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Fundamental Limit of Angular Resolution in Partly Calibrated Arrays with Position Errors

Guangbin Zhang, Yan Wang, Tianyao Huang and Yonina C. Eldar  This work was supported by the National Natural Science Foundation of China under Grants 62271053, 62331007, 62171259, 62401063. G. Zhang is with Yangtze Delta Region Academy of Beijing Institute of Technology, Jiaxing, Zhejiang, China (e-mail:[email protected]). Y. Wang is with Radar Research Laboratory, School of Information and Electronics, Beijing Institute of Technology, Beijing, China (e-mail:[email protected]). T. Huang is with the School of Computer and Communication Engineering, University of Science and Technology Beijing, Beijing, China (e-mail:[email protected]). Yonina C. Eldar is with the Department of Computer Science and Applied Mathematics, Weizmann Institute of Science, Israel (e-mail:[email protected]). Y. Wang is the corresponding author.
Abstract

We consider high angular resolution detection using distributed mobile platforms implemented with so-called partly calibrated arrays, where position errors between subarrays exist and the counterparts within each subarray are ideally calibrated. Since position errors between antenna arrays affect the coherent processing of measurements from these arrays, it is commonly believed that its angular resolution is influenced. A key question is whether and how much the angular resolution of partly calibrated arrays is affected by the position errors, in comparison with ideally calibrated arrays. To address this fundamental problem, we theoretically illustrate that partly calibrated arrays approximately achieve high angular resolution. Our analysis uses a special characteristic of Crame´{\rm\acute{e}}r-Rao lower bound (CRB) w.r.t. the source separation: When the source separation increases, the CRB first declines rapidly, then plateaus out, and the turning point is close to the angular resolution limit. This means that the turning point of CRB can be used to indicate angular resolution. We then theoretically analyze the declining and plateau phases of CRB, and explain that the turning point of CRB in partly calibrated arrays is close to the angular resolution limit of distributed arrays without errors, demonstrating high resolution ability. This work thus provides a theoretical guarantee for the high-resolution performance of distributed antenna arrays in mobile platforms.

Index Terms:
Partly calibrated arrays, angular resolution, the declining and plateau phases of CRB, the turning point of CRB.

I Introduction

High angular resolution is desired to achieve precise target detection in applications such as radar, sonar, and astronomy. Antenna array is a common tool for direction finding. Since the angular resolution of an antenna array is inversely proportional to the aperture of the array [1], large aperture arrays are used to achieve high resolution. However, for a single array, large aperture means high system complexity, high cost and poor mobility, which restricts the scope of application.

A promising solution is to instead use multiple distributed arrays of small apertures and fuse their measurements coherently, known as ‘distributed arrays’ [2]. Ideally, distributed arrays achieve high angular resolution inversely proportional to the whole array aperture with lower system complexity. However, for distributed arrays loaded on mobile platforms such as unmanned aerial vehicles (UAVs), which are common in the low-altitude economy, drone swarms, and similar applications, it is difficult to locate the arrays accurately in real time due to the mobility of the platforms, and position errors between subarrays are unavoidable. Such distributed arrays with unknown inter-subarray position errors (and with no or calibrated intra-subarray position errors) are called partly calibrated arrays [3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13, 14]. In contrast, distributed arrays with exactly known array positions are called fully calibrated arrays [15]. A main concern is whether partly calibrated arrays could achieve the same (or similar) angular resolution as fully calibrated arrays under the negative influence of unknown errors. Note that partly calibrated arrays in this paper refer to distributed arrays with position errors between subarrays, and do not include other types of errors such as gain and phase errors [16, 17] or clock synchronization errors [18].

Though the performance of direction finding with partly calibrated arrays is intuitively inferior to the counterpart with error-free arrays, some existing algorithms experimentally show that under certain assumptions the former achieve similar angular resolution as the latter. These assumptions include, for example, high signal-to-noise rate (SNR), enough snapshots and uncorrelated source signals [4, 5], and isotropic linear arrays with the same topology [14]. However, the high-resolution ability depends on specific algorithms and their assumptions, and the scope of application is limited. Whether errors seriously degrade the resolution or not is still an open problem in more general scenarios, and is hard to solve only from the perspective of algorithm design.

Inspired by the positive empirical results, we aim to theoretically analyze the fundamental limit of angular resolution in partly calibrated arrays. The first step is to quantify angular resolution for general arrays. However, the typical Rayleigh criterion, where the central maximum of one source’s beamforming result coincides with the first minimum of the other, struggles to effectively explain the resolution of distributed arrays with errors. This is because the Rayleigh criterion is under the assumption of error-free scenarios. When errors are present, the beamforming results are significantly affected by the unknown errors and exhibit irregular behavior, making it difficult to characterize the resolution performance as in the ideal cases. This motivates us to explore alternative resolution metrics.

To this end, the statistical resolution limit (SRL) was proposed in this context and studied extensively [19, 20, 21, 22, 23, 24, 25, 26, 27]. SRL is empirically defined as the minimum separation between the parameter of interest that makes two closely spaced signals distinguishable. Several criteria are introduced to describe SRL, which are mainly divided into spectrum based [19, 20], detection based [21, 22, 23, 24] and estimation based [25, 26, 27, 28] criteria. However, the spectrum based resolution criterion is not perfectly suitable for partly calibrated arrays with position errors, since the distortion of spectral peaks caused by errors can significantly complicates the analysis. Otherwise, spectrum based and detection based criteria depend on specific estimation algorithms and hypothesis testing strategies, respectively. Estimation based criteria use estimation accuracy limit, Crame´{\rm\acute{e}}r-Rao lower bound (CRB), to characterize the resolution limit, which is independent of specific algorithms or detection strategies. However, typical CRB based criteria rely on high SNR and no modeling or signal mismatch [26], which are not directly applicable in distributed arrays with position errors. Recently, a resolution criterion based on Gaussian process was proposed [29]. However, it primarily targets optical three-dimensional imaging, making it difficult to apply directly to radar signal processing.

The main factor affecting the resolution is array aperture. To better quantify the angular resolution in a way less dependent on SNR and the error-free assumptions, we exploit a characteristic of CRB with respect to angular separation. Particularly, the CRB curve first shows a rapid decline along with the increase of the source separation Δω\Delta\omega from zero to a turning point. After that turning point, the curve displays minor fluctuations, and soon converges to some fixed level. The turning point is close to the angular resolution limit Ω\Omega [26]. We explain the reason of this phenomenon as follows: 1) when sources are closely placed and are unresolvable (ΔωΩ\Delta\omega\leqslant\Omega), the estimation accuracy is poor and the CRB is high; in this region, as the separation increases, the CRB declines, indicating the significant improvement on the estimation accuracy; when the sources becomes resolvable (ΔωΩ\Delta\omega\geqslant\Omega), the CRB tends to be stable. This shows the rationality of using the CRB curve’s turning point as an indicator of angular resolution.

We then show that in partly calibrated arrays the CRB curve’s turning point is inversely proportional to the whole aperture of the array by analyzing the behavior of CRB in two regions: in the unresolvable part (ΔωΩ\Delta\omega\ll\Omega), we show that the CRB declines polynomially with respect to Δω\Delta\omega and theoretically calculate the decline speed; in the resolvable part (ΔωΩ\Delta\omega\geqslant\Omega), we illustrate that the partial derivative of CRB with respect to Δω\Delta\omega is close to zero. These two behaviours in the declining and plateau phases confirm the existence and location of the turning point, and consequently indicate angular resolution.

Our main contributions are summarized as follows:

  • We propose a new criterion that uses the turning point of CRB to indicate angular resolution;

  • We use the proposed criterion to demonstrate that partly calibrated arrays achieve high angular resolution similar as fully calibrated arrays, both inversely proportional to the whole array aperture.

The above conclusion provides an important theoretical guarantee for the high-resolution performance of distributed antenna arrays in mobile platforms. To our best knowledge, this work is the first to theoretically explain the high resolution performance limit of distributed arrays in the presence of position errors between subarrays.

The rest of this paper is organized as follows. Section II reviews the related works. Section III provides the signal models of fully and partly calibrated arrays. Section IV introduces our main contributions of indicating the angular resolution of partly calibrated arrays using the proposed criterion. In Section V, we detail the proofs of our main contributions. Numerical simulations are given in Section VI to verify the analysis, followed by a conclusion in Section VII.

