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Active and Passive IRS Jointly Aided Communication: Deployment Design and Achievable Rate

Min Fu,  and Rui Zhang This work is supported in part by MOE Singapore under Award T2EP50120-0024, National University of Singapore under Research Grant R-261-518-005-720, and The Guangdong Provincial Key Laboratory of Big Data Computing. (Corresponding author: Rui Zhang.)M. Fu is with the Department of Electrical and Computer Engineering, National University of Singapore, Singapore 117583 (e-mail: [email protected]). R. Zhang is with the Chinese University of Hong Kong, Shenzhen, and Shenzhen Research Institute of Big Data, Shenzhen, China 518172 (e-mail: [email protected]). He is also with the Department of Electrical and Computer Engineering, National University of Singapore, Singapore 117583 (e-mail: [email protected]).
Abstract

In this letter, we study the wireless point-to-point communication from a transmitter (Tx) to a receiver (Rx), which is jointly aided by an active intelligent reflecting surface (AIRS) and a passive IRS (PIRS). We consider two practical transmission schemes by deploying the two IRSs in different orders, namely, Tx\rightarrowPIRS\rightarrowAIRS\rightarrowRx (TPAR) and Tx\rightarrowAIRS\rightarrowPIRS\rightarrowRx (TAPR). Assuming line-of-sight channels, we derive the achievable rates for the two schemes by optimizing the placement of the AIRS with the location of the PIRS fixed. Our analysis shows that when the number of PIRS elements and/or the AIRS amplification power is small, the AIRS should be deployed closer to the Rx in both schemes, and TAPR outperforms TPAR with their respective optimized AIRS/PIRS placement. Simulation results validate our analysis and show the considerable performance gain achieved by the jointly optimized AIRS/PIRS deployment over the existing benchmarks under the same power and IRS element budgets.

Index Terms:
Intelligent reflecting surfaces (IRS), active IRS, double IRSs, IRS deployment, rate maximization.

I Introduction

Intelligent reflecting surface (IRS) [1] has recently received significant attention from both academia and industry to improve the spectral and energy efficiency of future wireless networks cost-effectively. An IRS typically consists of an array of passive reflecting elements, each of which reflects the incident signal with a desired phase shift and/or amplitude. Unlike conventional active relays, passive IRSs (PIRSs) do not require costly transmit/receive radio-frequency (RF) chains and thus incur significantly lower power consumption [2]. As IRSs can be flexibly deployed in wireless networks to reconfigure wireless channels dynamically, they have been studied for achieving various functions such as coverage extension, rate enhancement, interference mitigation, etc (see, e.g., [1] and the references therein).

Most of the existing works (e.g., [3, 4, 5, 6, 7]) on IRS have considered the PIRS. Equipped with passive loads (positive resistance), PIRS reflects the incident signal with desired phase shift and reflection gain no larger than one. In addition, PIRSs operate in the full-duplex mode without amplification/processing noise or self-interference [1]. In particular, [3] showed that deploying a single PIRS with NN reflecting elements can lead to a squared power scaling order (i.e., 𝒪(N2)\mathcal{O}(N^{2})) of the reflected signal, which is even higher than that (𝒪(N)\mathcal{O}(N)) of the active arrays. Furthermore, [5] proposed a double-PIRS system where NN reflecting elements are equally allocated over two distributed PIRSs, which yields an even higher power scaling order (𝒪(N4)\mathcal{O}(N^{4})) as compared to the single-PIRS system. Recently, wireless systems aided by multiple PIRSs with multiple signal reflections among them have also been investigated (see [8] and the references therein). Additionally, transmitting passive surfaces were proposed in [9], where they are enclosed on the user’s side to allow the incident signal penetration and provide passive beamforming gain for enhancing the performance. Despite the low cost of PIRSs, their signal coverage performance is severely limited by the product-distance path-loss of the cascaded multi-reflection channel[8]. As a result, one PIRS needs to be allocated massive elements and/or deployed near the transmitter (Tx), the receiver (Rx), or other PIRSs in practice to make its signal reflection effective [8].

Refer to caption
Figure 1: The illustrations of AIRS-PIRS jointly aided wireless communication.

To address this issue with PIRS, the active IRS (AIRS) has emerged as a promising solution [10, 11, 12, 13, 14, 15]. With negative resistance components connected to an additional power supply, AIRSs can adjust phase shifts as well as amplitude amplification with a gain exceeding one. Compared to PIRSs, although AIRSs offer an amplification gain (typically lower than that of active relays with dedicated RF amplifiers), they also induce non-negligible amplification noise in their reflected signals [11]. In particular, given the IRS location and the total power budget, an AIRS was shown to achieve higher spectral efficiency[11], energy efficiency[14], and reliability[13] than its PIRS counterpart. Furthermore, with optimized AIRS/PIRS placements, [12] showed that an AIRS only provides a power scaling of 𝒪(N)\mathcal{O}(N) with NN active reflecting elements due to the amplification noise, but it achieves a higher rate than the PIRS when NN is small or the AIRS amplification power is high. Nevertheless, the AIRS system design (e.g., AIRS deployment and amplification factor optimization) is more complicated to mitigate noise amplification introduced by the AIRS. Existing research on AIRS has mainly focused on comparing a single AIRS [10, 11, 12, 13, 14, 15] or a hybrid IRS comprising active and passive elements [16] to a single PIRS. However, the joint use of distributed AIRS and PIRS in practically challenging scenarios [8] such as multi-turn corridors in an indoor environment has not been studied yet.

