathbf{X} can be decomposed into 𝐗=𝐚𝐚H\mathbf{X}=\mathbf{a}\mathbf{a}^{H}, and 2) the solution of the phase shift in 𝜽\bm{\theta} in the resolved 𝐗\mathbf{X} is equivalent to the solution of the phase shift in 𝚽\mathbf{\Phi} in (P1).

Nevertheless, (P3) is still non-convex and is difficult to solve. Therefore, the problem transformation should be further performed. Thanks to the Charnes-Cooper transformation [37, 46], let 𝐘\mathbf{Y} and μ\mu be defined by 𝐘=μ𝐗\mathbf{Y}=\mu\mathbf{X} and μ=1tr(𝚵𝐗)+hSU22+σw2P(κt+κr)\mu=\frac{1}{tr(\mathbf{\Xi}\mathbf{X})+||h_{SU}||_{2}^{2}+\frac{\sigma_{w}^{2}}{P\left(\kappa_{t}+\kappa_{r}\right)}}. Then, the OBF in (31a) is expressed as 1(κt+κr)×[tr(𝚵𝐘)+μhSU22]\frac{1}{\left(\kappa_{t}+\kappa_{r}\right)}\times\left[tr(\mathbf{\Xi}\mathbf{Y})+\mu||h_{SU}||_{2}^{2}\right]. Therefore, (P3) is transformed into

(P4):max𝐘𝟎,μ0\displaystyle(\mathrm{P4}):\ \mathop{\max}\limits_{\mathbf{Y}\succeq\mathbf{0},\mu\geq 0} 1(κt+κr)×[tr(𝚵𝐘)+μhSU22]\displaystyle\frac{1}{\left(\kappa_{t}+\kappa_{r}\right)}\times\left[tr(\mathbf{\Xi}\mathbf{Y})+\mu||h_{SU}||_{2}^{2}\right] (32a)
s.t.\displaystyle s.t.\ tr(𝐄n𝐘)=μα2,n=1,2N\displaystyle tr\left(\mathbf{E}_{n}\mathbf{Y}\right)=\mu\alpha^{2},\ n=1,2\ldots N (32b)
tr(𝐄N+1𝐘)=μ\displaystyle tr\left(\mathbf{E}_{N+1}\mathbf{Y}\right)=\mu (32c)
tr(𝚵𝐘)+μ[hSU22+σw2P(κt+κr)]=1\displaystyle tr\left(\mathbf{\Xi Y}\right)+\mu\left[||h_{SU}||_{2}^{2}+\frac{\sigma_{w}^{2}}{P\left(\kappa_{t}+\kappa_{r}\right)}\right]=1 (32d)
rank(𝐘)=1\displaystyle rank(\mathbf{Y})=1 (32e)

Although (P4) is still non-convex due to the non-convex (32e), it can be relaxed if the constraint of rank(𝐘)=1rank(\mathbf{Y})=1 is omitted. Hence, the relaxed problem is formulated as

(P5):max𝐘𝟎,μ0\displaystyle(\mathrm{P5}):\ \mathop{\max}\limits_{\mathbf{Y}\succeq\mathbf{0},\mu\geq 0} 1(κt+κr)×[tr(𝚵𝐘)+μhSU22]\displaystyle\frac{1}{\left(\kappa_{t}+\kappa_{r}\right)}\times\left[tr(\mathbf{\Xi}\mathbf{Y})+\mu||h_{SU}||_{2}^{2}\right] (33a)
s.t.\displaystyle s.t.\ tr(𝐄n𝐘)=μα2,n=1,2N\displaystyle tr\left(\mathbf{E}_{n}\mathbf{Y}\right)=\mu\alpha^{2},\ n=1,2\ldots N (33b)
tr(𝐄N+1𝐘)=μ\displaystyle tr\left(\mathbf{E}_{N+1}\mathbf{Y}\right)=\mu (33c)
tr(𝚵𝐘)+μ[hSU22+σw2P(κt+κr)]=1\displaystyle tr\left(\mathbf{\Xi Y}\right)+\mu\left[||h_{SU}||_{2}^{2}+\frac{\sigma_{w}^{2}}{P\left(\kappa_{t}+\kappa_{r}\right)}\right]=1 (33d)

which is currently a SDP problem and can be solved by existing techniques [38].

However, the matrix 𝚵\mathbf{\Xi} involves the stochastic phase errors, which are generally unknown due to their randomness and prevent us from predetermining 𝚵\mathbf{\Xi} and obtaining the solution in reality. In view of this issue, we will further calculate the expectation of 𝚵\mathbf{\Xi}, denoted by 𝔼𝚯E[𝚵]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right], in order to facilitate the optimization procedure and achieve a statistical average optimization result.

IV-B Expectation of 𝚵\mathbf{\Xi}

According to (26), 𝔼𝚯E[𝚵]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right] can be written as

𝔼𝚯E[𝚵]=𝔼𝐯E[𝚵]=(𝐃IU𝐃SI𝔼𝐯E[𝐯E𝐯EH]𝐃SIH𝐃IUHhSU𝐃IU𝐃SI𝔼𝐯E[𝐯E]𝔼𝐯E[𝐯EH]𝐃SIH𝐃IUHhSU0)\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right]=\mathbb{E}_{\mathbf{v}_{E}}\left[\mathbf{\Xi}\right]=\left(\begin{matrix}\mathbf{D}_{IU}\mathbf{D}_{SI}\mathbb{E}_{\mathbf{v}_{E}}\!\!\left[\mathbf{v}_{E}\mathbf{v}_{E}^{H}\right]\mathbf{D}_{SI}^{H}\mathbf{D}_{IU}^{H}&h_{SU}^{*}\mathbf{D}_{IU}\mathbf{D}_{SI}\mathbb{E}_{\mathbf{v}_{E}}\!\!\left[\mathbf{v}_{E}\right]\\ \mathbb{E}_{\mathbf{v}_{E}}\!\!\left[\mathbf{v}_{E}^{H}\right]\mathbf{D}_{SI}^{H}\mathbf{D}_{IU}^{H}h_{SU}&0\\ \end{matrix}\right) (34)

where 𝐃SI=diag(𝐡SI)\mathbf{D}_{SI}=diag(\mathbf{h}_{SI}) and 𝐯E=(ejθE1,ejθE2,,ejθEN)T\mathbf{v}_{E}=\left(e^{j\theta_{E1}},e^{j\theta_{E2}},\ldots,e^{j\theta_{EN}}\right)^{T}. 𝔼𝐯E[𝐯E𝐯EH]\mathbb{E}_{\mathbf{v}_{E}}\left[\mathbf{v}_{E}\mathbf{v}_{E}^{H}\right], which is expressed as

𝔼𝐯E[𝐯E𝐯EH]=(1𝔼δθ[ejθE1jθE2]𝔼δθ[ejθE2jθE1]1𝔼δθ[ejθE1jθEN]𝔼δθ[ejθE2jθEN]𝔼δθ[ejθENjθE1]𝔼δθ[ejθENjθE2] 1)\begin{split}\mathbb{E}_{\mathbf{v}_{E}}\left[\mathbf{v}_{E}\mathbf{v}_{E}^{H}\right]=\left(\begin{matrix}\begin{matrix}1&\mathbb{E}_{\delta_{\theta}}\!\!\left[e^{j\theta_{E1}-j\theta_{E2}}\right]\\ \mathbb{E}_{\delta_{\theta}}\!\!\left[e^{j\theta_{E2}-j\theta_{E1}}\right]&1\\ \end{matrix}&\begin{matrix}\cdots&\mathbb{E}_{\delta_{\theta}}\!\!\left[e^{j\theta_{E1}-j\theta_{EN}}\right]\\ \cdots&\mathbb{E}_{\delta_{\theta}}\!\!\left[e^{j\theta_{E2}-j\theta_{EN}}\right]\\ \end{matrix}\\ \begin{matrix}\vdots&\vdots\\ \mathbb{E}_{\delta_{\theta}}\!\!\left[e^{j\theta_{EN}-j\theta_{E1}}\right]&\mathbb{E}_{\delta_{\theta}}\!\!\left[e^{j\theta_{EN}-j\theta_{E2}}\right]\\ \end{matrix}&\begin{matrix}\ddots&\ \ \ \ \ \ \ \ \ \vdots\ \ \ \ \ \ \ \ \ \\ \cdots&\ \ \ 1\ \ \ \\ \end{matrix}\\ \end{matrix}\right)\end{split} (35)

represents the autocorrelation matrix of 𝐯E\mathbf{v}_{E}, where δθ=θEiθEj\delta_{\theta}=\theta_{Ei}-\theta_{Ej} obeys triangular distribution on [π,π][-\pi,\pi] as θEi\theta_{Ei} obeys uniform distribution on [π/2,π/2]\left[-\pi/2,\pi/2\right] (detailed in Appendix A). Because 𝔼δθ[ejθEijθEj]=𝔼δθ[ejδθ]=ππf(δθ)ejδθ𝑑δθ=4/π2\mathbb{E}_{\delta_{\theta}}\left[e^{j\theta_{Ei}-j\theta_{Ej}}\right]=\mathbb{E}_{\delta_{\theta}}\left[e^{j\delta_{\theta}}\right]=\int_{-\pi}^{\pi}{f\left(\delta_{\theta}\right)e^{j\delta_{\theta}}d\delta_{\theta}}=4/\pi^{2}, where f(δθ)f\left(\delta_{\theta}\right), expressed as (65) in Appendix A, is the probability density function of δθ\delta_{\theta}, we have 𝔼𝐯E[𝐯E𝐯EH]=𝐈N+𝐉\mathbb{E}_{\mathbf{v}_{E}}\left[\mathbf{v}_{E}\mathbf{v}_{E}^{H}\right]=\mathbf{I}_{N}+\mathbf{J}, where the (i,j)(i,j)-th element in the matrix 𝐉\mathbf{J} is expressed as

[𝐉](i,j)={0,i=j4π2,ij\left[\mathbf{J}\right]_{(i,j)}=\left\{\begin{matrix}0,\ \ \ i=j\\ \frac{4}{\pi^{2}},\ \ i\neq j\end{matrix}\right. (36)