We use \mathbb{Z}, \mathbb{R} and \mathbb{C} to denote the sets of integer, real and complex numbers, respectively. The expectation of a random variable \cdot is written as 𝔼[]\mathbb{E}[\cdot]. Uppercase boldface letters denote matrices (e.g. 𝑨\bm{A}) and lowercase boldface letters denote vectors (e.g. 𝒂\bm{a}). The (m,n)(m,n)-th element of a matrix 𝑨\bm{A} is denoted by [𝑨]m,n[\bm{A}]_{m,n}, and the nn-th column is represented by [𝑨]n[\bm{A}]_{n}. We use trace(){\rm trace}(\cdot) to indicate the trace of a matrix and diag(𝒂){\rm diag}(\bm{a}) to represent a matrix with diagonal elements given by 𝒂\bm{a}. The conjugate, transpose, and conjugate transpose operators are denoted by ,T,H{}^{*},^{T},^{H}, respectively. The amplitude of a scalar and the l2l_{2} norm of a vector are represented by |||\cdot| and 2\|\cdot\|_{2}, respectively. The cardinality of a set 𝒩\mathcal{N} is represented by |𝒩||\mathcal{N}|. The Hadamard product is written as \odot, the semi-definite operator is denoted by \succcurlyeq, and the definition symbol is defined as \equiv. We denote the imaginary unit for complex numbers by j=1j=\sqrt{-1}.

II CRB as a resolution metric

In this section, we review the related works of CRB based resolution criteria and analyze their application in indicating angular resolution of partly calibrated arrays.

To clarify the resolvability of closely spaced signals in a given scenario, SRL is an efficient typical tool that received wide attention [19, 20, 21, 22, 23, 24, 25, 26, 27, 30, 31, 32]. Particularly, SRL is defined as the minimum distance between two closely spaced signals embedded in an additive noise that allows a correct resolvability/parameter estimation [21]. One of the main techniques to describe and derive SRL is based on estimation accuracy since the resolved signals intuitively have higher estimation accuracy than the corresponding unresolved ones. CRB is widely used to characterize the upper bound of estimation accuracy, and therefore it is natural to combine SRL and CRB to explain the resolution limit.

Particularly, assume that there are two signals with frequencies 𝒇=[f1,f2]T\bm{f}=[f_{1},f_{2}]^{T} mixed together and denote the resolution limit of 𝒇\bm{f} by Ωf\Omega_{f}. Let the CRB of 𝒇\bm{f} be written as

CRB(𝒇)=[CRB(f1)CRB(f1,f2)CRB(f1,f2)CRB(f2)].\displaystyle{\rm CRB}(\bm{f})=\begin{bmatrix}{\rm CRB}(f_{1})&{\rm CRB}(f_{1},f_{2})\\ {\rm CRB}(f_{1},f_{2})&{\rm CRB}(f_{2})\end{bmatrix}. (1)

The average CRB of frequency 𝒇\bm{f} is defined as

CRB¯(𝒇)=12(CRB(f1)+CRB(f2)).\displaystyle\overline{\rm CRB}(\bm{f})=\frac{1}{2}\big{(}{\rm CRB}(f_{1})+{\rm CRB}(f_{2})\big{)}. (2)

Unless otherwise emphasized, the CRBs mentioned after this section refer to the average CRB (omitting the horizontal bar).

Existing related works construct the correlation between resolution limit and CRB by some criteria. In [25], Lee criterion states that: two signals are resolvable w.r.t. the frequencies if the maximum standard deviation of each frequency estimate is less than half the difference between f1f_{1} and f2f_{2}, shown as Ωf=2max{CRB(f1),CRB(f2)}\Omega_{f}=2{\rm max}\left\{\sqrt{{\rm CRB}(f_{1})},\sqrt{{\rm CRB}(f_{2})}\right\}. This criterion ignores the coupling between the parameters f1,f2f_{1},f_{2}, i.e., CRB(f1,f2){\rm CRB}(f_{1},f_{2}) in (1). To this end, Smith criterion in [26] states that: two signals are resolvable w.r.t. the frequencies if the difference between the frequencies, Δf=f2f1\Delta f=f_{2}-f_{1}, is greater than the standard deviation of the estimation of Δf\Delta f, shown as Ωf=Δf=CRB(Δf)\Omega_{f}=\Delta f=\sqrt{{\rm CRB}(\Delta f)}. This means that SRL is obtained by solving the following equation,

CRB(Δf)=𝒖TCRB(𝒇)𝒖,\displaystyle{\rm CRB}(\Delta f)=\bm{u}^{T}{\rm CRB}(\bm{f})\bm{u}, (3)

where 𝒖=[1,1]T\bm{u}=[1,-1]^{T}. The work in [21] extends these criteria to multidimensional harmonic retrieval cases.

However, the above metrics are only feasible in scenarios with appropriately high SNR and no modeling or signal mismatch [26]. For example, when the SNR approaches infinity, the CRB decreases to 0, implying that the resolution approaches 0 by theses criteria. This apparently contradicts the principle that the angular resolution of arrays mainly depends on the aperture, known as Rayleigh resolution limit [33]. The contradiction mainly stems from the significant influence of noise on the absolute value of CRB, and the scope of application is hence limited.

Directly using the existing CRB based criteria to analyze the angular resolution limit of partly calibrated arrays leads to impractical conclusions: We take the Smith criterion as an example. Denote the angular resolution limit of fully and partly calibrated arrays by ΩFC\Omega_{\rm FC} and ΩPC\Omega_{\rm PC}, respectively. Smith criterion in (3) implies that

ΩFC2\displaystyle\Omega_{\rm FC}^{2} =𝒖TCRBFC(𝝎)𝒖,\displaystyle=\bm{u}^{T}{\rm CRB}_{\rm FC}(\bm{\omega})\bm{u}, (4)
ΩPC2\displaystyle\Omega_{\rm PC}^{2} =𝒖TCRBPC(𝝎)𝒖,\displaystyle=\bm{u}^{T}{\rm CRB}_{\rm PC}(\bm{\omega})\bm{u}, (5)

where 𝒖=[1,1]T\bm{u}=[1,-1]^{T}. Since CRBPCCRBFC{\rm CRB}_{\rm PC}\succcurlyeq{\rm CRB}_{\rm FC} [4], we have ΩPCΩFC\Omega_{\rm PC}\geqslant\Omega_{\rm FC}, yielding that the angular resolution of partly calibrated arrays can be much worse than fully calibrated arrays’. This conclusion conflicts with the high-resolution performance of existing direction-finding algorithms for partly calibrated arrays [4, 5, 14].

In summary, the performance of existing CRB based criteria is seriously affected by noise and model error. The above shortcomings motivate us to propose a new resolution criterion that is less sensitive to noise and explains the angular resolution of partly calibrated arrays more practically, which is detailed in Subsection IV-A.

III Signal model

Consider KK linear antenna subarrays with NN array elements in total located on a line. The kk-th subarray is composed of |𝒩k||\mathcal{N}_{k}| elements, where 𝒩k\mathcal{N}_{k} denotes the index set of elements in the kk-th subarray and the full index set is denoted by 𝒩k𝒩k={1,,N}\mathcal{N}\equiv\bigcup_{k}\mathcal{N}_{k}=\{1,\dots,N\}. Denote by φn\varphi_{n} the position of the nn-th element relative to the 1-st element’s for n𝒩n\in\mathcal{N}. Without loss of generality, we assume φN>>φ1=0\varphi_{N}>\dots>\varphi_{1}=0, and denote the whole array aperture by D=φND=\varphi_{N}. Partly calibrated arrays assume that the intra-subarray displacements, φpkφqk\varphi_{p_{k}}-\varphi_{q_{k}} with pk,qk𝒩kp_{k},q_{k}\in\mathcal{N}_{k} are exactly known or well calibrated, however, the inter-subarray displacement between the kk-th subarray and the 1-st subarray, denoted by ξkφn¯k1+1φ1=φn¯k1+1\xi_{k}\equiv\varphi_{\bar{n}_{k-1}+1}-\varphi_{1}=\varphi_{\bar{n}_{k-1}+1}, is assumed unknown, where the number of elements in the first kk subarrays is defined as n¯k=i=1k|𝒩i|\bar{n}_{k}=\sum_{i=1}^{k}|\mathcal{N}_{i}| for k=1,,Kk=1,\dots,K (ξ1=0\xi_{1}=0). In comparison, fully calibrated arrays assume that the positions of all the elements, {φn}n𝒩\{\varphi_{n}\}_{n\in\mathcal{N}}, are exactly known. Let 𝝃=[ξ2,,ξK]T(K1)×1\bm{\xi}=[\xi_{2},\dots,\xi_{K}]^{T}\in\mathbb{R}^{(K-1)\times 1}. Assume that the NN elements share a common/well-synchronized sampling clock. The diagram of partly calibrated array is shown in Fig. 1.

Refer to caption
Figure 1: Partly calibrated array.