To address the above problem, this letter proposes a new wireless communication system jointly aided by a pair of AIRS and PIRS to provide a double-reflection link between a single-antenna Tx and a single-antenna Rx via the two IRSs, while the other links are assumed to be blocked by obstacles. Additionally, we assume that the two IRSs can be properly deployed so that a cascaded line-of-sight (LOS) connection between the Tx and Rx can be established successively through them. Considering two deployment orders for the two IRSs, we present two practical transmission schemes, which are Tx\rightarrowPIRS\rightarrowAIRS\rightarrowRx (TPAR) and Tx\rightarrowAIRS\rightarrowPIRS\rightarrowRx (TAPR) schemes, respectively (see Fig. 1). Under the above settings, we aim to characterize the achievable rates for the two schemes with their respective optimized AIRS/PIRS placement. Our analytic results show that for both schemes, when the number of PIRS elements is small, the AIRS should be placed closer to the Rx with decreasing amplification power. Besides, the TAPR scheme generally outperforms the TPAR scheme when the number of PIRS elements and/or the AIRS amplification power is small. Simulation results validate our analysis and demonstrate that the jointly optimized AIRS/PIRS deployment achieves a much higher rate than the existing benchmarks under the same power and IRS element budgets.

II System Model and Problem Formulation

As illustrated in Fig. 1, a single-antenna111 For the multiple-antenna case, the maximal ratio transmission/combining techniques can be applied at the Tx/Rx. Tx transmits data to a single-antenna Rx222 This work can be extended to multi-user systems, but the corresponding multi-access design requires further investigation; an initial study on AIRS-aided multiple access is given in[17]. that is DD meters (m) away. Under a three-dimensional Cartesian coordinate system, the locations of the Tx and Rx are denoted by 𝒖T=(0,0,0)\bm{u}_{T}=(0,0,0) and 𝒖R=(D,0,0)\bm{u}_{R}=(D,0,0), respectively. A pair of PIRS and AIRS are deployed between them to assist in their communication. The PIRS and AIRS are respectively placed at given altitudes, denoted by HPH_{P} and HAH_{A}, so that the Tx can communicate with the Rx via only a double-reflection link through the two IRSs over three LOS channels. In particular, we assume that the PIRS is fixed above the Tx or Rx to minimize the path loss, and the AIRS can be flexibly placed between them to maximize the channel gain. Thus, two transmission schemes333These two schemes can be practically used for downlink and uplink communications; however, the different deployment order of AIRS and PIRS generally results in different weighted sum-rate performance. are considered by deploying the PIRS and AIRS in different orders, i.e., TAPR shown in Fig. 1(a) and TPAR shown in Fig. 1(b).

Let NpN_{p} and NaN_{a} denote the number of passive/active reflecting elements on the PIRS/AIRS, respectively. We further define 𝒩a\mathcal{N}_{a} and 𝒩p\mathcal{N}_{p} as the sets containing all the elements on the AIRS and PIRS, respectively. Let 𝚯P=diag(ηP,1ejϕP,1,,ηP,NpejϕP,Np)\bm{\Theta}_{P}=\text{diag}(\eta_{P,1}e^{j\phi_{P,1}},\ldots,\eta_{{P,N_{p}}}e^{j\phi_{P,N_{p}}}) and 𝚽A=diag(ηA,1ejϕA,1,,ηA,NaejϕA,Na)\bm{\Phi}_{A}=\text{diag}(\eta_{A,1}e^{j\phi_{A,1}},\ldots,\eta_{{A,N_{a}}}e^{j\phi_{A,N_{a}}}) denote the reflection matrices of PIRS and AIRS respectively, where ηP,n/ηA,n\eta_{P,n}/\eta_{A,n} and ϕP,n/ϕA,n[0,2π)\phi_{P,n}/\phi_{A,n}\in[0,2\pi)444 The results in this letter can be extended to the practical setup with discrete phase-shift levels (e.g., by applying the quantization technique[7]). denote respectively the passive/active reflection amplitude and passive/active phase-shift at element nn. Therein, for maximal reflection of the PIRS and ease of practical implementation [1], we further set ηP,n=1,n𝒩p\eta_{P,n}=1,\forall n\in\mathcal{N}_{p}. Furthermore, since the transmitted signal arriving at all active elements experiences the same path loss under LOS channels, a common amplification factor η\eta should be used to maximize the rate performance as in[11, 14], i.e., ηA,n=η1,n𝒩a\eta_{A,n}=\eta\geq 1,\forall n\in\mathcal{N}_{a}, which also simplifies the design of amplification factors of different IRS elements in practice. Moreover, different from the PIRS that reflects signals without incurring amplification noise, the AIRS generates non-negligible amplification noise at all reflecting elements, which is denoted by 𝒏aNa×1\bm{n}_{\rm a}\in\mathbb{C}^{N_{a}\times 1} and assumed to follow the independent circularly symmetric complex Gaussian distribution, i.e., 𝒏a𝒞𝒩(𝟎Na,σF2𝐈Na)\bm{n}_{\rm a}\sim\mathcal{CN}(\bm{0}_{N_{a}},\sigma^{2}_{\rm F}{\bf I}_{N_{a}}) with power σF2\sigma^{2}_{\rm F}.

II-A TAPR Transmission Scheme

First, we consider the TAPR scheme with the PIRS fixed above the Rx, as shown in Fig. 1(a).