Moreover, because 𝔼𝐯E[𝐯E]=(𝔼θEi[ejθE1],𝔼θEi[ejθE2],,𝔼θEi[ejθEN])T\mathbb{E}_{\mathbf{v}_{E}}\left[\mathbf{v}_{E}\right]=\left(\mathbb{E}_{\theta_{Ei}}\!\!\left[e^{j\theta_{E1}}\right],\mathbb{E}_{\theta_{Ei}}\!\!\left[e^{j\theta_{E2}}\right],\ldots,\mathbb{E}_{\theta_{Ei}}\!\!\left[e^{j\theta_{EN}}\right]\right)^{T} and 𝔼θEi[ejθEi]=π2π2f(θEi)ejθEi𝑑θEi=π2π2f(θEi)(cosθEi+jsinθEi)𝑑θEi=2/π\mathbb{E}_{\theta_{Ei}}\left[e^{j\theta_{Ei}}\right]=\int_{-\frac{\pi}{2}}^{\frac{\pi}{2}}{f(\theta_{Ei})e^{j\theta_{Ei}}d\theta_{Ei}}=\int_{-\frac{\pi}{2}}^{\frac{\pi}{2}}{f(\theta_{Ei})(cos\theta_{Ei}+jsin\theta_{Ei})d\theta_{Ei}}=2/\pi for i=1,2,,Ni=1,2,...,N, where f(θEi)=1/πf\left(\theta_{Ei}\right)=1/\pi is the probability density function of θEi\theta_{Ei}, we have 𝔼𝐯E[𝐯E]=(2/π)𝟏T\mathbb{E}_{\mathbf{v}_{E}}\left[\mathbf{v}_{E}\right]=\left(2/\pi\right)\mathbf{1}^{T}.

By substituting 𝔼𝐯E[𝐯E𝐯EH]=𝐈N+𝐉\mathbb{E}_{\mathbf{v}_{E}}\left[\mathbf{v}_{E}\mathbf{v}_{E}^{H}\right]=\mathbf{I}_{N}+\mathbf{J} and 𝔼𝐯E[𝐯E]=(2/π)𝟏T\mathbb{E}_{\mathbf{v}_{E}}\left[\mathbf{v}_{E}\right]=\left(2/\pi\right)\mathbf{1}^{T} into (34), we have

𝔼𝚯E[𝚵]=(𝐃IU𝐃SI(𝐈N+𝐉)𝐃SIH𝐃IUH2πhSU𝐃IU𝐃SI𝟏T2π𝟏𝐃SIH𝐃IUHhSU0)\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right]=\left(\begin{matrix}\mathbf{D}_{IU}\mathbf{D}_{SI}(\mathbf{I}_{N}+\mathbf{J})\mathbf{D}_{SI}^{H}\mathbf{D}_{IU}^{H}&\frac{2}{\pi}h_{SU}^{*}\mathbf{D}_{IU}\mathbf{D}_{SI}\mathbf{1}^{T}\\ \frac{2}{\pi}\mathbf{1}\mathbf{D}_{SI}^{H}\mathbf{D}_{IU}^{H}h_{SU}&0\\ \end{matrix}\right) (37)

Consequently, by replacing 𝚵\mathbf{\Xi} in (P5) with 𝔼𝚯E[𝚵]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right], we obtain

(P6):max𝐘𝟎,μ~0\displaystyle(\mathrm{P6}):\ \mathop{\max}\limits_{\mathbf{Y}\succeq\mathbf{0},\widetilde{\mu}\geq 0} 1(κt+κr)×[tr(𝔼𝚯E[𝚵]𝐘)+μ~hSU22]\displaystyle\frac{1}{\left(\kappa_{t}+\kappa_{r}\right)}\times\left[tr(\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right]\mathbf{Y})+\widetilde{\mu}||h_{SU}||_{2}^{2}\right] (38a)
s.t.\displaystyle s.t.\ tr(𝐄n𝐘)=μ~α2,n=1,2N\displaystyle tr\left(\mathbf{E}_{n}\mathbf{Y}\right)=\widetilde{\mu}\alpha^{2},\ n=1,2\ldots N (38b)
tr(𝐄N+1𝐘)=μ~\displaystyle tr\left(\mathbf{E}_{N+1}\mathbf{Y}\right)=\widetilde{\mu} (38c)
tr(𝔼𝚯E[𝚵]𝐘)+μ~[hSU22+σw2P(κt+κr)]=1\displaystyle tr\left(\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right]\mathbf{Y}\right)+\widetilde{\mu}\left[||h_{SU}||_{2}^{2}+\frac{\sigma_{w}^{2}}{P\left(\kappa_{t}+\kappa_{r}\right)}\right]=1 (38d)

where μ~=1tr(𝔼𝚯E[𝚵]𝐗)+hSU22+σw2P(κt+κr)\widetilde{\mu}=\frac{1}{tr(\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right]\mathbf{X})+||h_{SU}||_{2}^{2}+\frac{\sigma_{w}^{2}}{P\left(\kappa_{t}+\kappa_{r}\right)}}.

Currently, because the matrix 𝔼𝚯E[𝚵]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right] in the OBF and constraints only includes the channel coefficients, which can be estimated via existing channel estimation techniques, it is easy for us to configure 𝔼𝚯E[𝚵]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right], which assists us in completing the phase shift optimization in terms of maximizing the average SNR in the presence of HWI.

It is remarkable that after (P6) is solved, the 𝜽T\bm{\theta}^{T} in the (N+1)(N+1)-th row of the 𝐗=μ~1𝐘\mathbf{X}=\widetilde{\mu}^{-1}\mathbf{Y} in the solution can be extracted to reconstruct 𝐘\mathbf{Y} based on (28) and 𝐘=μ~𝐗\mathbf{Y}=\widetilde{\mu}\mathbf{X}. If the reconstructed 𝐘\mathbf{Y}, denoted by 𝐘r\mathbf{Y}_{r}, satisfies 𝐘r=𝐘\mathbf{Y}_{r}=\mathbf{Y} and rank(𝐘r)=1rank(\mathbf{Y}_{r})=1, the 𝜽T\bm{\theta}^{T} can be regarded as the optimal phase shift vector. As a result, we will test the values in 𝐘r\mathbf{Y}_{r} and the rank of 𝐘r\mathbf{Y}_{r} in the simulations in Section VI, in order to investigate whether the optimal IRS phase shifts can be acquired from 𝜽T\bm{\theta}^{T} in the (N+1)(N+1)-th row of the 𝐗=μ~1𝐘\mathbf{X}=\widetilde{\mu}^{-1}\mathbf{Y} in the solution of the relaxed problem.

In addition, after the phase shift optimization process, two possible factors may still remain and influence the performance. 1) Most channel estimation methods suffer from estimation errors, which lead to imperfect CSI of 𝐡IU\mathbf{h}_{IU}, 𝐡SI\mathbf{h}_{SI} and hSUh_{SU}. Based on the imperfect CSI, we can only construct an inaccurate 𝔼𝚯E[𝚵]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right], and then acquire a non-optimal phase shift vector. 2) Due to the inherent hardware imperfection, synchronization offset and estimation accuracy limit in the real world, the optimized phase values may not be precisely obtained. In this case, we may actually obtain 𝜽~T=𝜽T𝜽pT\widetilde{\bm{\theta}}^{T}=\bm{\theta}^{T}\odot\bm{\theta}_{p}^{T} instead of 𝜽T\bm{\theta}^{T} after the optimization, where 𝜽p=(ejθp1,ejθp2,,ejθpN)T\bm{\theta}_{p}=(e^{j\theta_{p1}},e^{j\theta_{p2}},...,e^{j\theta_{pN}})^{T} denotes a residual phase noise vector with θpi\theta_{pi} being the ii-th random residual phase noise, which may disturb 𝜽T\bm{\theta}^{T} and affect the optimization performance.

The performance degradation caused by the aforementioned two factors is worth to be discussed. Thus, we will present the discussions on them in Section VI.

  

V Comparisons with DF Relay

The DF relay is a conventional active approach which is also applied for data transmission enhancement in the wireless communication network. Hence, it is necessary to compare the performance of the IRS with that of the DF relay in the same situation. It was already confirmed that the ideal-hardware IRS equipped with a large number of reflecting units could help the wireless communication system provide higher ACR than the ideal-hardware DF relay equipped with one antenna [23]. However, the comparisons in [23] were made in consideration of single-antenna DF relay and multiple-unit IRS without HWI. Note that as NN grows, the average ACR of the multiple-unit IRS-aided communication system increases, while that of the single-antenna DF relay assisted communication system remains constant under a certain condition. This might be unfair for the DF relay during the comparisons. Therefore, in this section, we will compare the performances of the IRS with NN passive reflecting units and the DF relay with NN active antennas, for the purpose of exploring whether the IRS can still possess advantages in ACR and utility over the multiple-antenna DF relay when there exists HWI.

Before the comparisons, determining the exact closed-form ACR of the multiple-antenna DF relay assisted communication system with respect to NN in the presence of HWI, is a hard nut to crack, as the channel coefficients include random phase shifts, which cannot be compensated by the DF relay. Fortunately, we realize that the source-to-relay and the relay-to-destination channels can similarly be regarded as the uplink and downlink channels modelled in [27], which assists us in establishing the closed-form upper bound of the ACR in relation to NN for the multiple-antenna DF relay supported communication system.