Consider LL far-field [34], narrow-band sources impinging the signals onto the whole array from different directions θ1,,θL(π/2,π/2)\theta_{1},\dots,\theta_{L}\in(-\pi/2,\pi/2) with θ1<<θL\theta_{1}<\dots<\theta_{L}. Assume that these LL sources are identifiable for each subarray, i.e., L<min{|𝒩k|,k=1,,K}L<\min\{|\mathcal{N}_{k}|,k=1,\dots,K\}. Denote by ωl=2πsinθlλ\omega_{l}=\frac{2\pi\sin\theta_{l}}{\lambda} the spatial angular frequency of the ll-th source for l=1,,Ll=1,\dots,L, where λ\lambda is the wavelength of the source signals. The Rayleigh resolution limit of ω\omega in the fully calibrated array case is defined as Ω2π/D\Omega\equiv 2\pi/D (ignoring the coefficient). Denote the vectors of directions and spatial angular frequencies by 𝜽=[θ1,,θL]TL×1\bm{\theta}=[\theta_{1},\dots,\theta_{L}]^{T}\in\mathbb{R}^{L\times 1} and 𝝎=[ω1,,ωL]TL×1\bm{\omega}=[\omega_{1},\dots,\omega_{L}]^{T}\in\mathbb{R}^{L\times 1}, respectively. The maximum spatial frequency separation is defined as ΔωωLω1>0\Delta\omega\equiv\omega_{L}-\omega_{1}>0.

In the partly calibrated array case, the received signal of the kk-th subarray is expressed as

𝒚k(t)=𝑨k(𝝎,ξ)𝒔(t)+𝒏k(t)|𝒩k|×1,\displaystyle\bm{y}_{k}(t)=\bm{A}_{k}(\bm{\omega},\xi)\bm{s}(t)+\bm{n}_{k}(t)\in\mathbb{C}^{|\mathcal{N}_{k}|\times 1}, (6)

where 𝑨k(𝝎,ξ)=[𝒂k(ω1,ξ),,𝒂k(ωL,ξ)]|𝒩k|×L\bm{A}_{k}(\bm{\omega},\xi)=[\bm{a}_{k}(\omega_{1},\xi),\dots,\bm{a}_{k}(\omega_{L},\xi)]\in\mathbb{C}^{|\mathcal{N}_{k}|\times L} is the kk-th steering matrix, [𝒂k(ωl,ξ)]i=ejωlφn[\bm{a}_{k}(\omega_{l},\xi)]_{i}=e^{j\omega_{l}\varphi_{n}} for i=nn¯k1i=n-\bar{n}_{k-1} and n𝒩kn\in\mathcal{N}_{k}, 𝒔(t)L×1\bm{s}(t)\in\mathbb{C}^{L\times 1} contains the complex coefficients of the sources, 𝒏k(t)|𝒩k|×1\bm{n}_{k}(t)\in\mathbb{C}^{|\mathcal{N}_{k}|\times 1} denotes white noise with power σ2\sigma^{2}, and tt denotes sample time, t=t1,t2,,tTt=t_{1},t_{2},\dots,t_{T}. Note that [𝒂k(ωl,ξ)]i=ejωl(φnξk)ejωlξk[\bm{a}_{k}(\omega_{l},\xi)]_{i}=e^{j\omega_{l}(\varphi_{n}-\xi_{k})}\cdot e^{j\omega_{l}\xi_{k}}, where φnξk\varphi_{n}-\xi_{k} denotes the known intra-subarray displacement and ξk\xi_{k} denotes the unknown inter-subarray displacement.

Stacking the KK received signals in (6) together yields

𝒚(t)=𝑨(𝝎,𝝃)𝒔(t)+𝒏(t),\displaystyle\bm{y}(t)=\bm{A}(\bm{\omega},\bm{\xi})\bm{s}(t)+\bm{n}(t), (7)

where

𝒚(t)\displaystyle\bm{y}(t) =[𝒚1T(t),,𝒚KT(t)]TN×1,\displaystyle=[\bm{y}_{1}^{T}(t),\dots,\bm{y}_{K}^{T}(t)]^{T}\in\mathbb{C}^{N\times 1},
𝑨(𝝎,𝝃)\displaystyle\bm{A}(\bm{\omega},\bm{\xi}) =[𝒂(ω1,𝝃),,𝒂(ωL,𝝃)]N×L,\displaystyle=[\bm{a}(\omega_{1},\bm{\xi}),\dots,\bm{a}(\omega_{L},\bm{\xi})]\in\mathbb{C}^{N\times L},
𝒂(ωl,𝝃)\displaystyle\bm{a}(\omega_{l},\bm{\xi}) =[𝒂1T(ωl,ξ),,𝒂KT(ωl,ξ)]TN×1,\displaystyle=[\bm{a}_{1}^{T}(\omega_{l},\xi),\dots,\bm{a}_{K}^{T}(\omega_{l},\xi)]^{T}\in\mathbb{C}^{N\times 1},
𝒏(t)\displaystyle\bm{n}(t) =[𝒏1T(t),,𝒏KT(t)]TN×1.\displaystyle=[\bm{n}_{1}^{T}(t),\dots,\bm{n}_{K}^{T}(t)]^{T}\in\mathbb{C}^{N\times 1}.

In (7), 𝒚(t)\bm{y}(t) is known, 𝑨(𝝎,𝝃),𝒔(t),𝒏(t)\bm{A}(\bm{\omega},\bm{\xi}),\bm{s}(t),\bm{n}(t) are unknown and 𝝎\bm{\omega} is to be estimated. For fully and partly calibrated arrays, 𝝃\bm{\xi} in 𝑨(𝝎,𝝃)\bm{A}(\bm{\omega},\bm{\xi}) is assumed to be completely known and unknown, respectively. For conciseness, we abbreviate 𝑨(𝝎,𝝃)\bm{A}(\bm{\omega},\bm{\xi}) to 𝑨\bm{A}, 𝒂k(ωl,ξ)\bm{a}_{k}(\omega_{l},\xi) to 𝒂k(ωl)\bm{a}_{k}(\omega_{l}) and 𝒂(ωl,𝝃)\bm{a}(\omega_{l},\bm{\xi}) to 𝒂(ωl)\bm{a}(\omega_{l}), respectively.

The CRBs of spatial frequencies 𝝎\bm{\omega} in fully and partly calibrated arrays, denoted by CRBFC(𝝎){\rm CRB}_{\rm FC}(\bm{\omega}) and CRBPC(𝝎){\rm CRB}_{\rm PC}(\bm{\omega}), respectively, are shown in Appendix A.

IV Our main contributions

In this section, we detail our main contributions: 1) propose a new CRB based resolution criterion less sensitive to noise and model error; 2) use the proposed criterion to show that partly calibrated arrays achieve high angular resolution similar to fully calibrated arrays.

Particularly, we first introduce the intuition behind the proposed criterion of indicating angular resolution by the turning point of CRB in Subsection IV-A. We then analyze the angular resolution of partly calibrated arrays and show the high-resolution ability in Subsection IV-B. Finally, we apply the proposed resolution criterion to fully calibrated arrays and compare the analysis results with prior works in Subsection IV-C.

IV-A The proposed resolution criterion

To meet the challenge of analyzing the resolution limit of partly calibrated arrays, we propose a new resolution criterion using the turning point of CRB. The proposed criterion states that: two signals are said to be resolvable w.r.t. the frequencies if the difference between the frequencies, Δf=f2f1\Delta f=f_{2}-f_{1}, is greater than the turning point of CRB w.r.t. Δf\Delta f denoted by Ωf𝒯(CRB(𝐟))\Omega_{f}\equiv\mathcal{T}\left({\rm CRB}(\bm{f})\right). The definition of the CRB turning point is detailed in Section V-D.

The basic principle of this criterion is based on a significant phenomenon of CRB(𝒇){\rm CRB}(\bm{f}): Fix the source of f1f_{1} as a reference and gradually increase the frequency difference Δf>0\Delta f>0. The CRB(𝒇){\rm CRB}(\bm{f}) first declines rapidly w.r.t. Δf\Delta f, and then it almost remains constant (with a small fluctuation). The turning point is located close to the angular resolution limit. We show this phenomenon in fully and partly calibrated arrays as an example. Consider using 1010 half-wavelength, uniform linear subarrays to estimate the directions of 22 sources with the angles 𝜽=[1.2,1.2+Δθ]T\bm{\theta}=[1.2^{\circ},1.2^{\circ}+\Delta\theta]^{T}, where Δθ>0\Delta\theta>0 denotes the angle difference. There are 1010 elements in each subarray and the adjacent subarrays are spaced at half-wavelength apart. Denote by Ωf2π/D\Omega_{f}\equiv 2\pi/D the angular resolution limit, where DD is the whole array aperture. The CRBs of fully and partly calibrated arrays, CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC}, are shown in Fig. 2.

Refer to caption
Figure 2: CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} w.r.t. Δf\Delta f.