II-A1 Signal model

Denoting the Tx-AIRS horizontal distance as xTAx_{TA}(a design variable), the locations of the PIRS/AIRS are represented by 𝒖P=(D,0,HP)\bm{u}_{P}=(D,0,H_{P}) and 𝒖A=(xTA,0,HA)\bm{u}_{A}=(x_{TA},0,H_{A}), respectively. Thus, the distances between the Rx and PIRS, the Tx and AIRS, and the AIRS and PIRS are respectively given by

dPR=HP,dTA(xTA)=xTA2+HA2,\displaystyle d_{PR}=H_{P},d_{TA}(x_{TA})=\sqrt{x_{TA}^{2}+H_{A}^{2}}, (1)
dAP(xTA)=(DxTA)2+(HPHA)2.\displaystyle d_{AP}(x_{TA})=\sqrt{(D-x_{TA})^{2}+(H_{P}-H_{A})^{2}}. (2)

Let 𝒈TANa×1\bm{g}_{\rm TA}\in\mathbb{C}^{N_{a}\times 1}, 𝑺APNp×Na\bm{S}_{\rm AP}\in\mathbb{C}^{N_{p}\times N_{a}}, and 𝒉RP𝖧1×Np\bm{h}_{\rm RP}^{\sf H}\in\mathbb{C}^{1\times N_{p}} denote the baseband equivalent LOS channels for Tx\rightarrowAIRS, AIRS\rightarrowPIRS, and PIRS\rightarrowRx links, respectively. Before modeling LOS channels, we first define the one-dimensional steering vector function for a uniform linear array (ULA) as

𝒆(θ,M)=[1,ejπθ,,ejπ(M1)θ]𝖳M×1,\displaystyle\bm{e}(\theta,M^{\prime})=[1,e^{-j\pi\theta},\ldots,e^{-j\pi(M^{\prime}-1)\theta}]^{\sf T}\in\mathbb{C}^{M^{\prime}\times 1}, (3)

where θ\theta denotes the constant phase-shift difference between the signals at two adjacent elements and MM^{\prime} denotes the size of the ULA. For the uniform planar array (UPA) model, each array response vector can be expressed as the Kronecker product of two steering vector functions in the x-axis and y-axis directions, respectively. For example, the array response vector for the UPA from the Tx to AIRS is expressed as

𝒂TA(θTA,ϑTA,Na)=𝒆(2ΔAλsin(θTA)cos(ϑTA),Na,x)\displaystyle\!\!\!\!\!\bm{a}_{TA}(\theta_{TA},\vartheta_{TA},N_{a})=\bm{e}(\frac{2\Delta_{A}}{\lambda}\sin(\theta_{TA})\cos(\vartheta_{TA}),N_{a,x})\otimes
𝒆(2ΔAλsin(θTA)sin(ϑTA),Na,y)Na×1,\displaystyle\hskip 40.00006pt\bm{e}(\frac{2\Delta_{A}}{\lambda}\sin(\theta_{TA})\sin(\vartheta_{TA}),N_{a,y})\in\mathbb{C}^{N_{a}\times 1}, (4)

where λ\lambda denotes the signal wavelength, ΔA\Delta_{A} denotes the element space at the AIRS, (θTA,ϑTA)(\theta_{TA},\vartheta_{TA}) is the angle-of-arrival pair, and Na,xN_{a,x} and Na,yN_{a,y} denote the number of horizontal/vertical elements at the AIRS with Na=Na,x×Na,yN_{a}=N_{a,x}\times N_{a,y}. As such, 𝑺PA\bm{S}_{\rm PA}, 𝒈AT\bm{g}_{\rm AT}, and 𝒉PR𝖧\bm{h}_{\rm PR}^{\sf H} are respectively given by

𝑺AP=β/dAPej2πdAPλ𝒔¯AP𝒔~PA𝖧,\displaystyle\bm{S}_{\rm AP}\!=\!{\sqrt{\beta}}/{d_{AP}}e^{\frac{-j2\pi d_{AP}}{\lambda}}\bar{\bm{s}}_{AP}\tilde{\bm{s}}_{PA}^{\sf H}, (5)
𝒈TA=β/dTAej2πdTAλ𝒈¯TA,𝒉RP𝖧=β/HPej2πHpλ𝒉¯RP𝖧,\displaystyle\bm{g}_{\rm TA}\!=\!{\sqrt{\beta}}/{d_{TA}}e^{\frac{-j2\pi d_{TA}}{\lambda}}\bar{\bm{g}}_{TA},\bm{h}_{\rm RP}^{\sf H}\!=\!{\sqrt{\beta}}/{H_{P}}e^{\frac{-j2\pi H_{p}}{\lambda}}\bar{\bm{h}}_{RP}^{\sf H}, (6)

where β\beta denotes the reference channel power at a distance of 1 m, 𝒔¯AP=𝒂AP(θAP,ϑAP,Np)\bar{\bm{s}}_{AP}=\bm{a}_{AP}(\theta_{AP},\vartheta_{AP},N_{p}), 𝒔~PA=𝒂PA(θPA,ϑPA,Na)\tilde{\bm{s}}_{PA}=\bm{a}_{PA}(\theta_{PA},\vartheta_{PA},N_{a}), 𝒈¯TA=𝒂TA(θTA,ϑTA,Na)\bar{\bm{g}}_{TA}=\bm{a}_{TA}(\theta_{TA},\vartheta_{TA},N_{a}), and 𝒉¯RP=𝒂RP(θRP,ϑRP,Np)\bar{\bm{h}}_{RP}=\bm{a}_{RP}(\theta_{RP},\vartheta_{RP},N_{p}). In this letter, we assume perfect channel state information (CSI) is available555 The existing channel estimation techniques proposed for double-IRS-aided systems (see e.g., [8]) can be applied to obtain the CSI in our considered system. .