Let 𝐡SR\mathbf{h}_{SR}, 𝐡RU\mathbf{h}_{RU} and hSUh_{SU} denote the source-to-relay, relay-to-destination and source-to-destination channels, respectively. For comparing, we assume that 𝐡SR=𝐡SI\mathbf{h}_{SR}=\mathbf{h}_{SI}, 𝐡RU=𝐡IU\mathbf{h}_{RU}=\mathbf{h}_{IU}, and the receiver noises at the DF relay and the destination terminal have the same variance of σw2\sigma_{w}^{2}. If the HWI appears at the source transmitter, the DF relay and the destination receiver, according to Eq. (6) and Eq. (2) in [27], the signals received by the DF relay and the destination terminal are modelled as

𝐲DF(t)=𝐡SR[P1s(t)+ηt(t)]+𝜼rDF(t)+𝐰DF(t)\mathbf{y}_{DF}(t)=\mathbf{h}_{SR}\left[\sqrt{P_{1}}s(t)+\eta_{t}(t)\right]+\bm{\eta}_{r_{DF}}(t)+\mathbf{w}_{DF}(t) (39)

and

yU1(t)=𝐡RU[P2𝐬(t)+𝜼tDF(t)]+ηr1(t)+w(t)y_{U1}(t)=\mathbf{h}_{RU}\left[\sqrt{P_{2}}\mathbf{s}(t)+\bm{\eta}_{t_{DF}}(t)\right]+\eta_{r1}(t)+w(t) (40)
yU2(t)=hSU[P1s(t)+ηt(t)]+ηr2(t)+w(t)y_{U2}(t)=h_{SU}\left[\sqrt{P_{1}}s(t)+\eta_{t}(t)\right]+\eta_{r2}(t)+w(t) (41)

where P1P_{1} and P2P_{2} are the transmitting powers of the source and the DF relay under the constraint of P=P1+P22P=\frac{P_{1}+P_{2}}{2} [23]; yU1(t)y_{U1}(t) and yU2(t)y_{U2}(t) are the signals received by the destination terminal through channel 𝐡RU\mathbf{h}_{RU} and hSUh_{SU}, respectively; 𝐰DF(t)𝒞𝒩(𝟎,σw2𝐈)\mathbf{w}_{DF}(t)\sim\mathcal{CN}(\mathbf{0},\sigma_{w}^{2}\mathbf{I}) and w(t)𝒞𝒩(0,σw2)w(t)\sim\mathcal{CN}(0,\sigma_{w}^{2}) are the receiver noises at the DF relay and the destination terminal; ηt(t)𝒞𝒩(0,Υt)\eta_{t}(t)\sim\mathcal{CN}(0,\Upsilon_{t}), 𝜼rDF(t)𝒞𝒩(𝟎,𝐕rDF)\bm{\eta}_{r_{DF}}(t)\sim\mathcal{CN}(\mathbf{0},\mathbf{V}_{r_{DF}}), 𝜼tDF(t)𝒞𝒩(𝟎,𝚼tDF)\bm{\eta}_{t_{DF}}(t)\sim\mathcal{CN}(\mathbf{0},\mathbf{\Upsilon}_{t_{DF}}), ηr1(t)𝒞𝒩(0,Vr1)\eta_{r1}(t)\sim\mathcal{CN}(0,V_{r1}) and ηr2(t)𝒞𝒩(0,Vr2)\eta_{r2}(t)\sim\mathcal{CN}(0,V_{r2}) are the distortion noises at the source transmitter, the DF-relay receiver, the DF-relay transmitter and the destination receiver, respectively, with Υt\Upsilon_{t}, 𝐕rDF\mathbf{V}_{r_{DF}}, 𝚼tDF\mathbf{\Upsilon}_{t_{DF}}, Vr1V_{r1} and Vr2V_{r2} given by

Υt=κtP1𝔼[s(t)s(t)]\Upsilon_{t}=\kappa_{t}P_{1}\mathbb{E}[s(t)s^{*}(t)] (42)
𝐕rDF=κrDFP1𝔼[s(t)s(t)]×diag(|hSR,1|2,,|hSR,N|2)\mathbf{V}_{r_{DF}}=\kappa_{r_{DF}}P_{1}\mathbb{E}[s(t)s^{*}(t)]\times diag(|h_{SR,1}|^{2},...,|h_{SR,N}|^{2}) (43)
𝚼tDF=κtDFP2×diag{𝔼[s1(t)s1(t)],,𝔼[sN(t)sN(t)]}\mathbf{\Upsilon}_{t_{DF}}=\kappa_{t_{DF}}P_{2}\times diag\{\mathbb{E}[s_{1}(t)s_{1}^{*}(t)],...,\mathbb{E}[s_{N}(t)s_{N}^{*}(t)]\} (44)
Vr1=κr1P2𝐡RUT𝔼[𝐬(t)𝐬H(t)]𝐡RUV_{r1}=\kappa_{r1}P_{2}\mathbf{h}_{RU}^{T}\mathbb{E}[\mathbf{s}(t)\mathbf{s}^{H}(t)]\mathbf{h}_{RU}^{*} (45)
Vr2=κr2P1|hSU|2𝔼[s(t)s(t)]V_{r2}=\kappa_{r2}P_{1}|h_{SU}|^{2}\mathbb{E}[s(t)s^{*}(t)] (46)

where 𝐬(t)\mathbf{s}(t) denotes the signal transmitted by the DF relay at time tt; si(t)s_{i}(t), for i=1,2,,Ni=1,2,...,N, represents the ii-th transmit symbol in 𝐬(t)\mathbf{s}(t), with 𝔼[si(t)si(t)]=1\mathbb{E}[s_{i}(t)s_{i}^{*}(t)]=1; κt\kappa_{t}, κrDF\kappa_{r_{DF}}, κtDF\kappa_{t_{DF}}, κr1\kappa_{r1} and κr2\kappa_{r2} are the proportionality factors.

For simple analysis, we consider that κtDF=κt\kappa_{t_{DF}}=\kappa_{t} and κr1=κr2=κrDF=κr\kappa_{r1}=\kappa_{r2}=\kappa_{r_{DF}}=\kappa_{r}, as the hardware characteristics of the transceivers in the DF relay are similar to those in the source equipment and the destination terminal. Therefore, referring to Eq. (26), Eq. (27) in [27], and Eq. (15) in [39], the upper bound of the ACR of the multiple-antenna DF relay assisted communication system with HWI is expressed as

RHWIDF(N)=12min{𝔄(N),𝔅(N)}R_{HWI}^{DF}(N)=\frac{1}{2}\min{\left\{\mathfrak{A}(N),\mathfrak{B}(N)\right\}} (47)

where

𝔄(N)=log2(1+NμSIκrμSI+NκtμSI+σw2P1)\mathfrak{A}(N)=\log_{2}\left(1+\frac{N\mu_{SI}}{\kappa_{r}\mu_{SI}+N\kappa_{t}\mu_{SI}+\frac{\sigma_{w}^{2}}{P_{1}}}\right) (48)
𝔅(N)=log2(1+μSU(κt+κr)μSU+σw2P1+NμIUκtμIU+NκrμIU+σw2P2)\mathfrak{B}(N)=\log_{2}\left(1+\frac{\mu_{SU}}{(\kappa_{t}+\kappa_{r})\mu_{SU}+\frac{\sigma_{w}^{2}}{P_{1}}}+\frac{N\mu_{IU}}{\kappa_{t}\mu_{IU}+N\kappa_{r}\mu_{IU}+\frac{\sigma_{w}^{2}}{P_{2}}}\right) (49)

Correspondingly, the utility of the multiple-antenna DF relay is expressed as

γHWIDF(N)={κrμSI2+σw2P1μSI2(κrμSI+NκtμSI+σw2P1)(κrμSI+NκtμSI+σw2P1+NμSI)ln2,𝔄(N)<𝔅(N)κtμIU2+σw2P2μIU2(1+μSU(κt+κr)μSU+σw2P1+NμIUκtμIU+NκrμIU+σw2P2)(κtμIU+NκrμIU+σw2P2)2ln2,𝔄(N)>𝔅(N)\gamma_{HWI}^{DF}(N)=\left\{\begin{matrix}\frac{\kappa_{r}\mu_{SI}^{2}+\frac{\sigma_{w}^{2}}{P_{1}}\mu_{SI}}{2\left(\kappa_{r}\mu_{SI}+N\kappa_{t}\mu_{SI}+\frac{\sigma_{w}^{2}}{P_{1}}\right)\left(\kappa_{r}\mu_{SI}+N\kappa_{t}\mu_{SI}+\frac{\sigma_{w}^{2}}{P_{1}}+N\mu_{SI}\right)\ln 2},\ \ \mathfrak{A}(N)<\mathfrak{B}(N)\\ \frac{\kappa_{t}\mu_{IU}^{2}+\frac{\sigma_{w}^{2}}{P_{2}}\mu_{IU}}{2\left(1+\frac{\mu_{SU}}{(\kappa_{t}+\kappa_{r})\mu_{SU}+\frac{\sigma_{w}^{2}}{P_{1}}}+\frac{N\mu_{IU}}{\kappa_{t}\mu_{IU}+N\kappa_{r}\mu_{IU}+\frac{\sigma_{w}^{2}}{P_{2}}}\right)\left(\kappa_{t}\mu_{IU}+N\kappa_{r}\mu_{IU}+\frac{\sigma_{w}^{2}}{P_{2}}\right)^{2}\ln 2},\ \ \mathfrak{A}(N)>\mathfrak{B}(N)\end{matrix}\right. (50)

For analysis convenience and symbol unification, we assume that κt+κr=κ\kappa_{t}+\kappa_{r}=\kappa with κt=κr=12κ\kappa_{t}=\kappa_{r}=\frac{1}{2}\kappa [27], and the total transmitting power of the DF relay assisted communication system (P1+P2=2PP_{1}+P_{2}=2P) is allocated by P1=P2=PP_{1}=P_{2}=P. Subsequently, in order to investigate whether the IRS is potentially capable of outperforming the DF relay in the presence of HWI, we will compare RHWIDF(N)R_{HWI}^{DF}(N) in (47) with RHWI¯(N)\overline{R_{HWI}}(N) in (10) from the perspective of scaling law, by considering first NN\rightarrow\infty and then PP\rightarrow\infty in the following Lemma 2 and Lemma 3.

Lemma 2.

When NN\rightarrow\infty, we have

RHWI¯(N)|N>RHWIDF(N)|N\left.\overline{R_{HWI}}(N)\right|_{N\rightarrow\infty}>\left.R_{HWI}^{DF}(N)\right|_{N\rightarrow\infty} (51)
γHWI(N)|N=γHWIDF(N)|N=0\left.\gamma_{HWI}(N)\right|_{N\rightarrow\infty}=\left.\gamma_{HWI}^{DF}(N)\right|_{N\rightarrow\infty}=0 (52)
Proof.