From Fig. 2, we find that the two CRBs decline when Δf/Ωf1\Delta f/\Omega_{f}\leqslant 1, and tend to be stable when Δf/Ωf>1\Delta f/\Omega_{f}>1. We provide an intuitive explanation of this phenomenon: when the frequency difference Δf\Delta f is within the resolution limit Ωf\Omega_{f}, the sources cannot be distinguished, disrupting the estimation performance and greatly increasing the CRB; in this case, increasing Δf\Delta f increases the resolvability and hence decreases the CRB, which corresponds to the declining phase of the CRB. When Δf\Delta f exceeds Ωf\Omega_{f}, the estimation accuracy is close to the counterpart of estimating the sources separately [25]; consequently, the accuracy is less relevant to Δf\Delta f, keeping the CRB constant, which corresponds to the plateau phase of the CRB. Here, ’plateaus phase’ refers to a situation where, after some change, a trend or curve stabilizes and no longer shows significant variation or fluctuation, which is consistent with the CRB when ΔfΩf\Delta f\geqslant\Omega_{f}. Therefore, the turning point between the declining and the plateau phases indicates angular resolution.

For another reason, we use the turning point of CRB as the angular resolution limit since it can reflect the influence on each other for parameter estimation, which is precisely the meaning of resolution. Particularly, when two sources are not distinguished, they significantly influence each other, resulting in poor estimation performance as reflected in the decline part of CRB. When the two sources can be separated, their mutual influence is minimal, and the CRB approaches the performance of separate estimation. Thus, the transition point between these two states can be used to indicate the resolution, which is the turning point of CRB.

The reason that the turning point is not exactly located at Δf=Ωf\Delta f=\Omega_{f} is that on one hand, the theoretical proof in the paper represents the result in a statistical average sense (see the A2 assumption in Section V), which cannot ensure that the turning point of the CRB in every specific scenario precisely locates on the resolution cell; on the other hand, resolution criterion, either the Rayleigh resolution limit or 3dB beam width, is an empirical concept, which is not an absolute indication of separability or non-separability. Overall, it can ensure that the magnitude of the resolution is correct.

In the proposed resolution criterion, angular resolution depends not only on the angular difference but also on the absolute angle values. This is because that we use the frequency separation, Δf\Delta f, to reflect source separation instead of angle separation, Δθ\Delta\theta. Particularly in Fig. 2, we have Δf=2π(sinθ2sinθ1)/λ\Delta f=2\pi(\sin\theta_{2}-\sin\theta_{1})/\lambda and Δθ=θ2θ1\Delta\theta=\theta_{2}-\theta_{1}. Through trigonometric transformation, we have

Δf=4πλsin(Δθ2)cos(θ2+θ12).\displaystyle\Delta f=\frac{4\pi}{\lambda}\sin\left(\frac{\Delta\theta}{2}\right)\cos\left(\frac{\theta_{2}+\theta_{1}}{2}\right). (8)

In the above equation, the sin part reflects the angular resolution and the cos part reflects the angle values themselves. Therefore, the CRB is not only related to the angle separation Δθ\Delta\theta, but also angle values (θ2+θ1)/2(\theta_{2}+\theta_{1})/2. It can be found that large angle values have worse resolution.

Note that the proposed resolution criterion using the CRB turning point is almost unaffected by SNR. This is because in the CRB expression (see (35) and (36) in Appendix A), the component of white noise σ2\sigma^{2} can be isolated, which means that it only affects the absolute value of the CRB without altering its relative variation with respect to the angle difference. Although this property contradicts the commonly held conclusion that resolution is related to SNR, it is rational in analyzing the effect of position errors in distributed arrays. This is because that inter-subarray position errors fundamentally differ from white noise errors: the former are multiplicative errors, while the latter are additive errors. When the SNR is extremely low, it becomes impossible to distinguish and estimate the angles, making it ineffective to analyze the impact of multiplicative errors on resolution. Therefore, we aim to conduct an analysis method that is unaffected or minimally affected by additive noise. The proposed resolution criterion using the CRB turning point can effectively address this challenge.

In the sequel, we apply the proposed criterion to analyze the angular resolution of fully and partly calibrated arrays. A main conclusion is that partly calibrated arrays achieve high resolution similar to that of fully calibrated arrays. Note that the above phenomenon of CRB w.r.t. Δf\Delta f was also mentioned in previous works [25, 26], but they did not use it to indicate resolution and provide the corresponding theoretical guarantees. The key challenge is to analyze the partial derivative of CRB to Δf\Delta f, which is hard to analytically calculate. In Section V, we provide an approximate method to solve this problem.

IV-B Resolution analysis on partly calibrated arrays

Here, we analyze the declining phase, plateau phase, and turning point of CRBPC{\rm CRB}_{\rm PC}, and use the turning point to indicate angular resolution of partly calibrated arrays.

IV-B1 Declining phase of CRBPC{\rm CRB}_{\rm PC}

We analyze the declining phase of CRBPC{\rm CRB}_{\rm PC} using small quantity approximation, shown as Proposition 1, which illustrates that the main declining rate of CRBPC{\rm CRB}_{\rm PC} is proportional to (Δω)2(L1)(\Delta\omega)^{-2(L-1)}.

Proposition 1 (declining phase for partly calibrated arrays).

When ΔωΩ\Delta\omega\ll\Omega, we have

CRBPC=(Δω)2(L1)𝑪G+O((Δω)2(L1)+1),\displaystyle{\rm CRB}_{\rm PC}=(\Delta\omega)^{-2(L-1)}\bm{C}_{G}+O((\Delta\omega)^{-2(L-1)+1}), (9)

where 𝐂G\bm{C}_{G} is a constant w.r.t. Δω\Delta\omega.

Proof.

See Appendix B. ∎

IV-B2 Plateau phase of CRBPC{\rm CRB}_{\rm PC}

We analyze the plateau phase of CRBPC{\rm CRB}_{\rm PC}, shown as Proposition 2, where the assumptions are detailed in Subsection V-A. Proposition 2 illustrates that CRBPC{\rm CRB}_{\rm PC} remains almost constant w.r.t. Δω\Delta\omega when ΔωΩ\Delta\omega\geqslant\Omega. Here CRB(Δω){\rm CRB}(\Delta\omega) denotes the functional relationship between CRB and Δω\Delta\omega instead of the CRB of Δω\Delta\omega.

Proposition 2 (plateau phase for partly calibrated arrays).

Under assumptions A1-A3, when ΔωΩ\Delta\omega\geqslant\Omega, we have

|CRBPC(Δω)Δω|0\displaystyle\left|\frac{\partial{\rm CRB}_{\rm PC}(\Delta\omega)}{\partial\Delta\omega}\right|\approx 0 (10)

with high probability.

Proof.

See Subsection V-B. ∎

This proposition illustrates that under the scenario of using a large, sparse, uniformly distributed array to resolve two closely spaced sources (corresponding to assumptions A1-A3 in Section V-A), CRBPC{\rm CRB}_{\rm PC} remains almost constant w.r.t. Δω\Delta\omega when ΔωΩ\Delta\omega\geqslant\Omega. Based on the proposed criterion, the stable CRB implies that the sources are resolvable in this situation. The approximation in Proposition 2 is used for the convenience of explanation and a more rigorous expression is detailed in the corresponding proof.

IV-B3 Turning point of CRBPC{\rm CRB}_{\rm PC}

Intuitively, the intersection of the declining phase and plateau phase of CRB corresponds to the turning point. Based on Proposition 1 and Proposition 2, a criterion [35] is used to determine the turning point of CRBPC{\rm CRB}_{\rm PC} in a strict sense, given by

𝒯(CRBPC)=Ω=2π/D,\displaystyle\mathcal{T}\left({\rm CRB}_{\rm PC}\right)=\Omega=2\pi/D, (11)

where the explanation is detailed in Subsection V-D.

The conclusion of applying our proposed resolution criterion to CRBPC{\rm CRB}_{\rm PC} in (11) implies that high angular resolution is achievable for partly calibrated arrays, inversely proportional to the whole array aperture DD, which is consistent with existing direction-finding algorithms for partly calibrated arrays [4, 5, 14]. A main advantage relative to the existing CRB based SRL criteria is that the proposed criterion is less sensitive to noise. This helps to focus on the main factors that affect the resolution (array aperture), while reducing the interference of secondary factors (noise), and avoid the limitations of existing CRB based criteria.

IV-C Resolution analysis on fully calibrated arrays

For comparison, we analyze the declining phase, plateau phase, and turning point of CRBFC{\rm CRB}_{\rm FC}, and use the turning point to indicate angular resolution of fully calibrated arrays.

IV-C1 Declining phase of CRBFC{\rm CRB}_{\rm FC}

The declining phase of CRBFC{\rm CRB}_{\rm FC} has been theoretically analyzed using small quantity approximation in [25], shown as Lemma 1. It is proven that when ΔωΩ\Delta\omega\ll\Omega, CRBFC{\rm CRB}_{\rm FC} declines at the rate mainly proportional to (Δω)2(L1)(\Delta\omega)^{-2(L-1)}, which is the same as the counterpart of CRBPC{\rm CRB}_{\rm PC}.

Lemma 1 (declining phase for fully calibrated arrays[25]).