Though the Tx\rightarrowAIRS\rightarrowPIRS\rightarrowRx reflecting link, the signal received at the Rx is given by

ya\displaystyle\!\!\!\!\!\!y_{a} =\displaystyle= 𝒉RP𝖧𝚯P𝑺APη𝚯A(𝒈TAs+𝒏a)+e\displaystyle\bm{h}_{\rm RP}^{\sf{H}}\bm{\Theta}_{P}\bm{S}_{\rm AP}\eta\bm{\Theta}_{A}\Big{(}\bm{g}_{\rm TA}s+\bm{n}_{\rm a}\Big{)}+e (7)
=\displaystyle= 𝒉RP𝖧𝚯P𝑺APη𝚯A𝒈TAsDouble-reflected signal+𝒉RP𝖧𝚯P𝑺APη𝚯A𝒏aNoise introduced by the AIRS+e,\displaystyle\underbrace{\bm{h}_{\rm RP}^{\sf{H}}\bm{\Theta}_{P}\bm{S}_{\rm AP}\eta\bm{\Theta}_{A}\bm{g}_{\rm TA}s}_{\text{Double-reflected signal}}+\underbrace{\bm{h}_{\rm RP}^{\sf{H}}\bm{\Theta}_{P}\bm{S}_{\rm AP}\eta\bm{\Theta}_{A}\bm{n}_{\rm a}}_{\text{Noise introduced by the AIRS}}+e,

where ss denotes the transmitted signal with power PtP_{\rm t} of the Tx, and ee denotes the additive white Gaussian noise at the Rx with power σ2\sigma^{2}. As observed from (7), the two IRSs can jointly enhance the double-reflected signal power whereas the AIRS introduces additional amplification noise. The received signal-to-noise ratio (SNR) at the Rx is expressed as

𝖲𝖭𝖱a(𝚯A,𝚯P,η,xTA)=𝒉RP𝖧𝚯P𝑺APη𝚯A𝒈TA2Pt𝒉RP𝖧𝚯P𝑺APη𝚯A2σF2+σ2,\displaystyle\!\!{\sf SNR}_{a}(\bm{\Theta}_{A},\bm{\Theta}_{P},\eta,x_{TA})=\frac{\|\bm{h}_{\rm RP}^{\sf{H}}\bm{\Theta}_{P}\bm{S}_{\rm AP}\eta\bm{\Theta}_{A}\bm{g}_{\rm TA}\|^{2}P_{\rm t}}{\|\bm{h}_{\rm RP}^{\sf{H}}\bm{\Theta}_{P}\bm{S}_{\rm AP}\eta\bm{\Theta}_{A}\|^{2}\sigma^{2}_{\rm F}+\sigma^{2}}, (8)

and the achievable rate (in bits per second per Hertz or bps/Hz) for the TAPR scheme is given by

𝖱a=log2(1+𝖲𝖭𝖱a(𝚯A,𝚯P,η,xTA)).\displaystyle{\sf R}_{a}=\log_{2}\left(1+{\sf SNR}_{a}(\bm{\Theta}_{A},\bm{\Theta}_{P},\eta,x_{TA})\right). (9)

To ensure its reflection amplifier operating in an amplification mode [18] so as to improve the performance over PIRS, the AIRS should be properly deployed to meet the following constraint:

η1.\displaystyle\eta\geq 1. (10)

Denoting PFP_{\rm F} as the given amplification power budget of the AIRS, the amplification power constraint over the signal reflected by the AIRS is given by [12, 11]

η2(Pt𝚯A𝒈TA2+σF2𝚯A𝐈Na2)PF.\displaystyle\eta^{2}\left(P_{\rm{t}}\|\bm{\Theta}_{A}\bm{g}_{\rm TA}\|^{2}+\sigma_{\rm F}^{2}\|{\bm{\Theta}_{A}}{\bf I}_{N_{a}}\|^{2}\right)\leq P_{\rm F}. (11)

II-A2 Problem formulation

We aim to maximize the achievable rate for the Rx by jointly optimizing the reflection matrices at the PIRS/AIRS (i.e., 𝚯P\bm{\Theta}_{P} and η𝚯A\eta\bm{\Theta}_{A}) and the AIRS deployment (i.e., xTAx_{TA}). Accordingly, for the TAPR scheme, the optimization problem is formulated as

maximize𝚯A,𝚯P,η,xTA\displaystyle\mathop{\text{maximize}}\limits_{\begin{subarray}{c}\bm{\Theta}_{A},\bm{\Theta}_{P},\eta,\\ x_{TA}\end{subarray}} log2(1+𝖲𝖭𝖱𝖺(𝚯A,𝚯P,η,xTA))\displaystyle\log_{2}\left(1+{\sf SNR_{a}}(\bm{\Theta}_{A},\bm{\Theta}_{P},\eta,x_{TA})\right)
subject to |𝚯P(n,n)|=1,n𝒩p,\displaystyle|\bm{\Theta}_{P}(n,n)|=1,\forall n\in{{\mathcal{N}_{p}}},
|𝚯A(n,n)|=1,n𝒩a,\displaystyle|\bm{\Theta}_{A}(n,n)|=1,\forall n\in{{\mathcal{N}_{a}}},
0xTAD,\displaystyle 0\leq x_{TA}\leq D,
Constraints (10),(11).\displaystyle\text{Constraints~{}}\eqref{Cons:activeIRS1-TAPR},~{}\eqref{Cons:activeIRS2-TAPR}.