The proof is given in Appendix B. ∎

Lemma 3.

When PP\rightarrow\infty, we have

RHWI¯(N)|P>RHWIDF(N)|P\left.\overline{R_{HWI}}(N)\right|_{P\rightarrow\infty}>\left.R_{HWI}^{DF}(N)\right|_{P\rightarrow\infty} (53)
γHWI(N)|P=0\left.\gamma_{HWI}(N)\right|_{P\rightarrow\infty}=0 (54)
γHWIDF(N)|P=κ(κ+Nκ+2N)(κ+Nκ)ln2\left.\gamma_{HWI}^{DF}(N)\right|_{P\rightarrow\infty}=\frac{\kappa}{(\kappa+N\kappa+2N)(\kappa+N\kappa)\ln 2} (55)
Proof.

The proof is given in Appendix C. ∎

Lemma 2 and Lemma 3 demonstrate that: 1) when NN becomes large enough, or when PP is sufficiently high, the IRS can surpass the conventional multiple-antenna DF relay in terms of the ACR performance in the presence of HWI. 2) If NN\rightarrow\infty, both the utilities of the IRS and the multiple-antenna DF relay verge on zero, hinting that adding one more reflecting element on the IRS or one more antenna on the DF relay hardly improves the ACR. 3) When PP is nearly infinite, the utility of the IRS is close to zero, while that of the multiple-antenna DF relay converges to a positive value, which indicates that adding one more antenna on the DF relay can still improve the ACR. This is because the IRS is passive and almost useless when PP\rightarrow\infty, which makes the line-of-sight (LoS) link infinitely strong, while the DF relay is active and consumes power when retransmitting the wireless signals, so that when PP\rightarrow\infty, each active antenna can always possess positive transmitting power and contribute to the data transmission enhancement. On this point, the multiple-antenna DF relay is more advantageous.

Moreover, it can be predicted that the IRS may possibly always outperform the multiple-antenna DF relay when the level of the transceiver HWI is high, because the HWI at the IRS is modelled as a phase error matrix which does not contain κt\kappa_{t} or κr\kappa_{r}, while the HWI at the DF relay involves the distortion noises which contain the two terms. The DF relay may perform worse with higher κt+κr\kappa_{t}+\kappa_{r} while the IRS may maintain the performance due to the fixed uniform distribution of the phase errors. Therefore, we will also derive the interval of κt+κr\kappa_{t}+\kappa_{r}, in which the IRS can always surpass the DF relay for all N>0N>0 in the following Lemma 4.

Lemma 4.

The IRS will always outperform the multiple-antenna DF relay for all N>0N>0, when κt+κr\kappa_{t}+\kappa_{r} satisfies

κt+κr>2σw4[P2(β+λ+μSU)22σw2P(β+λ+μSU)]1=κth\kappa_{t}+\kappa_{r}>2\sigma_{w}^{4}\left[P^{2}(\beta+\lambda+\mu_{SU})^{2}-2\sigma_{w}^{2}P(\beta+\lambda+\mu_{SU})\right]^{-1}=\kappa_{th} (56)

where β\beta and λ\lambda have been defined in (11) and (12), respectively.

Proof.

The proof is given in Appendix D. ∎

Lemma 4 demonstrates that κt+κr\kappa_{t}+\kappa_{r} determines whether the IRS can always outperform the DF relay for all N>0N>0 by a threshold κth\kappa_{th} in (56), which is mainly decided by μSI\mu_{SI}, μIU\mu_{IU}, μSU\mu_{SU}, PP and σw2\sigma_{w}^{2}. If PP\rightarrow\infty, we have κth0\kappa_{th}\rightarrow 0, which makes (56) always hold and makes the IRS perform better for all N>0N>0 and κt+κr>0\kappa_{t}+\kappa_{r}>0 in terms of the ACR. The outcome is consistent with (53) in Lemma 3.

VI Simulation Results

VI-A System Setup and Parameter Setting

This section will numerically elaborate the results of the ACR and the IRS utility with or without HWI, and compare the performances of the IRS and the DF relay. As shown in Figure 2, a two-dimensional plane in meters is established to indicate the positions of the source, the IRS and the destination,

Refer to caption
Figure 2: Communication system design in the simulations. Three dashed lines which indicate dSId_{SI}, dIUd_{IU} and dSUd_{SU} constitute a right triangle, where dSU=dSI2+dIU2d_{SU}=\sqrt{d_{SI}^{2}+d_{IU}^{2}}.

which are placed at (0,15)(0,15), (50,15)(50,15) and (50,0)(50,0). Regardless of the height, the distances between the source and the IRS (dSId_{SI}), the IRS and the destination (dIUd_{IU}) and the source and the destination (dSUd_{SU}) are dSI=50d_{SI}=50 mm, dIU=15d_{IU}=15 mm and dSU=dSI2+dIU252.2d_{SU}=\sqrt{d_{SI}^{2}+d_{IU}^{2}}\approx 52.2 mm, respectively. According to [20, 27], the other parameters are set in Table I. Based on Table I, the power attenuation coefficients of channel 𝐡IU\mathbf{h}_{IU} (or 𝐡RU\mathbf{h}_{RU}), 𝐡SI\mathbf{h}_{SI} (or 𝐡SR\mathbf{h}_{SR}) and hSUh_{SU} are derived by μIU=ζ0(d0/dIU)αIU\sqrt{\mu_{IU}}=\sqrt{\zeta_{0}(d_{0}/d_{IU})^{\alpha_{IU}}}, μSI=ζ0(d0/dSI)αSI\sqrt{\mu_{SI}}=\sqrt{\zeta_{0}(d_{0}/d_{SI})^{\alpha_{SI}}} and μSU=ζ0(d0/dSU)αSU\sqrt{\mu_{SU}}=\sqrt{\zeta_{0}(d_{0}/d_{SU})^{\alpha_{SU}}} [20].

TABLE I: Parameter configurations.
Parameters Definitions Values
Amplitude Reflection Coefficient α\alpha 11
Signal Power PP 2020 dBm
Receiver Noise Power σw2\sigma_{w}^{2} 80-80 dBm
Path Loss ζ0\zeta_{0} 20-20 dB
Reference Distance d0d_{0} 11 m
Path Loss Exponents αIU=αSI=αSU\alpha_{IU}=\alpha_{SI}=\alpha_{SU} 33
Phase Shift in 𝐡IU\mathbf{h}_{IU} φIU,i\varphi_{IU,i} Random in [0,2π][0,2\pi]
Phase Shift in 𝐡SI\mathbf{h}_{SI} φSI,i\varphi_{SI,i} Random in [0,2π][0,2\pi]
Phase Shift in hSUh_{SU} φSU\varphi_{SU} π4\frac{\pi}{4}
Proportionality Coefficients of Distortion Noises κt=κr\kappa_{t}=\kappa_{r} 0.0520.05^{2}
Oscillator Quality δ\delta 1.58×1041.58\times 10^{-4}

During the comparisons with DF relay, dSId_{SI}, dIUd_{IU} and dSUd_{SU} are also regarded as the distances between the source and the DF relay, the DF relay and the destination, and the source and the destination, respectively, which still adhere to dSU=dSI2+dIU2d_{SU}=\sqrt{d_{SI}^{2}+d_{IU}^{2}}. The proportionality coefficients can be changed for diverse observations, but still satisfy κt=κr\kappa_{t}=\kappa_{r}.

VI-B Numerical Illustrations for Theorem 1 and Lemma 1

For further discussing and validating the theoretical analysis in Section III, we carry out the simulations via the following steps:

B-Step 1: We calculate RHWI¯(N)\overline{R_{HWI}}(N) in (10) and γHWI(N)\gamma_{HWI}(N) in (13), and record the results with HWI from N=1N=1 to N=5000N=5000.

B-Step 2: We calculate R(N)R(N) in (18) and γ(N)\gamma(N) in (19), and record the results without HWI from N=1N=1 to N=5000N=5000.

B-Step 3: We calculate the rate gap δR(N)\delta_{R}(N) in (14) and the utility gap δγ(N)\delta_{\gamma}(N) in (17), and record the results from N=1N=1 to N=5000N=5000.

B-Step 4: We calculate and record the numerical results of RHWI(N)R_{HWI}(N) in (9) from N=1N=1 to N=5000N=5000. Due to the randomness of the phase errors generated by the IRS, the ACR is averaged on 1000 Monte Carlo trials every 500 points.

The average ACRs and IRS utilities as functions of NN from N=1N=1 to N=5000N=5000 are described in Figure 3. It is indicated that: 1) the experimental results fit well with the theoretical ones from N=1N=1 to N=5000N=5000, which verifies the tightness of (10). 2) The average ACR with HWI is lower and increases more slowly than that without HWI, and the rate gap widens as NN grows. This phenomenon implies that when NN grows, the HWI accumulates and begets more severe ACR degradation. 3) When NN becomes pretty large, the ACR with HWI verges on log2(1+1κt+κr)=7.6511\log_{2}\left(1+\frac{1}{\kappa_{t}+\kappa_{r}}\right)=7.6511, which testifies the correctness of (20). 4) The IRS utility with HWI is lower than that without HWI, which demonstrates that the HWI reduces the IRS utility as well. Besides, both the IRS utility and the utility gap descend as NN grows, which reveals that the influence of the HWI on the IRS utility becomes slighter when NN is larger.

Refer to caption
(a)
Refer to caption
(b)
Figure 3: Average ACRs and IRS utilities as functions of NN with or without HWI. (a) Average ACRs with respect to NN, the curves marked with ”\square”, ”\bigcirc”, ”\bigtriangledown” and ”*”, represent the results obtained in B-Step 1 to B-Step 4, respectively. (b) IRS utilities with respect to NN, the curves marked with ”\square”, ”\bigcirc” and ”\bigtriangledown”, represent the results obtained in B-Step 1 to B-Step 3, respectively.