When ΔωΩ\Delta\omega\ll\Omega, we have

CRBFC=(Δω)2(L1)𝑪F+O((Δω)2(L1)+1),\displaystyle{\rm CRB}_{\rm FC}=(\Delta\omega)^{-2(L-1)}\bm{C}_{F}+O((\Delta\omega)^{-2(L-1)+1}), (12)

where 𝐂F\bm{C}_{F} is a constant w.r.t. Δω\Delta\omega.

IV-C2 Plateau phase of CRBFC{\rm CRB}_{\rm FC}

We analyze the plateau phase of CRBFC{\rm CRB}_{\rm FC} in Proposition 3, which illustrates that CRBFC{\rm CRB}_{\rm FC} remains almost constant w.r.t. Δω\Delta\omega when ΔωΩ\Delta\omega\geqslant\Omega. The rigorous expression is similar to the counterpart of CRBPC{\rm CRB}_{\rm PC}, which is detailed in the corresponding proof.

Proposition 3 (plateau phase for fully calibrated arrays).

Under assumptions A1-A3, when ΔωΩ\Delta\omega\geqslant\Omega, we have

|CRBFC(Δω)Δω|0\displaystyle\left|\frac{\partial{\rm CRB}_{\rm FC}(\Delta\omega)}{\partial\Delta\omega}\right|\approx 0 (13)

with high probability.

Proof.

See Subsection V-C. ∎

IV-C3 Turning point of CRBFC{\rm CRB}_{\rm FC}

Based on Lemma 1 and Proposition 3, we use the criterion in [35] to determine the turning point of CRBFC{\rm CRB}_{\rm FC} in a strict sense, given by

𝒯(CRBFC)=Ω=2π/D,\displaystyle\mathcal{T}\left({\rm CRB}_{\rm FC}\right)=\Omega=2\pi/D, (14)

where the explanation is similar with that of CRBPC{\rm CRB}_{\rm PC}.

Based on the proposed criterion, (14) means that the resolution limit of fully calibrated arrays is inversely proportional to the whole array aperture DD, which is consistent with existing Rayleigh resolution limit. This verifies the feasibility of the proposed criterion and supports to apply it on the resolution analysis of partly calibrated arrays.

Our main contributions on theoretically analyzing the declining phase, plateau phase and turning point of CRB are summarized in Table I.

TABLE I: Our main contributions
fully calibrated partly calibrated
declining phase Lemma 1 [25] Proposition 1
plateau phase Proposition 3 Proposition 2
turning point Ω=2π/D\Omega=2\pi/D Ω=2π/D\Omega=2\pi/D

Note that the super-resolution phenomenon in the existing self-calibration methods does not contradict the conclusion of this paper. This is because existing super-resolution algorithms [36, 37] make additional prior assumptions about the scenario and model, whereas the signal model in this paper does not. For instance, sparse recovery algorithms assume that targets are sparsely located within the solution space, and subspace methods assume uncorrelated source signals. These assumptions introduce extra feature information compared to the classical model, thereby affecting the model’s performance bounds, which manifest as improvements in resolution. However, we base our study on the classical model assumptions without incorporating other prior assumptions such as sparsity, and therefore, it does not involve super-resolution performance.

V Proof of the propositions in Section IV

In this section, we prove Propositions 2 and 3, while the proof of Proposition 1 is left to Appendix B since it is a direct extension of [25]. First, we introduce assumptions A1-A3 in Subsection V-A, followed by the detailed proofs of Propositions 2 and 3 in Subsection V-B and V-C, respectively. Based on the proofs above, we explain how to determine the turning point of CRB in Subsection V-D.

V-A Assumptions

To analyze the angular resolution in fully and partly calibrated arrays, we impose the following assumptions (A3 is not necessary for fully calibrated arrays.). A diagram is shown in Fig. 3.

  • A1:

    Consider L=2L=2 sources with spatial frequencies denoted by ω1=ω0\omega_{1}=\omega_{0} and ω2=ω0+Δω\omega_{2}=\omega_{0}+\Delta\omega.

  • A2:

    The average of the element positions of each subarray is uniformly distributed in [0,D][0,D], i.e., φ¯k𝒰[0,D]\bar{\varphi}_{k}\sim\mathcal{U}[0,D], where

    φ¯k=n𝒩kφn|𝒩k|.\displaystyle\bar{\varphi}_{k}=\frac{\sum_{n\in\mathcal{N}_{k}}\varphi_{n}}{|\mathcal{N}_{k}|}. (15)

    Each subarray has the same number of elements, i.e., |𝒩k|=NK|\mathcal{N}_{k}|=\frac{N}{K}, and the number of subarrays, KK, is large such that 1/K01/K\approx 0.

  • A3:

    The interval between the array elements within a subarray is small relative to the whole distributed array, i.e., a subarray can be approximated as a point in the geometry. Particularly, assume φnφ¯k\varphi_{n}\approx\bar{\varphi}_{k} for n𝒩kn\in\mathcal{N}_{k}, such that

    1|𝒩k|n𝒩kf(φn)g(ejΔωφn)f(φ¯k)g(Q0k),\displaystyle\frac{1}{|\mathcal{N}_{k}|}\sum_{n\in\mathcal{N}_{k}}f(\varphi_{n})\cdot g(e^{j\Delta\omega\varphi_{n}})\approx f(\bar{\varphi}_{k})\cdot g(Q_{0}^{k}), (16)

    where

    Q0k=n𝒩kejΔωφn|𝒩k|,\displaystyle Q_{0}^{k}=\frac{\sum_{n\in\mathcal{N}_{k}}e^{j\Delta\omega\varphi_{n}}}{|\mathcal{N}_{k}|}, (17)

    and f(),g()f(\cdot),g(\cdot) are any general polynomial functions.

Refer to caption
Figure 3: Assumptions A1-A3 in partly calibrated arrays.

In Assumption A1, we mainly consider the case L=2L=2 to simplify the expressions. In Assumption A2, uniformly distributed subarrays are common in practice. Note that Assumption 2 can be extended to more general cases, such as the case where the inter-subarray position errors are bounded instead of being distributed on the whole array aperture. These proofs are similar and we take Assumption A2 for example in this paper. In Assumption A3, we consider that the apertures of the subarrays, dkφn¯k+1φn¯k+1,k=1,,Kd_{k}\equiv\varphi_{\bar{n}_{k+1}}-\varphi_{\bar{n}_{k}+1},k=1,\dots,K, are far less than the whole distributed array aperture DD, such that a subarray can be viewed as a point geometrically, i.e., φnφ¯k\varphi_{n}\approx\bar{\varphi}_{k} for n𝒩kn\in\mathcal{N}_{k}. In an extreme case, substituting φn=φ¯k\varphi_{n}=\bar{\varphi}_{k} for n𝒩kn\in\mathcal{N}_{k} to (16) yields the corresponding equation. Therefore, closer intra-subarray displacements between φn,n𝒩k\varphi_{n},n\in\mathcal{N}_{k} implies smaller approximation errors in (16). This means that assumption A3 actually corresponds to a large, sparsely distributed array sensor network, which is usually used for high angular resolution.

V-B Proof of Proposition 2

The proof of Proposition 2 is not direct due to the complex form of CRBPC{\rm CRB}_{\rm PC} w.r.t. Δω\Delta\omega. We then introduce intermediate variables w.r.t. Δω\Delta\omega, denoted by Q(Δω)Q(\Delta\omega). We divide the proof of Proposition 2 into several tractable lemmas. In the sequel, we first introduce the intermediate variables QQ and the lemmas, and then show how Proposition 2 is proved with these lemmas.