Since the objective function is increasing with η\eta, the amplification power constraint in (11) needs to be active at the optimal solution of problem (12). Furthermore, constraint (11) is independent of the phase values in 𝚯A\bm{\Theta}_{A} and 𝚯P\bm{\Theta}_{P}. In addition, since the objective function is increasing with 𝒉RP𝖧𝚯P𝒔¯AP2\|\bm{h}_{\rm RP}^{\sf{H}}\bm{\Theta}_{P}\bar{\bm{s}}_{\rm AP}\|^{2} and its denominator is independent of the phase value of 𝚯A\bm{\Theta}_{A}, it is maximized by designing the phases of the AIRS and PIRS to align in the cascaded Tx-AIRS-PIRS-Rx channel. Thus, for given xTAx_{TA}, the optimal phase design of the AIRS/PIRS and amplification factor are respectively given by

𝚯A(n,n)=ej([𝒔~PA𝖧]n+[𝒈TA]n),\displaystyle\bm{\Theta}_{A}(n,n)=e^{-j(\angle[\tilde{\bm{s}}_{PA}^{\sf H}]_{n}+\angle[\bm{g}_{\rm TA}]_{n})}, (13)
𝚯P(n,n)=ej([𝒔¯AP]n+[𝒉RP𝖧]n),\displaystyle\bm{\Theta}_{P}(n,n)=e^{-j(\angle[\bar{\bm{s}}_{AP}]_{n}+\angle[\bm{h}^{\sf H}_{\rm RP}]_{n})}, (14)
η=PFdTA2(xTA)/(PtNaβ+dTA2(xTA)σF2Na).\displaystyle\eta=\sqrt{P_{\rm F}d^{2}_{TA}(x_{TA})/(P_{\rm{t}}N_{a}\beta+d^{2}_{TA}(x_{TA})\sigma_{\rm F}^{2}N_{a}}). (15)

Combining (13), (14), (15) into (8) yields

𝖲𝖭𝖱a(xTA)\displaystyle\!\!\!\!\!{\sf SNR}_{a}(x_{TA})
=PtPFβ2NaNp2C1dTA2(xTA)+C2dAP2(xTA)+C3dTA2(xTA)dAP2(xTA),\displaystyle\!\!\!\!\!=\frac{P_{\rm{t}}P_{\rm F}\beta^{2}N_{a}N_{p}^{2}}{C_{1}d^{2}_{TA}(x_{TA})+C_{2}d^{2}_{AP}(x_{TA})+C_{3}d^{2}_{TA}(x_{TA})d^{2}_{AP}(x_{TA})},

where C1=σF2PFβNp2C_{1}=\sigma_{F}^{2}P_{\rm F}\beta N_{p}^{2}, C2=σ2PtHP2C_{2}=\sigma^{2}P_{\rm{t}}H_{P}^{2}, and C3=HP2σF2σ2/βC_{3}=H_{P}^{2}\sigma_{\rm F}^{2}\sigma^{2}/\beta. After substituting (13), (14), and (15) into (12), problem (12) is equivalent to the following,

maximizexTA\displaystyle\mathop{\text{maximize}}\limits_{x_{TA}} log2(1+𝖲𝖭𝖱a(xTA))\displaystyle\log_{2}(1+{\sf SNR}_{a}(x_{TA}))
subject to xaxTAD,\displaystyle x_{a}\leq x_{TA}\leq D, (17a)

where constraint (17a) corresponds to (10) in problem (12),

xa=max{0,NaβPt/(PFNaσF2)HA2}.\displaystyle x_{a}=\sqrt{\max\{0,N_{a}\beta P_{\rm{t}}/(P_{\rm F}-N_{a}\sigma_{\rm F}^{2})-H_{A}^{2}\}}. (18)

Although the optimal solution to problem (17) is difficult to be characterized in closed form due to the complicated expression of 𝖲𝖭𝖱a(xTA){\sf SNR}_{a}(x_{TA}), its value can be obtained by using a one-dimensional search over xTA[xa,D]x_{TA}\in[x_{a},D]. In the following, we first characterize the effects of AIRS amplification power and the number of PIRS elements on the optimal AIRS placement.

Lemma 1.

The optimal Tx-AIRS horizontal distance (i.e., xTAx^{\star}_{TA}) to problem (17) is non-increasing with PFP_{\rm F} and monotonically decreasing with NpN_{p}.

Proof.

First, it can be shown that xax_{a} in (17a) is non-increasing with PFP_{\rm F}. In addition, it is observed that C1C_{1} and dTA(xTA)d_{TA}(x_{TA}) in 𝖲𝖭𝖱a(xTA){\sf SNR}_{a}(x_{TA}) monotonically increase with both PFP_{\rm F} and xTAx_{TA} while dAP(xTA)d_{AP}(x_{TA}) in 𝖲𝖭𝖱a(xTA){\sf SNR}_{a}(x_{TA}) decreases with xTAx_{TA}. As a result, supposing without constraint (17a), when PFP_{\rm F} increases, the optimal solution xTAx^{\star}_{TA} should be decreased to guarantee the first derivative of the objective function to be zero. Combining the above, xTAx^{\star}_{TA} is non-increasing with PFP_{\rm F}. As for NpN_{p}, it can be shown that xax_{a} is independent of NpN_{p} while C1C_{1} monotonically increases with NpN_{p}. Similarly, it can be concluded that xTAx^{\star}_{TA} is decreasing with NpN_{p}. This thus completes the proof. ∎

First, as observed from (15), amplification factor η\eta is proportional to xTAx_{TA} and PFP_{\rm F}. Based on (8), although the received signal power increases with η\eta and NpN_{p}, the AIRS-induced noise is also increased. Thus, from Lemma 1, as PFP_{\rm F} and NpN_{p} increase, the AIRS has to be deployed closer to the Tx to attenuate the AIRS-PIRS channel gain, thus suppressing its induced noise power at the Rx.

II-B TPAR Transmission Scheme

Next, we consider TPAR with the PIRS fixed above the Tx, as shown in Fig. 1(b). Similarly to TAPR, denoting the horizontal distance between the Tx and AIRS as xTAx_{TA}, the locations of the PIRS/AIRS are represented by 𝒖P=(0,0,HP)\bm{u}_{P}=(0,0,H_{P}) and 𝒖A=(xTA,0,HA)\bm{u}_{A}=(x_{TA},0,H_{A}), respectively. The signal model of TPAR is also similar to that of TAPR, while the expressions of the AIRS amplification noise and its power constraint are different since the order of the AIRS/PIRS placements is reversed. The detailed expressions are omitted for brevity.