  

VI-C Phase Shift Optimization

For giving insights into the phase shift optimization approach in Section IV, we carry out the simulations through the following steps:

C-Step 1: We solve (P6) by adopting CVX Toolbox with SDPT3 Solver, and obtain the maximum average SNR from the solution of the OBF in (38a). Based on this solution, we calculate and record the ACRs at N=1,13,25,37N=1,13,25,37.

C-Step 2: We solve (P6) and obtain the optimized matrix 𝐘\mathbf{Y} and variable μ~\widetilde{\mu}. Next, we extract the 𝜽T\bm{\theta}^{T} in the (N+1)(N+1)-th row of 𝐗=μ~1𝐘\mathbf{X}=\widetilde{\mu}^{-1}\mathbf{Y}. Then, we utilize 𝜽T\bm{\theta}^{T} to reconstruct 𝐗\mathbf{X} according to (28) and 𝐘\mathbf{Y} according to 𝐘=μ~𝐗\mathbf{Y}=\widetilde{\mu}\mathbf{X}, and denote the reconstructed 𝐗\mathbf{X} and 𝐘\mathbf{Y} by 𝐗r\mathbf{X}_{r} and 𝐘r\mathbf{Y}_{r}, respectively. Finally, we substitute 𝐘r\mathbf{Y}_{r} into the OBF in (38a) and obtain the average SNR, based on which we calculate and record the ACRs at N=1,13,25,37N=1,13,25,37.

C-Step 3: Based on the extracted 𝜽T\bm{\theta}^{T}, we obtain the optimized IRS phase shift matrix 𝚽\mathbf{\Phi} according to 𝚽=diag(𝜽T)\mathbf{\Phi}=diag(\bm{\theta}^{T}). Then, we substitute 𝚽\mathbf{\Phi} into (23) and obtain the ACRs with HWI, which are averaged on 1000 Monte Carlo trials at N=1,13,25,37N=1,13,25,37.

Refer to caption
Figure 4: Average ACRs as functions of NN with HWI. The curves marked with ”\Diamond”, ”+” and ”\bigcirc” represent the results obtained in C-Step 1 to C-Step 3, respectively. The curves marked with ”\square” and ”*” are copied from Figure 3 (a) for comparisons.

The average ACRs as functions of NN with HWI are depicted in Figure 4. Results in Figure 4 show that: 1) the curves obtained in C-Step 1 and C-Step 2 coincide, indicating that 𝐘r=𝐘\mathbf{Y}_{r}=\mathbf{Y}. Moreover, we calculate the rank of 𝐘r\mathbf{Y}_{r} and obtain rank(𝐘r)=1rank(\mathbf{Y}_{r})=1. Because 𝐘r\mathbf{Y}_{r} is constructed by 𝜽T\bm{\theta}^{T} in the (N+1)(N+1)-th row of 𝐗=μ~1𝐘\mathbf{X}=\widetilde{\mu}^{-1}\mathbf{Y} in the solution, 𝜽T\bm{\theta}^{T} is testified to be the optimal IRS phase shift vector. 2) The curves obtained in C-Step 1 and C-Step 3 coincide, confirming that the mathematical derivations for 𝔼𝚯E[𝚵]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right] in (37) are correct. 3) The average ACRs with the optimized IRS phase shifts exceed the average ACRs with θi=(φIU,i+φSI,i)\theta_{i}=-\left(\varphi_{IU,i}+\varphi_{SI,i}\right), demonstrating that θi=(φIU,i+φSI,i)\theta_{i}=-\left(\varphi_{IU,i}+\varphi_{SI,i}\right) is not the optimal phase shift as it does not take hSUh_{SU} into account.

  

VI-D Discussions on Channel Estimation Errors and Residual Phase Noises

Because most IRS-aided communication systems suffer from channel estimation errors, and the optimized IRS phase shifts may generally be affected by residual phase noises, as narrated at the end of Section IV, we will probe into the influence of the two factors on the optimization performance. The channel estimation errors are set to be additive complex variables according to Eq. (2) in [40], which follow the zero-mean complex Gaussian distribution with the variance of σw2\sigma_{w}^{2}. More detailed information about the CSI uncertainty models and simulation parameters can be found in [40]. The residual phase noises θpi\theta_{pi} in 𝜽p\bm{\theta}_{p}, for i=1,2,,Ni=1,2,...,N, are also set to be uniformly distributed on [π/2,π/2][-\pi/2,\pi/2].

Refer to caption
Figure 5: Influences of the channel estimation errors and residual phase noises on the optimization results. The ACRs are derived by substituting 𝚽=diag(𝜽T)\mathbf{\Phi}=diag(\bm{\theta}^{T}) or 𝚽=diag(𝜽T𝜽pT)\mathbf{\Phi}=diag(\bm{\theta}^{T}\odot\bm{\theta}_{p}^{T}) into (23) and are averaged on 1000 Monte Carlo trials. ”Imperfect CSI” means that there are channel estimation errors, while ”Perfect CSI” represents the opposite.

In the simulations, for investigating the average ACR with channel estimation errors, we first adopt the CSI with errors to construct 𝔼𝚯E[𝚵]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\mathbf{\Xi}\right] and solve (P6), and then substitute 𝚽=diag(𝜽T)\mathbf{\Phi}=diag(\bm{\theta}^{T}) into (23) which contains the actual CSI. For investigating the average ACR with residual phase noises, we first solve (P6) and exert the influence of 𝜽p\bm{\theta}_{p} on 𝜽T\bm{\theta}^{T} by constructing 𝜽T𝜽pT\bm{\theta}^{T}\odot\bm{\theta}_{p}^{T}, and then substitute 𝚽=diag(𝜽T𝜽pT)\mathbf{\Phi}=diag(\bm{\theta}^{T}\odot\bm{\theta}_{p}^{T}) into (23). Figure 5 depicts the influences of the channel estimation errors and residual phase noises on the optimization results. It is demonstrated that: 1) both the channel estimation errors and the residual phase noises reduce the average ACR and degrade the optimization performance. 2) The residual phase noises impose more serious negative impact on the performance than the channel estimation errors, manifesting that the inherent hardware imperfection, synchronization offset and estimation accuracy limit in the real world, are key potential factors that affect the optimization performance.

  

VI-E Comparisons with DF Relay

In order to validate the theoretical analysis in Section V, we will numerically compare the ACRs and the utilities for the IRS-aided and the conventional multiple-antenna DF relay assisted wireless communication systems in the presence of HWI. Following Section V, we will compare the performances by varying NN and PP.

  

1) Comparisons by varying NN:

Refer to caption
(a)
Refer to caption
(b)
Figure 6: Comparisons with DF relay by varying NN. (a) Average ACRs as functions of NN, with P=20P=20 dBm and κt=κr=0.052,0.072,0.092\kappa_{t}=\kappa_{r}=0.05^{2},0.07^{2},0.09^{2}. (b) Utilities as functions of NN, with P=20P=20 dBm and κt=κr=0.052,0.072,0.092\kappa_{t}=\kappa_{r}=0.05^{2},0.07^{2},0.09^{2}.

First, considering the transmitting power to be fixed (P=20P=20 dBm), we compare the average ACR in (10) with that in (47) by varying NN, and observe the simulation results at κt=κr=0.052,0.072,0.092\kappa_{t}=\kappa_{r}=0.05^{2},0.07^{2},0.09^{2}. Figure 6 (a) displays the average ACRs of the IRS-aided and the DF relay assisted wireless communication systems in relation to NN, from N=1N=1 to N=5000N=5000. It is indicated that: 1) the ACRs decrease when κt\kappa_{t} and κr\kappa_{r} grow, which verifies that more severe HWI is concomitant with more serious ACR reduction. 2) Although it might not be realistic for the IRS and the DF relay to be equipped with such a large number (e.g. 5000) of reflecting elements and antennas in practical implementations, the result testifies (51) in Lemma 2 and confirms the possibility that when NN is extremely large, the IRS is capable of outperforming the DF relay in terms of the ACR performance. It is worth noting that when κt=κr=0.052,0.072,0.092\kappa_{t}=\kappa_{r}=0.05^{2},0.07^{2},0.09^{2}, the IRS always performs better for all N[1,5000]N\in[1,5000]. This is because with the system parameters set in Section VI-A, the κth\kappa_{th} in (56) in Lemma 4 is computed as κth=4.0451×106\kappa_{th}=4.0451\times 10^{-6}, which is smaller than κ=κt+κr=0.052+0.052, 0.072+0.072, 0.092+0.092\kappa=\kappa_{t}+\kappa_{r}=0.05^{2}+0.05^{2},\ 0.07^{2}+0.07^{2},\ 0.09^{2}+0.09^{2}. 3) As NN grows, the ACRs do not continuously increase appreciably. Instead, the ACRs of the IRS-aided communication system are approximately limited by 7.6511 bps/Hz at κt=κr=0.052\kappa_{t}=\kappa_{r}=0.05^{2}, 6.6871 bps/Hz at κt=κr=0.072\kappa_{t}=\kappa_{r}=0.07^{2} and 5.9710 bps/Hz at κt=κr=0.092\kappa_{t}=\kappa_{r}=0.09^{2}; while those of the DF relay assisted communication system are approximately limited by 4.3237 bps/Hz at κt=κr=0.052\kappa_{t}=\kappa_{r}=0.05^{2}, 3.8400 bps/Hz at κt=κr=0.072\kappa_{t}=\kappa_{r}=0.07^{2} and 3.4798 bps/Hz at κt=κr=0.092\kappa_{t}=\kappa_{r}=0.09^{2}. The values are consistent with what are computed from RHWI¯(N)|N=log2(1+1κt+κr)\left.\overline{R_{HWI}}\left(N\right)\right|_{N\rightarrow\infty}=\log_{2}\left(1+\frac{1}{\kappa_{t}+\kappa_{r}}\right) and RHWIDF(N)|N=12log2(1+2κ)R_{HWI}^{DF}(N)|_{N\rightarrow\infty}=\frac{1}{2}\log_{2}\left(1+\frac{2}{\kappa}\right). 4) The ACRs of the DF relay assisted communication system increase rapidly when N<100N<100, illustrating that the ACR performance of the DF relay can be significantly improved by increasing the quantity of the antennas when NN is small.