The intermediate variables QQ are defined as

Qi(Δω)\displaystyle Q_{i}(\Delta\omega) =n=1NφniejΔωφn/n=1Nφni,\displaystyle=\sum_{n=1}^{N}\varphi_{n}^{i}\cdot e^{j\Delta\omega\varphi_{n}}\bigg{/}\sum_{n=1}^{N}\varphi_{n}^{i}, (18)
Qik(Δω)\displaystyle Q_{i}^{k}(\Delta\omega) =n𝒩kφniejΔωφn/n𝒩kφni,\displaystyle=\sum_{n\in\mathcal{N}_{k}}\varphi_{n}^{i}\cdot e^{j\Delta\omega\varphi_{n}}\bigg{/}\sum_{n\in\mathcal{N}_{k}}\varphi_{n}^{i}, (19)

where i=0,1,2i=0,1,2 and k=1,,Kk=1,\dots,K. In the sequel, we abbreviate Qi(Δω)Q_{i}(\Delta\omega) and Qik(Δω)Q_{i}^{k}(\Delta\omega) as QiQ_{i} and QikQ_{i}^{k}, respectively. The intermediate variables QiQ_{i} correspond to the whole distributed array, and QikQ_{i}^{k} correspond to the kk-th subarray. Our theoretical results are mainly about QiQ_{i}, while QikQ_{i}^{k} are used for intermediate derivations. These intermediate variables are all bounded by 1. Abandoning extreme scenarios (ejΔωφn=1,n=1,,Ne^{j\Delta\omega\varphi_{n}}=1,\ n=1,\dots,N), we assume

|Qi|<1,|Qik|<1.\displaystyle|Q_{i}|<1,\ |Q_{i}^{k}|<1. (20)

With the help of QQ, we rewrite the CRB w.r.t. QQ instead of Δω\Delta\omega, facilitating the analysis of the plateau phase. This is feasible because the proof of Lemma 2 and 3 is equivalent to that of Proposition 2:

Proposition2Lemma2+Lemma3,\displaystyle{\rm Proposition}\ \ref{prop:prop_CRB_approx2}\Longleftrightarrow{\rm Lemma}\ \ref{lemma:Q}+{\rm Lemma}\ \ref{lemma:PC},

and the lemmas are shown as follows. Lemma 2 shows that the intermediate variables QQ and their derivatives w.r.t. Δω\Delta\omega tend to be zero when ΔωΩ\Delta\omega\geqslant\Omega. The approximation to zero in Lemma 2 is a rough but intuitive expression, and the more rigorous expression is shown in the proof. Lemma 3 means that the main influence of Δω\Delta\omega on CRBPC{\rm CRB}_{\rm PC} is embodied by Q(Δω)Q(\Delta\omega), which supports the analysis of how Q(Δω)Q(\Delta\omega) affects CRBPC{\rm CRB}_{\rm PC} instead.

Lemma 2.

Under assumptions A1-A3, when ΔωΩ\Delta\omega\geqslant\Omega, we have

|Q(Δω)|0,|Q(Δω)Δω|0.\displaystyle\left|Q(\Delta\omega)\right|\approx 0,\ \left|\frac{\partial Q(\Delta\omega)}{\partial\Delta\omega}\right|\approx 0. (21)
Proof.

See Appendix C. ∎

Here we give an intuitive explanation of how |Q(Δω)||Q(\Delta\omega)| is close to 0 in Lemma 2. From Lemma 2. 1 in Appendix C, when t=0.25t=0.25, ΔωD=2π\Delta\omega D=2\pi and N=200N=200, we have

P(|Q0|0.35)0.0077.\displaystyle P\left(|Q_{0}|\geqslant 0.35\right)\leqslant 0.0077. (22)

The above conclusion can be extended to the cases of ΔωD2π\Delta\omega D\geqslant 2\pi. Therefore, when NN is large enough, we have |Q(Δω)|0|Q(\Delta\omega)|\approx 0 with high probability, yielding that Proposition 2 also holds with high probability.

Lemma 3.

Under assumptions A1-A3, when ΔωΩ\Delta\omega\geqslant\Omega, we have

CRBPC(Δω)CRBPC(Q(pΔω)),\displaystyle{\rm CRB}_{\rm PC}(\Delta\omega)\approx{\rm CRB}_{\rm PC}(Q(p\Delta\omega)), (23)

where |p|1,p|p|\geqslant 1,p\in\mathbb{Z}.

Proof.

See Appendix D. ∎

Based on the chain rule of partial derivatives, we have

CRBPC(Δω)Δω=CRBPC(Δω)Q(pΔω)Q(pΔω)Δω.\displaystyle\frac{\partial{\rm CRB}_{\rm PC}(\Delta\omega)}{\partial\Delta\omega}=\frac{\partial{\rm CRB}_{\rm PC}(\Delta\omega)}{\partial Q(p\Delta\omega)}\cdot\frac{\partial Q(p\Delta\omega)}{\partial\Delta\omega}. (24)

Substituting CRBPC(Δω)CRBPC(Q(pΔω)){\rm CRB}_{\rm PC}(\Delta\omega)\approx{\rm CRB}_{\rm PC}(Q(p\Delta\omega)) in Lemma 3 to (24) yields that

CRBPC(Δω)ΔωCRBPC(Q(pΔω))Q(pΔω)pQ(pΔω)pΔω.\displaystyle\frac{\partial{\rm CRB}_{\rm PC}(\Delta\omega)}{\partial\Delta\omega}\approx\frac{\partial{\rm CRB}_{\rm PC}(Q(p\Delta\omega))}{\partial Q(p\Delta\omega)}\cdot p\frac{\partial Q(p\Delta\omega)}{\partial p\Delta\omega}. (25)

Under assumptions A1-A3, the Fisher information matrix (FIM) of CRB is not singular, yielding |CRBPC(Q(pΔω))Q(pΔω)|C\left|\frac{\partial{\rm CRB}_{\rm PC}(Q(p\Delta\omega))}{\partial Q(p\Delta\omega)}\right|\leqslant C, where CC is some constant. Based on Lemma 2, we have |Q(pΔω)/pΔω|0\left|\partial Q(p\Delta\omega)/\partial p\Delta\omega\right|\approx 0 when ΔωΩ/p\Delta\omega\geqslant\Omega/p, which is also satisfied for ΔωΩ\Delta\omega\geqslant\Omega since |p|1|p|\geqslant 1. Therefore, when ΔωΩ\Delta\omega\geqslant\Omega we have

|CRBPC(Δω)Δω|0,\displaystyle\left|\frac{\partial{\rm CRB}_{\rm PC}(\Delta\omega)}{\partial\Delta\omega}\right|\approx 0, (26)

completing the proof.

V-C Proof of Proposition 3

The proof of Proposition 3 is similar to the counterpart of Proposition 2, except that Lemma 3 is replaced by Lemma 4, given by:

Proposition3Lemma2+Lemma4,\displaystyle{\rm Proposition}\ \ref{prop:prop_CRB_approx1}\Longleftrightarrow{\rm Lemma}~{}\ref{lemma:Q}+{\rm Lemma}~{}\ref{lemma:FC},

where Lemma 4 demonstrates that the main influence of Δω\Delta\omega on CRBFC{\rm CRB}_{\rm FC} is embodied by Q(Δω)Q(\Delta\omega):

Lemma 4.

Under assumptions A1-A3, when ΔωΩ\Delta\omega\geqslant\Omega, we have

CRBFC(Δω)=CRBFC(Q(Δω)).\displaystyle{\rm CRB}_{\rm FC}(\Delta\omega)={\rm CRB}_{\rm FC}(Q(\Delta\omega)). (27)
Proof.

See Appendix E. ∎

Combining Lemma 2 and 4 yields Proposition 3. The proof is the same as the counterpart of Proposition 2 and is thus omitted here.

V-D Determining the turning point of CRB

We explain how to determine the turning of CRB. From the above propositions, we know that when ΔωΩ\Delta\omega\ll\Omega, CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} decline rapidly as Δω\Delta\omega increases, and plateau out when ΔωΩ\Delta\omega\geqslant\Omega. A criterion is in demand to distinguish the plateau phase and the declining phase in a strict sense, which implies the turning point of CRB.

As the CRB curve has the identical trend with the intermediate variables Q(Δω)Q(\Delta\omega), by observing the structure of Q(Δω)Q(\Delta\omega) defined in (18), we use the criterion

ΔωφN>2π\Delta\omega\varphi_{N}>2\pi (28)

to determine the turning point of CRB. Consequently, the turning point is located at

Δω=2π/φN=Ω.\Delta\omega=2\pi/\varphi_{N}=\Omega. (29)

This criterion is inspired by [35], which considers a similar problem that distinguishes the correlated and uncorrelated signals, detailed as follows: Denote the correlation of two signals by E(Δf)E(\Delta f),

E(Δf)=1ΔxΔx2Δx2ejΔfx𝑑x,\displaystyle E(\Delta f)=\frac{1}{\Delta x}\int_{-\frac{\Delta x}{2}}^{\frac{\Delta x}{2}}e^{-j\Delta fx}dx, (30)

where Δf\Delta f is the frequency difference between two signals. The signals are regarded as correlated if E(Δf)E(\Delta f) is close to 1 or regarded as uncorrelated if E(Δf)E(\Delta f) approaches 0. In [35], it is explained that a sufficient condition for |E(Δf)||E(\Delta f)| to be much less than one is that the integrand completes at least one cycle or equivalently

ΔfΔx>2π.\displaystyle\Delta f\Delta x>2\pi. (31)

We use the similarity between Q(Δω)Q(\Delta\omega) in (18) and E(Δf)E(\Delta f) in (30) and determine the turning point of CRB as (29).