Similarly to the design of 𝚯A\bm{\Theta}_{A} and 𝚯P\bm{\Theta}_{P} in TAPR, the amplification factor and receiver SNR in TPAR are given by

η=PFdAP2/(PtNaβ2Np2/HP2+dAP2σF2Na),\displaystyle\eta=\sqrt{P_{\rm F}d^{2}_{AP}/(P_{\rm{t}}N_{a}\beta^{2}N_{p}^{2}/H_{P}^{2}+d^{2}_{AP}\sigma_{\rm F}^{2}N_{a})},
𝖲𝖭𝖱b(xTA)\displaystyle\!\!\!\!\!{\sf SNR}_{b}(x_{TA})
=\displaystyle= Naβ2Np2PtPFC2/adAP2(xTA)+aC1dAR2(xTA)+C3dAP2(xTA)dAR2(xTA),\displaystyle\!\!\!\!\!\frac{N_{a}\beta^{2}N_{p}^{2}P_{\rm t}P_{\rm F}}{C_{2}/ad^{2}_{AP}(x_{TA})\!+\!aC_{1}d^{2}_{AR}(x_{TA})\!+\!C_{3}d^{2}_{AP}(x_{TA})d^{2}_{AR}(x_{TA})},

where a=Ptσ2PFσF2a=\frac{P_{t}\sigma^{2}}{P_{\rm F}\sigma_{\rm F}^{2}}. As a result, the optimization problem of the TPAR scheme is formulated as

maximizexTA\displaystyle\mathop{\text{maximize}}\limits_{\ x_{TA}} log2(1+𝖲𝖭𝖱b(xTA))\displaystyle\log_{2}(1+{\sf SNR}_{b}(x_{TA}))
subject to xbxTAD,\displaystyle x_{b}\leq x_{TA}\leq D, (21a)

where constraint (21a) is due to the amplification power constraint at the AIRS, and

xb=max{0,NaNp2β2Pt/((PFNaσF2)HP2)(HPHA)2}.\displaystyle\!x_{b}\!=\!\sqrt{\!\max\{0,N_{a}N_{p}^{2}\beta^{2}P_{\rm{t}}/((P_{\rm F}\!-\!N_{a}\sigma_{\rm F}^{2})H_{P}^{2})\!-\!(H_{P}\!-\!H_{A})^{2}\}}.

Similarly to problem (17), the optimal solution of problem (21) can also be obtained by using the one-dimensional search over xTA[xb,D]x_{TA}\in[x_{b},D]. Likewise, we have the following lemma for the TPAR scheme.

Lemma 2.

The optimal Tx-AIRS horizontal distance (i.e., xTAx^{\star}_{TA}) to problem (21) is non-increasing with PFP_{\rm F} and monotonically increasing with NpN_{p}.

Proof.

The proof is similar to that of Lemma 1, and thus omitted for brevity. ∎

Lemma 2 can be intuitively understood for the TPAR scheme. The AIRS-induced noise is independent of the number of PIRS reflecting elements. As observed from (II-B), with a smaller PFP_{\rm F} and/or a larger NpN_{p}, the AIRS should be deployed closer to the Rx to provide a higher amplification factor with η>1\eta>1 and reduce the path loss of the cascaded channel, thus increasing the signal power at the Rx.

III Low-Complexity Placement Design and Performance Comparison

In this section, we present suboptimal AIRS deployment solutions in closed-form for the TAPR and TPAR schemes, respectively. Based on these results, we compare the performance of the two schemes in terms of achievable rate.

III-A Suboptimal Solutions

First, to simplify problems (17) and (21), we present a useful lemma as follows (for which the proof is omitted for brevity).

Lemma 3.

Given Dmax{HA,HP}D\gg\max\{H_{A},H_{P}\}, we have C1dTA2(xTA)+C2dAP2(xTA)C3dTA2(xTA)dAP2(xTA)C_{1}d^{2}_{TA}(x_{TA})+C_{2}d^{2}_{AP}(x_{TA})\gg C_{3}d^{2}_{TA}(x_{TA})d^{2}_{AP}(x_{TA}) and C2/adAP2(xTA)+aC1dAR2(xTA)C3dAP2(xTA)dAR2(xTA)C_{2}/ad^{2}_{AP}(x_{TA})+aC_{1}d^{2}_{AR}(x_{TA})\gg C_{3}d^{2}_{AP}(x_{TA})d^{2}_{AR}(x_{TA}), xTA[0,D]\forall x_{TA}\in[0,D], if

min{βNpPtβHpσF+PFβσ,βNpPFβHpσ+PtβσF}D.\displaystyle\!\!\!\!\min\{\!\frac{\sqrt{\beta}N_{p}\sqrt{P_{\rm t}\beta}}{H_{p}\sigma_{\rm F}}\!+\!\frac{\sqrt{P_{\rm F}\beta}}{\sigma},\frac{\sqrt{\beta}N_{p}\sqrt{P_{\rm F}\beta}}{H_{p}\sigma}\!+\!\frac{\sqrt{P_{\rm t}\beta}}{\sigma_{\rm F}}\}\!\gg\!D. (22)