Then, we compare the utility in (13) with that in (50) by varying NN. Figure 6 (b) describes the utilities of the IRS and the DF relay in relation to NN. The observation interval is shrunk (N[1,16]N\in[1,16]), for clearly viewing the details on the utility reduction of the DF relay. The results show that: 1) when κt\kappa_{t} and κr\kappa_{r} grow, the utilities decrease, which confirms that more severe HWI is concomitant with more serious utility degradation. 2) The IRS utility is lower than the DF-relay utility when NN is small, and both of them decrease to zero as NN grows. This is consistent with what is given in (52) in Lemma 2.

  

2) Comparisons by varying PP:

Refer to caption
(a)
Refer to caption
(b)
Figure 7: Comparisons with DF relay by varying PP. (a) Average ACRs as functions of PP, with N=256N=256 and κt=κr=0.052,0.072,0.092\kappa_{t}=\kappa_{r}=0.05^{2},0.07^{2},0.09^{2}. (b) Utilities as functions of PP, with N=256N=256 and κt=κr=0.052,0.072,0.092\kappa_{t}=\kappa_{r}=0.05^{2},0.07^{2},0.09^{2}.

First, considering the number of the reflecting elements or the DF-relay antennas to be fixed (N=256N=256), we compare the average ACR in (10) with that in (47) by varying PP, and observe the numerical results at κt=κr=0.052,0.072,0.092\kappa_{t}=\kappa_{r}=0.05^{2},0.07^{2},0.09^{2}. Figure 7 (a) plots the average ACRs of the IRS-aided and the DF relay assisted wireless communication systems with respect to PP, from P=1P=1 dBm to P=50P=50 dBm. It is indicated that: 1) when P<2P<2 dBm and N=256N=256, the IRS performs worse than the DF relay if κt=κr=0.052,0.072\kappa_{t}=\kappa_{r}=0.05^{2},0.07^{2}, but better if κt=κr=0.092\kappa_{t}=\kappa_{r}=0.09^{2}. This phenomenon reveals that when PP is low, the transceiver HWI influences the performance of the DF relay more seriously than the performance of the IRS. 2) The ACRs of the IRS-aided communication system increase faster as PP rises, and exceed the ACRs of the DF relay assisted communication system when P>5P>5 dBm. 3) Both the ACRs of the IRS-aided and the DF relay assisted communication systems are bounded when PP is high. Specifically, the ACRs of the IRS-aided communication system are approximately bounded by 7.6511 bps/Hz at κt=κr=0.052\kappa_{t}=\kappa_{r}=0.05^{2}, 6.6871 bps/Hz at κt=κr=0.072\kappa_{t}=\kappa_{r}=0.07^{2} and 5.9710 bps/Hz at κt=κr=0.092\kappa_{t}=\kappa_{r}=0.09^{2}; while the ACRs of the DF relay assisted communication system are approximately bounded by 4.3209 bps/Hz at κt=κr=0.052\kappa_{t}=\kappa_{r}=0.05^{2}, 3.8372 bps/Hz at κt=κr=0.072\kappa_{t}=\kappa_{r}=0.07^{2} and 3.4770 bps/Hz at κt=κr=0.092\kappa_{t}=\kappa_{r}=0.09^{2}. The values coincide with what can be derived from RHWI¯(N)|P=log2(1+1κ)\overline{R_{HWI}}(N)|_{P\rightarrow\infty}=\log_{2}\left(1+\frac{1}{\kappa}\right) and RHWIDF(N)|P=12log2(1+2Nκ+κN)R_{HWI}^{DF}(N)|_{P\rightarrow\infty}=\frac{1}{2}\log_{2}\left(1+\frac{2N}{\kappa+\kappa N}\right).

Then, we compare the utility in (13) with that in (50) by varying PP. Figure 7 (b) depicts the utilities of the IRS and the DF relay with respect to PP. The results demonstrate that: 1) when PP is relatively low, the utilities of the IRS outstrip those of the DF relay, but both of them descend as PP grows. 2) The utilities of the IRS decrease to zero, while those of the DF relay converge to certain positive values (around 1.09×1051.09\times 10^{-5}), which are consistent with what are calculated from γHWIDF(N)|P=κ(κ+Nκ+2N)(κ+Nκ)ln2\left.\gamma_{HWI}^{DF}(N)\right|_{P\rightarrow\infty}=\frac{\kappa}{(\kappa+N\kappa+2N)(\kappa+N\kappa)\ln 2}. These results validate (54) and (55) in Lemma 3, and reveal that in terms of the utility, although the IRS is preferable to the DF relay at a low system power, the DF relay becomes more advantageous if PP is significantly high.

VII Conclusion and Future Works

In this article, for the purpose of evaluating the performance of the IRS in consideration of the hardware non-ideality at both the IRS and the signal transceivers, we first analyse the average ACR and the IRS utility for the IRS-aided SISO communication system, then optimize the IRS phase shifts by converting the original non-convex problem into a SDP problem, subsequently investigate the impact of the channel estimation errors and the residual phase noises on the optimization performance, and finally compare the IRS with the conventional multiple-antenna DF relay in terms of the ACR and the utility in the presence of HWI. The results illustrate that: 1) as the number of the reflecting units grows, the average ACR of the IRS-aided communication system increases, while the utility of the IRS decreases. 2) The HWI degrades both the ACR and the utility, and it causes more severe ACR reduction when more reflecting elements are equipped. 3) If the number of the reflecting units is large enough or the transmitting power is sufficiently high, the IRS can surpass the conventional DF relay in terms of the ACR, although the DF relay is relatively more advantageous in terms of the utility. Consequently, the IRS is proved to be still an effective facility for data transmission enhancement in the future wireless communication networks with imperfect hardware in the real world.

As in most actual circumstances, the BS is generally equipped with multiple antennas and is responsible for serving multiple users, it is meaningful to dissect the system performance in the IRS-aided multiple-user MISO communication scenario in the presence of HWI. In view of the complex-matrix form of the BS-IRS channel, deriving the closed-form average ACR as a function of the number of the reflecting elements is a challenging task and deserves more effort. In addition, forasmuch as the typical amplify-and-forward (AF) relay is also widely utilized to assist the wireless communication, the insightful theoretical comparison with this conventional approach in the presence of HWI is challenging but worth to be performed in depth as well in the future.

Appendix A Proof of Theorem 1

In Appendix A, we will mathematically prove Theorem 1 in Section III.

First, based on (9), the exact average ACR can be derived from

RHWI¯(N)=𝔼𝚯E[RHWI(N)]=𝔼𝚯E{log2{1+P|ϕ(t)(α𝐠IUT𝚯E𝐠SI+hSU)|2P(κt+κr)|ϕ(t)(α𝐠IUT𝚯E𝐠SI+hSU)|2+σw2}}\begin{split}\overline{R_{HWI}}\left(N\right)=&\mathbb{E}_{\mathbf{\Theta}_{E}}\left[R_{HWI}\left(N\right)\right]\\ =&\mathbb{E}_{\mathbf{\Theta}_{E}}\left\{\log_{2}\left\{1+\frac{P\left|\phi(t)\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\right|^{2}}{P(\kappa_{t}+\kappa_{r})\left|\phi(t)\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\right|^{2}+\sigma_{w}^{2}}\right\}\right\}\end{split} (57)

However, as illustrated in [33], it is difficult, if not impossible, to obtain the exact closed-form expression for 𝔼𝚯E[RHWI(N)]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[R_{HWI}\left(N\right)\right]. Therefore, inspired by [33, 41, 42, 43, 44], we will also find an approximation to 𝔼𝚯E[RHWI(N)]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[R_{HWI}\left(N\right)\right].

Fortunately, according to Eq. (35) in [45], which is given by

𝔼{log2(1+xy)}log2(1+𝔼{x}𝔼{y})\mathbb{E}\left\{\log_{2}\left(1+\frac{x}{y}\right)\right\}\approx\log_{2}\left(1+\frac{\mathbb{E}\{x\}}{\mathbb{E}\{y\}}\right) (58)

a simpler closed-form expression for the average ACR can be achieved by the approximation in (58). Hence, based on (58), the RHWI¯(N)\overline{R_{HWI}}\left(N\right) in (57) can be approximated by

RHWI¯(N)log2{1+P𝔼𝚯E[|ϕ(t)(α𝐠IUT𝚯E𝐠SI+hSU)|2]P(κt+κr)𝔼𝚯E[|ϕ(t)(α𝐠IUT𝚯E𝐠SI+hSU)|2]+σw2}=log2(1+P𝒬P(κt+κr)𝒬+σw2)\begin{split}\overline{R_{HWI}}\left(N\right)\approx&\log_{2}\left\{1+\frac{P\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\left|\phi(t)\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\right|^{2}\right]}{P(\kappa_{t}+\kappa_{r})\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\left|\phi(t)\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\right|^{2}\right]+\sigma_{w}^{2}}\right\}\\ =&\log_{2}\left(1+\frac{P\mathcal{Q}}{P(\kappa_{t}+\kappa_{r})\mathcal{Q}+\sigma_{w}^{2}}\right)\end{split} (59)

where 𝒬=𝔼𝚯E[|ϕ(t)(α𝐠IUT𝚯E𝐠SI+hSU)|2]\mathcal{Q}=\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\left|\phi(t)\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\right|^{2}\right].