Finally, we give an intuitive explanation of this criterion applied in Q(Δω)Q(\Delta\omega). Take Q0=n=1NejΔωφn/NQ_{0}=\sum_{n=1}^{N}e^{j\Delta\omega\varphi_{n}}/N as an example. When ΔωΩ\Delta\omega\ll\Omega, we have ΔωφN2π\Delta\omega\varphi_{N}\ll 2\pi, which means that the phases of ejΔωφne^{j\Delta\omega\varphi_{n}} are centralized in a small range of [0,2π)[0,2\pi), yielding large |Q0||Q_{0}|. When ΔωΩ\Delta\omega\geqslant\Omega, we have ΔωφN2π\Delta\omega\varphi_{N}\geqslant 2\pi, which means that the phases of ejΔωφne^{j\Delta\omega\varphi_{n}} are distributed in [0,2π)[0,2\pi) and vectors in different directions cancel each other, yielding small |Q0||Q_{0}|. A diagram w.r.t. the phases of ejΔωφne^{j\Delta\omega\varphi_{n}} and Q0Q_{0} is shown in Fig. 4 Since Q1,Q2Q_{1},Q_{2} are the weighted extension of Q0Q_{0}, they also approximately have the above characteristics.

Refer to caption
(a) ΔωΩ\Delta\omega\ll\Omega.
Refer to caption
(b) ΔωΩ\Delta\omega\geqslant\Omega.
Figure 4: The phases of ejΔωφne^{j\Delta\omega\varphi_{n}} and Q0Q_{0}.

VI Simulations

In this section, we first show the declining and plateau phases of CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} by the simulation results in Subsection VI-A, supporting the CRB analysis in Section IV. We present that the turning points of CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} are not sensitive to SNR in Subsection VI-B. We then give the approximation errors in the proof of Lemma 3 in Subsection VI-C to verify the feasibility of the approximation. Finally, we explain that high angular resolution is achievable for both fully and partly calibrated arrays by subspace based algorithms in Subsection VI-D, verifying our main conclusion.

VI-A Verification of the CRB analysis in Section IV

We show the declining and plateau phases of CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} w.r.t. Δω\Delta\omega by simulations to verify the theoretical analysis of CRB in Section IV.

Consider K=10K=10 half-wavelength uniform linear subarrays, each composed of 10 elements, yielding N=100N=100. These subarrays are uniformly spaced on a straight line with ξk=I(k1)λ\xi_{k}=I(k-1)\lambda for k=1,,Kk=1,\dots,K, where I>0I>0 reflects the size of interval between subarrays and is set as I=50I=50. The wavelength of the received signals is λ=1m\lambda=1m, and the resolution limit of 𝝎\bm{\omega} is thus Ω=0.014m1\Omega=0.014{\rm m}^{-1}. The geometry of the distributed array is shown in Fig. 5.

Refer to caption
Figure 5: The geometry of distributed arrays.

The directions 𝜽\bm{\theta} are uniformly in the range of [θmin,θmax][\theta_{\min},\theta_{\max}], i.e., θl=θmin+(l1)(θmaxθmin)/(L1)\theta_{l}=\theta_{\min}+(l-1)(\theta_{\max}-\theta_{\min})/(L-1) for l=1,,Ll=1,\dots,L. In this case, we have Δω=2π(sin(θmax)sin(θmin))/λ\Delta\omega=2\pi(\sin(\theta_{\max})-\sin(\theta_{\min}))/\lambda, and Δω/(L1)\Delta\omega/(L-1) denotes the minimum separation between sources. We set θmin=1.2\theta_{\min}=1.2^{\circ}. The complex coefficients 𝒔\bm{s} are set as sl=ejπ/5s_{l}=e^{j\pi/5} for l=1,,Ll=1,\dots,L. The SNR is defined as 1/σ21/\sigma^{2} being 20dB. We consider L=2,3,4L=2,3,4, and show CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} w.r.t. (Δω/(L1))/Ω(\Delta\omega/(L-1))/\Omega with a logarithmic coordinate in Fig. 6.

Refer to caption
Figure 6: CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} w.r.t. (Δω/(L1))/Ω(\Delta\omega/(L-1))/\Omega for L=2,3,4L=2,3,4.

From Fig. 6, when Δω/(L1)Ω\Delta\omega/(L-1)\ll\Omega, we find that the slopes of CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} w.r.t. Δω\Delta\omega in the L=2,3,4L=2,3,4 cases are close to 2,4,6-2,-4,-6 in the logarithmic coordinate, respectively. This verifies the conclusions in Lemma 1 and Proposition 1 that CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} are mainly proportional to (Δω)2(L1)(\Delta\omega)^{-2(L-1)} when ΔωΩ\Delta\omega\ll\Omega, which correspond to the declining phase of CRB. When Δω/(L1)Ω\Delta\omega/(L-1)\geqslant\Omega, we find that CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} both begin to plateau out w.r.t. Δω\Delta\omega. This verifies the conclusions in Proposition 2 and Proposition 3, which correspond to the plateau phase of CRB.

Note that there is a fluctuation of CRB near the turning point, which is a common phenomenon in the CRB based resolution criterion. An intuitive reason is that the CRB involving the inverse of matrix usually has a complex form w.r.t. Δω\Delta\omega, particularly when Δω\Delta\omega is close to the resolution limit Ω\Omega. Based on the theoretical analysis method proposed in this paper, we can also give a more convincing explanation on this phenomenon. Particularly, from the discussion in Subsection V-B and Subsection V-C, we transform the analysis of CRB(Δω)/Δω\partial{\rm CRB}(\Delta\omega)/\partial\Delta\omega into that of Q(Δω)/Δω\partial Q(\Delta\omega)/\partial\Delta\omega. We take Q0Q_{0} as an example and statistically analyze the how Q0(Δω)Q_{0}(\Delta\omega) varies with Δω\Delta\omega. Based on the A1-A3 assumptions, we calculate the expectations of Q0Q_{0} as follows.

|𝔼Q0|\displaystyle|\mathbb{E}_{Q_{0}}| =|sin(ΔωD/2)ΔωD/2|.\displaystyle=\left|\frac{\sin(\Delta\omega D/2)}{\Delta\omega D/2}\right|. (32)

This is a sinc function, where the most significant change of is reflected near ΔωD/2=π\Delta\omega D/2=\pi, corresponding to the resolution cell Δω=Ω\Delta\omega=\Omega. Since our study indicates that Δω\Delta\omega primarily influences the CRB in the form of Q(Δω)Q(\Delta\omega), the significant variation of Q(Δω)Q(\Delta\omega) near Ω\Omega indirectly results in the rapid fluctuation of CRB(Δω){\rm CRB}(\Delta\omega) around Ω\Omega.

VI-B Verification of CRB turning point’s low sensitivity to SNR

We show the turning points of CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} in different SNRs to explain that the proposed resolution criterion is not sensitive to noise.

Consider the same simulation setting as Subsection VI-A except L=3L=3. We plot the CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} curves for SNR being 1010, 2020, and 3030 dB, shown as Fig. 7. From Fig. 7, we find that the curves of CRBPC{\rm CRB}_{\rm PC} in different SNRs have the same shapes, as well as the turning points. How the noise affects the CRB reflects on the absolute values of CRB, instead of the relative relationship between CRB and Δω\Delta\omega. This verifies that the proposed resolution criterion using the CRB turning point is not sensitive to SNR in Subsection IV-A.

Refer to caption
Figure 7: CRBFC{\rm CRB}_{\rm FC} and CRBPC{\rm CRB}_{\rm PC} w.r.t. (Δω/(L1))/Ω(\Delta\omega/(L-1))/\Omega for different SNRs when L=3L=3.

VI-C Verification of the approximation in Lemma 3

Since 𝑴𝑮1𝑴T\bm{M}\bm{G}^{-1}\bm{M}^{T} is the main component of CRBPC{\rm CRB}_{\rm PC} different from CRBFC{\rm CRB}_{\rm FC}, we show its approximation errors in the proof of Lemma 3. Particularly, we compare the approximate 𝑴𝑮1𝑴T\bm{M}\bm{G}^{-1}\bm{M}^{T} with the true counterpart.

Consider the same simulation setting as Subsection VI-A except L=2L=2. We take the (1,1) entries of the true and approximate 𝑴𝑮1𝑴T\bm{M}\bm{G}^{-1}\bm{M}^{T} as an example, and the comparison is shown in Fig. 8. From Fig. 8, we find that the approximation errors are large when Δω<Ω\Delta\omega<\Omega, and become small when ΔωΩ\Delta\omega\geqslant\Omega. This is because in the proof of Lemma 3, we use |Q(Δω)|0|Q(\Delta\omega)|\approx 0 in Lemma 2 to simplify the proof. This conclusion is feasible for ΔωΩ\Delta\omega\geqslant\Omega, but not for Δω<Ω\Delta\omega<\Omega. When ΔωΩ\Delta\omega\geqslant\Omega, the approximation results are close to the true values, yielding the feasibility of the approximation.

Refer to caption
Figure 8: The approximation performance of [𝑴𝑮1𝑴T]1,1[\bm{M}\bm{G}^{-1}\bm{M}^{T}]_{1,1}.