III-A1 TAPR Scheme

When condition (22) is satisfied, 𝖱𝖺\sf{R}_{a} in problem (17) can be approximated as 𝖱¯a=log2(1+𝖲𝖭𝖱¯a)\overline{\sf{R}}_{a}=\log_{2}(1+\overline{\sf{SNR}}_{a}), where 𝖲𝖭𝖱¯a=PtPFβ2NaNp2C1xTA2+C2(DxTA)2\overline{\sf{SNR}}_{a}=\frac{P_{\rm{t}}P_{\rm{F}}\beta^{2}N_{a}N_{p}^{2}}{C_{1}x^{2}_{TA}+C_{2}(D-x_{TA})^{2}}. Therefore, problem (17) is approximated as

maximizexTA\displaystyle\mathop{\text{maximize}}\limits_{x_{TA}} log2(1+PtPFβ2NaNp2C1xTA2+C2(DxTA)2)\displaystyle\log_{2}\Big{(}1+\frac{P_{\rm{t}}P_{\rm{F}}\beta^{2}N_{a}N_{p}^{2}}{C_{1}x^{2}_{TA}+C_{2}(D-x_{TA})^{2}}\Big{)}
subject to constraint (17a).\displaystyle\text{constraint~{}}\eqref{Cons:deployment1}. (23)

By setting the first derivative of the objective function of (III-A1) with respect to xTAx_{TA} to zero and then projecting it into the feasible set of problem (III-A1), the optimal solution to problem (III-A1) can be obtained as

xTAa=max{aDa+b,xa},\displaystyle x^{a}_{TA}=\max\{\frac{aD}{a+b},x_{a}\}, (24)

where a=Ptσ2PFσF2a=\frac{P_{t}\sigma^{2}}{P_{\rm F}\sigma_{\rm F}^{2}} and b=βNp2HP2b=\frac{\beta N_{p}^{2}}{H_{P}^{2}}. Note that when aDa+b>xa\frac{aD}{a+b}>x_{a}, the amplification factor (i.e., η\eta) in problem (12) is larger than 1. Given η>1\eta>1, the receiver SNR is approximated as

𝖲𝖭𝖱¯a=PFβNaD2σ2(a+b)=βNaD2(PtσF2+PFNp2βσ2Hp).\displaystyle\overline{\sf{SNR}}_{a}=\frac{P_{\rm F}\beta N_{a}}{D^{2}\sigma^{2}}(a+b)=\frac{\beta N_{a}}{D^{2}}(\frac{P_{\rm t}}{\sigma_{\rm F}^{2}}\!+\!\frac{P_{\rm F}N_{p}^{2}\beta}{\sigma^{2}H_{p}}). (25)

III-A2 TPAR Scheme

Similarly, based on Lemma 3, problem (21) is approximated as

maximizexTA\displaystyle\mathop{\text{maximize}}\limits_{x_{TA}} log2(1+PtPFβ2NaNp21/aC2xTA2+aC1(DxTA)2)\displaystyle\log_{2}\Big{(}1+\frac{P_{\rm t}P_{\rm F}\beta^{2}N_{a}N_{p}^{2}}{1/aC_{2}x_{TA}^{2}+aC_{1}(D-x_{TA})^{2}}\Big{)}
subject to constraint (21a).\displaystyle\text{constraint~{}}\eqref{Cons:TPAR-deployment}. (26)

Similarly to problem (III-A1), the optimal solution to problem (III-A2) is obtained as

xTAb=max{abDab+1,xb}.\displaystyle x^{b}_{TA}=\max\{\frac{abD}{ab+1},x_{b}\}. (27)

Given η>1\eta>1, the approximated receiver SNR is given by

𝖲𝖭𝖱¯b=PFβNaD2σ2(ab+1)=βNaD2(PtNp2βσF2Hp+PFσ2).\displaystyle\overline{\sf{SNR}}_{b}=\frac{P_{\rm F}\beta N_{a}}{D^{2}\sigma^{2}}(ab+1)=\frac{\beta N_{a}}{D^{2}}(\frac{P_{\rm t}N_{p}^{2}\beta}{\sigma_{\rm F}^{2}H_{p}}+\frac{P_{\rm F}}{\sigma^{2}}). (28)

III-B Comparisons between TPAR and TAPR

With the suboptimal AIRS deployments given in (24) and (27), the achievable rates for the TPAR and TAPR schemes are compared as follows.

Refer to caption
Figure 2: Optimal AIRS placement versus amplification power of the AIRS.
Refer to caption
Figure 3: Achievable rate versus amplification power of the AIRS.
Refer to caption
Figure 4: Achievable rate versus Tx-Rx distance when PF=2P_{F}=2 dBm.
Proposition 1.

Given η>1\eta>1 and NpHPβN_{p}\leq\frac{H_{P}}{\sqrt{\beta}}, the achievable rate of the TPAR scheme is no less than that of the TAPR scheme, i.e., 𝖱¯a𝖱¯b\overline{\sf{R}}_{a}\geq\overline{\sf{R}}_{b}, if

PFPtσ2σF2.\displaystyle P_{\rm F}\leq\frac{P_{\rm t}\sigma^{2}}{\sigma_{\rm F}^{2}}. (29)

Otherwise, 𝖱¯a<𝖱¯b\overline{\sf{R}}_{a}<\overline{\sf{R}}_{b}. The result is reversed when NpHPβN_{p}\geq\frac{H_{P}}{\sqrt{\beta}}.

Proof.

Comparing 𝖱¯a\overline{\sf{R}}_{a} and 𝖱¯b\overline{\sf{R}}_{b} is equivalent to comparing 𝖲𝖭𝖱¯a\overline{\sf{SNR}}_{a} and 𝖲𝖭𝖱¯b\overline{\sf{SNR}}_{b}. Thus, with η>1\eta>1, based on (25) and (28), we have

𝖲𝖭𝖱¯a𝖲𝖭𝖱¯b\displaystyle\overline{\sf{SNR}}_{a}-\overline{\sf{SNR}}_{b} =\displaystyle= PFβNaD2σ2(a+bab1)\displaystyle\frac{P_{\rm F}\beta N_{a}}{D^{2}\sigma^{2}}(a+b-ab-1) (30)
=\displaystyle= βNaD2(PtσF2PFσ2)(Hp2Np2β)Hp2.\displaystyle\frac{\beta N_{a}}{D^{2}}\frac{(\frac{P_{\rm t}}{\sigma_{\rm F}^{2}}-\frac{P_{\rm F}}{\sigma^{2}})(H_{p}^{2}-N_{p}^{2}\beta)}{H_{p}^{2}}.