From (59), the problem of deriving the closed-form expression for 𝔼𝚯E[RHWI(N)]\mathbb{E}_{\mathbf{\Theta}_{E}}\left[R_{HWI}\left(N\right)\right] is converted into that for 𝒬\mathcal{Q}, which is expanded into

𝒬=𝔼𝚯E{[ϕ(t)(α𝐠IUT𝚯E𝐠SI+hSU)][ϕ(t)(α𝐠IUT𝚯E𝐠SI+hSU)]}=𝔼𝚯E[(α𝐠IUT𝚯E𝐠SI+hSU)(α𝐠IUT𝚯E𝐠SI+hSU)]\begin{split}\mathcal{Q}=&\mathbb{E}_{\mathbf{\Theta}_{E}}\left\{\left[\phi(t)\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\right]^{*}\left[\phi(t)\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\right]\right\}\\ =&\mathbb{E}_{\mathbf{\Theta}_{E}}\left[\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)^{*}\left(\alpha\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}\mathbf{g}_{SI}+h_{SU}\right)\right]\end{split} (60)

Subsequently, let 𝐆IU\mathbf{G}_{IU} and 𝐯E\mathbf{v}_{E} be defined by 𝐆IU=diag(𝐠IU)=μIU𝐈N\mathbf{G}_{IU}=diag\left(\mathbf{g}_{IU}\right)=\sqrt{\mu_{IU}}\mathbf{I}_{N} and 𝐯E=(ejθE1,ejθE2,,ejθEN)T\mathbf{v}_{E}=\left(e^{j\theta_{E1}},e^{j\theta_{E2}},\ldots,e^{j\theta_{EN}}\right)^{T}. Because we have 𝐯ET𝐆IU=𝐠IUT𝚯E\mathbf{v}_{E}^{T}\mathbf{G}_{IU}=\mathbf{g}_{IU}^{T}\mathbf{\Theta}_{E}, 𝐆IU=𝐆IU\mathbf{G}_{IU}^{*}=\mathbf{G}_{IU} and 𝐠SI=𝐠SI\mathbf{g}_{SI}^{*}=\mathbf{g}_{SI}, from (60) we obtain

𝒬=𝔼𝚯E[α2𝐠SIT𝐆IUT𝐯E𝐯ET𝐆IU𝐠SI+α𝐠SIT𝐆IUT𝐯EhSU+αhSU𝐯ET𝐆IU𝐠SI+hSU22]=α2μIUμSI𝔼θEi[tr(𝐯ET𝚪N𝐯E)]+αμIUμSIμSU𝔼θEi{i=1N[ej(φSU+θEi)+ej(φSU+θEi)]}+hSU22\begin{split}\mathcal{Q}&=\mathbb{E}_{\mathbf{\Theta}_{E}}\left[{\alpha^{2}\mathbf{g}}_{SI}^{T}\mathbf{G}_{IU}^{T}\mathbf{v}_{E}^{*}\mathbf{v}_{E}^{T}\mathbf{G}_{IU}\mathbf{g}_{SI}+\alpha\mathbf{g}_{SI}^{T}\mathbf{G}_{IU}^{T}\mathbf{v}_{E}^{*}h_{SU}+\alpha h_{SU}^{*}\mathbf{v}_{E}^{T}\mathbf{G}_{IU}\mathbf{g}_{SI}+||h_{SU}||_{2}^{2}\right]\\ &=\alpha^{2}\mu_{IU}\mu_{SI}\mathbb{E}_{\theta_{Ei}}\left[tr\left(\mathbf{v}_{E}^{T}\mathbf{\Gamma}_{N}\mathbf{v}_{E}^{*}\right)\right]+\alpha\sqrt{\mu_{IU}\mu_{SI}\mu_{SU}}\mathbb{E}_{\theta_{Ei}}\left\{\sum_{i=1}^{N}\left[e^{j{{(\varphi}_{SU}+\theta}_{Ei})}+e^{-j{{(\varphi}_{SU}+\theta}_{Ei})}\right]\right\}+||h_{SU}||_{2}^{2}\end{split} (61)

where i=1,2,,Ni=1,2,...,N. In (61), we can expand tr(𝐯ET𝚪N𝐯E)tr\left(\mathbf{v}_{E}^{T}\mathbf{\Gamma}_{N}\mathbf{v}_{E}^{*}\right) into

tr(𝐯ET𝚪N𝐯E)=N+i1Nej(θE1θEi)+i2Nej(θE2θEi)++iN1Nej(θE(N1)θEi)+iNNej(θENθEi)=N+2i=2Ncos(θE1θEi)+2i=3Ncos(θE2θEi)++2i=NNcos(θE(N1)θEi)=N+𝟏𝐌𝟏T\begin{split}tr\left(\mathbf{v}_{E}^{T}\mathbf{\Gamma}_{N}\mathbf{v}_{E}^{*}\right)&=N+\sum_{i\neq 1}^{N}e^{j{{(\theta}_{E1}-\theta}_{Ei})}+\sum_{i\neq 2}^{N}e^{j{{(\theta}_{E2}-\theta}_{Ei})}+\ldots+\!\!\sum_{i\neq N-1}^{N}e^{j{{(\theta}_{E\left(N-1\right)}-\theta}_{Ei})}+\sum_{i\neq N}^{N}e^{j{{(\theta}_{EN}-\theta}_{Ei})}\\ &=N+2\sum_{i=2}^{N}{cos{{(\theta}_{E1}-\theta}_{Ei})}+2\sum_{i=3}^{N}{cos{{(\theta}_{E2}-\theta}_{Ei})}+\ldots+2\sum_{i=N}^{N}{cos{{(\theta}_{E\left(N-1\right)}-\theta}_{Ei})}\\ &=N+{\mathbf{1M1}}^{T}\end{split} (62)

where the matrix 𝐌\mathbf{M} is expressed as

𝐌=(2cos(θE1θE2)2cos(θE2θE3)2cos(θE(N1)θEN)2cos(θE1θE3)2cos(θE2θE4) 02cos(θE1θE(N1))2cos(θE1θEN)2cos(θE2θEN)00 00 0)\mathbf{M}=\left(\begin{matrix}2\cos{\left({\theta_{E1}-\theta}_{E2}\right)}&2\cos{\left({\theta_{E2}-\theta}_{E3}\right)}&\begin{matrix}\cdots\ &2\cos{\left({\theta_{E\left(N-1\right)}-\theta}_{EN}\right)}\\ \end{matrix}\\ 2\cos{\left({\theta_{E1}-\theta}_{E3}\right)}&2\cos{\left({\theta_{E2}-\theta}_{E4}\right)}&\begin{matrix}\cdots\ \ \ \ \ \ &\ \ \ \ 0\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \\ \end{matrix}\\ \begin{matrix}\vdots\\ \begin{matrix}2\cos{\left({\theta_{E1}-\theta}_{E\left(N-1\right)}\right)}\\ 2\cos{\left({\theta_{E1}-\theta}_{EN}\right)}\\ \end{matrix}\\ \end{matrix}&\begin{matrix}\vdots\\ \begin{matrix}2\cos{\left({\theta_{E2}-\theta}_{EN}\right)}\\ 0\\ \end{matrix}\\ \end{matrix}&\begin{matrix}\begin{matrix}\iddots\ \ \ \ \ \ \ \ \ \ &\ \vdots\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \\ \end{matrix}\\ \begin{matrix}0&\ \ \ \ \ \ \ \ \ \ \ 0\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \\ \end{matrix}\\ \begin{matrix}0&\ \ \ \ \ \ \ \ \ \ \ 0\ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \ \\ \end{matrix}\\ \end{matrix}\\ \end{matrix}\right) (63)

We can also utilize Euler formula to expand i=1N[ej(φSU+θEi)+ej(φSU+θEi)]\sum_{i=1}^{N}\left[e^{j{{(\varphi}_{SU}+\theta}_{Ei})}+e^{-j{{(\varphi}_{SU}+\theta}_{Ei})}\right] and then obtain i=1N[ej(φSU+θEi)+ej(φSU+θEi)]=2i=1Ncos(φSU+θEi)\sum_{i=1}^{N}\left[e^{j{{(\varphi}_{SU}+\theta}_{Ei})}+e^{-j{{(\varphi}_{SU}+\theta}_{Ei})}\right]=2\sum_{i=1}^{N}\cos{\left({\varphi_{SU}+\theta}_{Ei}\right)}.

As θEi\theta_{Ei}, for i=1,2,,Ni=1,2,...,N, are random variables which are uniformly distributed on [π/2,π/2]\left[-\pi/2,\pi/2\right], we should calculate the expectations of 2i=1Ncos(φSU+θEi)2\sum_{i=1}^{N}\cos{\left({\varphi_{SU}+\theta}_{Ei}\right)} and tr(𝐯ET𝚪N𝐯E)tr\left(\mathbf{v}_{E}^{T}\mathbf{\Gamma}_{N}\mathbf{v}_{E}^{*}\right) in order to obtain a statistical average ACR. First, we calculate 𝔼θEi[2i=1Ncos(φSU+θEi)]\mathbb{E}_{\theta_{Ei}}\left[2\sum_{i=1}^{N}\cos{\left({\varphi_{SU}+\theta}_{Ei}\right)}\right] and have

𝔼θEi[2i=1Ncos(φSU+θEi)]=2𝔼θEi[i=1NcosφSUcosθEii=1NsinφSUsinθEi]=2NcosφSUπ2π2f(θEi)cosθEidθEi2NsinφSUπ2π2f(θEi)sinθEidθEi=4πNcosφSU\begin{split}\mathbb{E}_{\theta_{Ei}}\!\!\left[2\sum_{i=1}^{N}\cos{\left({\varphi_{SU}+\theta}_{Ei}\right)}\right]&=2\mathbb{E}_{\theta_{Ei}}\!\!\left[\sum_{i=1}^{N}{\cos{\varphi_{SU}}\cos{\theta_{Ei}}}-\sum_{i=1}^{N}{\sin{\varphi_{SU}}\sin{\theta_{Ei}}}\right]\\ &=2N\!\cos{\varphi_{SU}}\!\!\int_{-\frac{\pi}{2}}^{\frac{\pi}{2}}\!\!\!{f\left(\theta_{Ei}\right)\cos{\theta_{Ei}{d\theta}_{Ei}}}-2N\sin{\varphi_{SU}}\int_{-\frac{\pi}{2}}^{\frac{\pi}{2}}{f\left(\theta_{Ei}\right)\sin{\theta_{Ei}{d\theta}_{Ei}}}\\ &=\frac{4}{\pi}N\cos{\varphi_{SU}}\end{split} (64)

where f(θEi)=1/πf\left(\theta_{Ei}\right)=1/\pi is the probability density function of variable θEi\theta_{Ei}.