Based on (30), we can conclude that 𝖱¯a𝖱¯b\overline{\sf{R}}_{a}\geq\overline{\sf{R}}_{b}, if

NpHPβ,PFσ2PtσF2,or NpHPβ,PFσ2PtσF2.\displaystyle N_{p}\leq\frac{H_{P}}{\sqrt{\beta}},\frac{P_{\rm F}}{\sigma^{2}}\leq\frac{P_{\rm t}}{\sigma_{\rm F}^{2}},\text{or~{}}N_{p}\geq\frac{H_{P}}{\sqrt{\beta}},\frac{P_{\rm F}}{\sigma^{2}}\geq\frac{P_{\rm t}}{\sigma_{\rm F}^{2}}. (31)

Otherwise, 𝖱¯a<𝖱¯b\overline{\sf{R}}_{a}<\overline{\sf{R}}_{b}. This thus completes the proof. ∎

IV Numerical Results

In this section, we present numerical results to compare the rate performance of the TAPR and TPAR schemes in an AIRS-PIRS jointly aided communication system. If not specified otherwise, the simulation parameters are set as follows. The AIRS and PIRS are assumed to be deployed at altitudes of HA=6H_{A}=6 m and HP=5H_{P}=5 m, respectively. The carrier frequency is 3.5 GHz and thus the reference channel gain is β=(λ/4π)2=43\beta=(\lambda/4\pi)^{2}=-43 dB, with the carrier wavelength λ=0.087\lambda=0.087 m. Other parameters are set as D=30D=30 m, Pt=20P_{\rm t}=20 dBm, σ2=80\sigma^{2}=-80 dBm, and σF2=4σ2=74\sigma_{\rm F}^{2}=4\sigma^{2}=-74 dBm. Under our simulation setup, we consider a limited budget of reflecting elements with Na<Np<HPβ700N_{a}<N_{p}<\frac{H_{P}}{\sqrt{\beta}}\approx 700 (see Proposition 1). The numbers of AIRS and PIRS elements are thus fixed as Na=450N_{a}=450 and Np=600N_{p}=600, respectively.

For performance comparison, we consider the existing benchmarks with a single AIRS [12], a hybrid IRS (with active and passive elements) [16], double PIRSs [5], and a single PIRS [7]. For the double-PIRS scheme, both PIRSs are equipped with (Na+Np)/2(N_{a}+N_{p})/2 passive elements and deployed above the Tx and Rx, respectively. As for the single-PIRS scheme, the PIRS is equipped with Na+NpN_{a}+N_{p} passive elements and deployed above the Tx or Rx. Furthermore, the transmit power of Tx in the double-PIRS/single-PIRS systems is (Pt+PF)(P_{\rm t}+P_{\rm F}). As such, it is fair to compare it with the AIRS-PIRS jointly aided system. For the latter, we also consider four fixed AIRS/PIRS deployments, where xAPx_{AP} equals D/2D/2 or DD in both TAPR/TPAR schemes.

Fig. 4 shows the optimal Tx-AIRS horizontal distance versus AIRS amplification power. We observe that the optimal AIRS placement in both schemes is closer to the Rx (i.e., larger xTAx_{TA}) as PFP_{\rm F} decreases. This is consistent with Lemmas 1 and 2. Additionally, the proposed suboptimal solution achieves near-optimal performance, validating its effectiveness and the result in Lemma 3.

Fig. 4 compares the achievable rates versus AIRS amplification power. First, as PFP_{F} increases, we observe that the rate performance of the AIRS-PIRS jointly aided system increases due to the increasing amplification gain from AIRS. However, compared to these fixed deployment strategies, the AIRS deployment design dynamically balances the signal and noise amplification at the AIRS, thereby further improving performance for both TAPR/TPAR schemes. Furthermore, with the optimal AIRS placement, TAPR performs better than TPAR when PF<Ptσ2σF2P_{\rm F}<\frac{P_{\rm t}\sigma^{2}}{\sigma_{\rm F}^{2}}, because it suffers less path loss of the cascaded channel and thus results in higher received power. These results are consistent with Proposition 1. In addition, thanks to the optimal AIRS/PIRS placement and the resulting amplification gain at AIRS, the AIRS-PIRS jointly aided system achieves a much higher rate than the baseline double-PIRS system under a limited IRS element budget.

Fig. 4 shows that the achievable rate of different schemes with optimal IRS placement versus Tx-Rx distance for PF=2P_{F}=2 dBm. We can observe that TAPR performs better than hybrid-IRS and single-AIRS benchmarks, especially when the Tx-Rx distance is relatively short. This is because TAPR provides higher multiplicative beamforming and amplification gains by jointly using PIRS and AIRS as well as an additional path to attenuate amplification noise as compared to the two single-reflection schemes. This indicates that deploying distributed AIRS and PIRS with the best ordering can be advantageous over combining them into one hybrid IRS or using AIRS only.

V Conclusion

In this letter, we studied a new AIRS-PIRS jointly aided wireless communication system. Under the LOS channel model, we analyzed the effects of the AIRS deployment in two transmission schemes (i.e., TAPR and TPAR) on their achievable rates. Our analysis revealed that the AIRS should be deployed closer to the Rx in both schemes, and TAPR achieves a higher rate than TPAR when the number of PIRS elements and/or AIRS amplification power is limited. Simulation results validated our analysis and demonstrated that our proposed system considerably outperforms the existing benchmarks in terms of achievable rate, and the performance gain highly depends on the AIRS/PIRS deployment.

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