Subsequently, we calculate 𝔼θEi[tr(𝐯ET𝚪N𝐯E)]=N+𝔼θEi[𝟏𝐌𝟏T]\mathbb{E}_{\theta_{Ei}}\left[tr\left(\mathbf{v}_{E}^{T}\mathbf{\Gamma}_{N}\mathbf{v}_{E}^{*}\right)\right]=N+\mathbb{E}_{\theta_{Ei}}\left[{\mathbf{1M1}}^{T}\right]. It is notable that the elements in 𝐌\mathbf{M} are either 0, or 2cos(θEiθEj)2\cos(\theta_{Ei}-\theta_{Ej}) for i<ji<j. Therefore, let δθ\delta_{\theta} be defined by δθ=θEiθEj\delta_{\theta}=\theta_{Ei}-\theta_{Ej}. Because θEi\theta_{Ei} obeys uniform distribution on [π/2,π/2]\left[-\pi/2,\pi/2\right], δθ\delta_{\theta} obeys triangular distribution on [π,π][-\pi,\pi] whose probability density function is expressed as

f(δθ)={1π2δθ+1π,δθ[π,0]1π2δθ+1π,δθ[0,π]f\left(\delta_{\theta}\right)=\left\{\begin{matrix}\frac{1}{\pi^{2}}\delta_{\theta}+\frac{1}{\pi},\ \delta_{\theta}\in\left[-\pi,0\right]\\ -\frac{1}{\pi^{2}}\delta_{\theta}+\frac{1}{\pi},\ \delta_{\theta}\in\left[0,\pi\right]\\ \end{matrix}\right. (65)

Thus, we have

N+𝔼θEi[𝟏𝐌𝟏T]=N+𝔼θEi[2i<jNcos(θEiθEj)]=N+N(N1)[π0(1π2δθ+1π)cos(δθ)𝑑δθ+0π(1π2δθ+1π)cos(δθ)𝑑δθ]=N+1π2N(N1)[π0δθcos(δθ)𝑑δθ0πδθcos(δθ)𝑑δθ]=N+4π2N(N1)=4N2π2+(14π2)N\begin{split}N+\mathbb{E}_{\theta_{Ei}}\left[{\mathbf{1M1}}^{T}\right]&=N+\mathbb{E}_{\theta_{Ei}}\left[2\sum_{i<j}^{N}\cos{\left({\theta_{Ei}-\theta}_{Ej}\right)}\right]\\ &=N+N\left(N-1\right)\left[\int_{-\pi}^{0}{\left(\frac{1}{\pi^{2}}\delta_{\theta}+\frac{1}{\pi}\right)\cos{\left(\delta_{\theta}\right)}d\delta_{\theta}}+\int_{0}^{\pi}{\left(-\frac{1}{\pi^{2}}\delta_{\theta}+\frac{1}{\pi}\right)\cos{\left(\delta_{\theta}\right)}d\delta_{\theta}}\right]\\ &=N+\frac{1}{\pi^{2}}N(N-1)\left[\int_{-\pi}^{0}\delta_{\theta}\cos{(\delta_{\theta})}d\delta_{\theta}-\int_{0}^{\pi}\delta_{\theta}\cos{(\delta_{\theta})}d\delta_{\theta}\right]\\ &=N+\frac{4}{\pi^{2}}N(N-1)=\frac{4N^{2}}{\pi^{2}}+\left(1-\frac{4}{\pi^{2}}\right)N\end{split} (66)

By substituting (64) and (66) into (61), and substituting (61) into (59), we finally prove (10). Then, by calculating γHWI(N)=RHWI¯(N)N\gamma_{HWI}(N)=\frac{\partial\overline{R_{HWI}}\left(N\right)}{\partial N}, we finally prove (13).

Appendix B Proof of Lemma 2

In Appendix B, we will prove Lemma 2 in Section V. On the assumption that κt=κr=12κ\kappa_{t}=\kappa_{r}=\frac{1}{2}\kappa and P1=P2=PP_{1}=P_{2}=P, when NN\rightarrow\infty, from (48) and (49), we have

𝔄(N)|N=log2(1+2κ)\mathfrak{A}(N)|_{N\rightarrow\infty}=\log_{2}\left(1+\frac{2}{\kappa}\right) (67)
𝔅(N)|N=log2(1+1κ+σw2PμSU+2κ)\mathfrak{B}(N)|_{N\rightarrow\infty}=\log_{2}\left(1+\frac{1}{\kappa+\frac{\sigma_{w}^{2}}{P\mu_{SU}}}+\frac{2}{\kappa}\right) (68)

Because 1+2κ<1+1κ+σw2PμSU+2κ1+\frac{2}{\kappa}<1+\frac{1}{\kappa+\frac{\sigma_{w}^{2}}{P\mu_{SU}}}+\frac{2}{\kappa}, according to (47), we have

RHWIDF(N)|N=12𝔄(N)|N=12log2(1+2κ)R_{HWI}^{DF}(N)|_{N\rightarrow\infty}=\frac{1}{2}\mathfrak{A}(N)|_{N\rightarrow\infty}=\frac{1}{2}\log_{2}\left(1+\frac{2}{\kappa}\right) (69)

Given RHWI¯(N)|N\overline{R_{HWI}}(N)|_{N\rightarrow\infty} in (20), we calculate RHWI¯(N)|NRHWIDF(N)|N\overline{R_{HWI}}(N)|_{N\rightarrow\infty}-R_{HWI}^{DF}(N)|_{N\rightarrow\infty} and obtain

RHWI¯(N)|NRHWIDF(N)|N=12log2(1+1κ2+2κ)>0\overline{R_{HWI}}(N)|_{N\rightarrow\infty}-R_{HWI}^{DF}(N)|_{N\rightarrow\infty}=\frac{1}{2}\log_{2}\left(1+\frac{1}{\kappa^{2}+2\kappa}\right)>0 (70)

from which we prove (51). Then, based on (13) and (50), we consider NN\rightarrow\infty and prove (52).

Appendix C Proof of Lemma 3

In Appendix C, we will prove Lemma 3 in Section V. Similar to the proof of Lemma 2 in Appendix B, when PP\rightarrow\infty, we have

𝔄(N)|P=log2(1+2Nκ+κN)\mathfrak{A}(N)|_{P\rightarrow\infty}=\log_{2}\left(1+\frac{2N}{\kappa+\kappa N}\right) (71)
𝔅(N)|P=log2(1+1κ+2Nκ+κN)\mathfrak{B}(N)|_{P\rightarrow\infty}=\log_{2}\left(1+\frac{1}{\kappa}+\frac{2N}{\kappa+\kappa N}\right) (72)

Because 1+2Nκ+κN<1+1κ+2Nκ+κN1+\frac{2N}{\kappa+\kappa N}<1+\frac{1}{\kappa}+\frac{2N}{\kappa+\kappa N}, according to (47), we have

RHWIDF(N)|P=12𝔄(N)|P=12log2(1+2Nκ+κN)R_{HWI}^{DF}(N)|_{P\rightarrow\infty}=\frac{1}{2}\mathfrak{A}(N)|_{P\rightarrow\infty}=\frac{1}{2}\log_{2}\left(1+\frac{2N}{\kappa+\kappa N}\right) (73)

Based on (10), we have

RHWI¯(N)|P=log2(1+1κ)\overline{R_{HWI}}(N)|_{P\rightarrow\infty}=\log_{2}\left(1+\frac{1}{\kappa}\right) (74)

Hence, we calculate RHWI¯(N)|PRHWIDF(N)|P\overline{R_{HWI}}(N)|_{P\rightarrow\infty}-R_{HWI}^{DF}(N)|_{P\rightarrow\infty} and obtain

RHWI¯(N)|PRHWIDF(N)|P=12log2{1+2κ+N+1(N+1)κ2+2Nκ}>0,N>0\overline{R_{HWI}}(N)|_{P\rightarrow\infty}-R_{HWI}^{DF}(N)|_{P\rightarrow\infty}=\frac{1}{2}\log_{2}\left\{1+\frac{2\kappa+N+1}{(N+1)\kappa^{2}+2N\kappa}\right\}>0,\ \ \forall N>0 (75)

from which we prove (53). Then, on the basis of (13) and (50), we consider PP\rightarrow\infty and prove (54) and (55).

Appendix D Proof of Lemma 4

In Appendix D, we will prove Lemma 4 in Section V. It is noted that RHWI¯(N)\overline{R_{HWI}}(N) in (10) is a monotonically increasing function with respect to N>0N>0. Thus, its minimum lies on

RHWI¯(1)=log2{1+β+λ+μSUκ(β+λ+μSU)+σw2P}\overline{R_{HWI}}\left(1\right)=\log_{2}\left\{1+\frac{\beta+\lambda+\mu_{SU}}{\kappa\left(\beta+\lambda+\mu_{SU}\right)+\frac{\sigma_{w}^{2}}{P}}\right\} (76)

Besides, RHWIDF(N)R_{HWI}^{DF}(N) in (47) is also a monotonically increasing function in relation to N>0N>0, which is limited by RHWIDF(N)|N=12log2(1+2κ)R_{HWI}^{DF}(N)|_{N\rightarrow\infty}=\frac{1}{2}\log_{2}\left(1+\frac{2}{\kappa}\right). Therefore, for the IRS to always outperform the DF relay in terms of the ACR for all N>0N>0, the following relationship should hold:

RHWI¯(1)>RHWIDF(N)|N\overline{R_{HWI}}\left(1\right)>R_{HWI}^{DF}(N)|_{N\rightarrow\infty} (77)

From (77), after a few manipulations, we obtain

κ>2σw4[P2(β+λ+μSU)22σw2P(β+λ+μSU)]1\kappa>2\sigma_{w}^{4}\left[P^{2}(\beta+\lambda+\mu_{SU})^{2}-2\sigma_{w}^{2}P(\beta+\lambda+\mu_{SU})\right]^{-1} (78)

and consequently prove Lemma 4.

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