VI-D Similar angular resolution between fully and partly calibrated arrays

We show that the angular resolution of fully and partly calibrated arrays is similar, which is achieved by comparing the upper resolution limit of the corresponding direction-finding algorithms. Particularly, we provide the estimation accuracy of these algorithms varying with the source separation, and regard the turning point where the estimation accuracy initially tends to plateau out as the resolution limit. For fair comparison, the directions are estimated using Multiple Signal Classification (MUSIC) [38] for fully calibrated arrays, and root-RARE [4], spectral-RARE [5], and ESPRIT-GP [16] for partly calibrated arrays, since these algorithms are all based on subspace separation techniques with the difference being whether errors exist.

Consider the same simulation settings as Subsection VI-A except L=2L=2, the complex coefficients 𝒔\bm{s} being standard Gaussian variables and the number of snapshots being T=50T=50. We use the root mean square error (RMSE) of Δω\Delta\omega to indicate the estimation performance of directions. We carry out Tm=300T_{m}=300 Monte Carlo trials and denote the RMSE of 𝝎\bm{\omega} by

RMSE(𝝎)=1Tmt=1Tm𝝎^t𝝎22,{\rm RMSE}(\bm{\omega})=\sqrt{\frac{1}{T_{m}}\sum_{t=1}^{T_{m}}\left\|\hat{\bm{\omega}}_{t}-\bm{\omega}^{*}\right\|_{2}^{2}}, (33)

where 𝝎^t\hat{\bm{\omega}}_{t} is the estimate in the tt-th trial and 𝝎\bm{\omega}^{*} is the true value. The estimation results of MUSIC for fully calibrated arrays and root-RARE, spectral-RARE, and ESPRIT-GP for partly calibrated arrays w.r.t. Δω\Delta\omega are shown in Fig. 9.

Refer to caption
(a) Partly calibrated case.
Refer to caption
(b) Fully calibrated case.
Figure 9: The RMSE of 𝝎\bm{\omega} w.r.t. Δω\Delta\omega in fully and partly calibrated arrays.

From Fig. 9(a), we find that when ΔωΩ\Delta\omega\leqslant\Omega, the RMSEs of root-RARE, spectral-RARE, and ESPRIT-GP decline as Δω\Delta\omega increases; when Δω>Ω\Delta\omega>\Omega, the RMSEs tend to be stable. Similar phenomenon is found in the fully calibrated case in Fig. 9(b), yielding that the resolution limit of these algorithms is close to Ω\Omega. This also heuristically indicates that the resolution limit of fully and partly calibrated arrays is similar, both close to Ω\Omega, corresponding to our main conclusion. We note that the turning points of the RMSEs w.r.t. Δω\Delta\omega in Fig. 9 are not exactly located at Ω\Omega since Ω\Omega is an empirical bound and the subspace based algorithms have super-resolution ability.

Then, we construct the dependence of the resolution probability for the RARE/ESPRIT methods in partly calibrated arrays and MUSIC method in fully calibrated arrays. Particularly, we define the resolution probability PtP_{t} as the probability that the estimation error is less than a threshold, given by

Pt=TpTm,\displaystyle P_{t}=\frac{T_{p}}{T_{m}}, (34)

where TpT_{p} is the number of trials in which the estimation error is less than 13-13dB for partly calibrated case and 30-30dB for fully calibrated case, respectively, and the thresholds are empirically chosen based on the corresponding CRBs. The resolution probability of RARE/ESPRIT and MUSIC is shown as Fig. 10, which also verifies that the angular resolution between fully and partly calibrated arrays is similar.

Refer to caption
(a) Partly calibrated case.
Refer to caption
(b) Fully calibrated case.
Figure 10: The resolution probability in fully and partly calibrated arrays.

VII Conclusion

In this paper, we theoretically explain that partly calibrated arrays achieve similar angular resolution as fully calibrated arrays, both inversely proportional to the whole array aperture. The analysis is based on a characteristics of CRB that when the source separation Δω\Delta\omega increases, the CRB w.r.t Δω\Delta\omega first declines rapidly, then plateaus out, and the turning point is close to the angular resolution limit. Hence, we transform the angular resolution analysis into comparing the turning points of the CRBs of fully and partly calibrated arrays, where the key technique lies in the partial derivative of CRB w.r.t. Δω\Delta\omega. To this end, we introduce some intermediate variables to simplify the analysis and theoretically explain the declining and plateau phases of the CRB. This work provides an important theoretical guarantee for the high-resolution performance of distributed arrays in mobile platforms. We believe that the proposed method to analyze the impact of position errors on resolution in distributed arrays using CRB turning points can be applied to other types of errors, such as gain and phase errors. This is theoretically feasible, but its specific implementation requires further research.

Appendix A Calculation of CRB

The CRBs of spatial frequencies 𝝎\bm{\omega} using fully and partly calibrated arrays, denoted by CRBFC(𝝎){\rm CRB}_{\rm FC}(\bm{\omega}) and CRBPC(𝝎){\rm CRB}_{\rm PC}(\bm{\omega}), respectively, are given by [4],

CRBFC(𝝎)\displaystyle{\rm CRB}_{\rm FC}(\bm{\omega}) =σ22𝑭1,\displaystyle=\frac{\sigma^{2}}{2}\bm{F}^{-1}, (35)
CRBPC(𝝎)\displaystyle{\rm CRB}_{\rm PC}(\bm{\omega}) =σ22(𝑭𝑴𝑮1𝑴T)1,\displaystyle=\frac{\sigma^{2}}{2}(\bm{F}-\bm{M}\bm{G}^{-1}\bm{M}^{T})^{-1}, (36)

where

𝑭\displaystyle\bm{F} =i=1TRe{𝑫iH𝚷𝑨𝑫i},\displaystyle=\sum_{i=1}^{T}{\rm Re}\left\{\bm{D}_{i}^{H}\bm{\Pi}_{\bm{A}}^{\perp}\bm{D}_{i}\right\}, (37)
𝑴\displaystyle\bm{M} =i=1TRe{𝑫iH𝚷𝑨𝑯i},\displaystyle=\sum_{i=1}^{T}{\rm Re}\left\{\bm{D}_{i}^{H}\bm{\Pi}_{\bm{A}}^{\perp}\bm{H}_{i}\right\}, (38)
𝑮\displaystyle\bm{G} =i=1TRe{𝑯iH𝚷𝑨𝑯i},\displaystyle=\sum_{i=1}^{T}{\rm Re}\left\{\bm{H}_{i}^{H}\bm{\Pi}_{\bm{A}}^{\perp}\bm{H}_{i}\right\}, (39)
𝚷𝑨\displaystyle\bm{\Pi}_{\bm{A}}^{\perp} =𝑰𝑨(𝑨H𝑨)1𝑨H,\displaystyle=\bm{I}-\bm{A}(\bm{A}^{H}\bm{A})^{-1}\bm{A}^{H}, (40)
𝑫i\displaystyle\bm{D}_{i} =[𝒂(ω1)ω1s1(ti),,𝒂(ωL)ωLsL(ti)],\displaystyle=\left[\frac{\partial\bm{a}(\omega_{1})}{\partial\omega_{1}}s_{1}(t_{i}),\dots,\frac{\partial\bm{a}(\omega_{L})}{\partial\omega_{L}}s_{L}(t_{i})\right], (41)
𝒂(ω)ω\displaystyle\frac{\partial\bm{a}(\omega)}{\partial\omega} =j[φ1ejωφ1,,φNejωφN]T,\displaystyle=j\cdot\left[\varphi_{1}e^{j\omega\varphi_{1}},\dots,\varphi_{N}e^{j\omega\varphi_{N}}\right]^{T}, (42)
𝑯i\displaystyle\bm{H}_{i} =[𝟎𝟎𝑩~𝝃,i2𝟎𝟎𝑩~𝝃,iK],\displaystyle=\begin{bmatrix}\bm{0}&&\bm{0}\\ \widetilde{\bm{B}}_{\bm{\xi},i}^{2}&&\bm{0}\\ &\ddots&\\ \bm{0}&&\widetilde{\bm{B}}_{\bm{\xi},i}^{K}\end{bmatrix}, (43)
𝑩~𝝃,ik\displaystyle\widetilde{\bm{B}}_{\bm{\xi},i}^{k} =jl=1Lsl(ti)ωl𝒂k(ωl).\displaystyle=j\cdot\sum_{l=1}^{L}\ s_{l}(t_{i})\cdot\omega_{l}\cdot\bm{a}_{k}(\omega_{l}). (44)

We consider the single-snapshot case and omit ii since the multiple-snapshot cases (T>1T>1) is a direct extension to those in the single-snapshot cases (T=1T=1).

Appendix B Proof of Proposition 1

The proof of Proposition 1 is an extension of Lemma 1 [25] from fully calibrated arrays to partly calibrated arrays. The main difference lies in the small quantity approximation of the matrix 𝑴𝑮1𝑴T\bm{M}\bm{G}^{-1}\bm{M}^{T} in (36).

Particularly, denote Δωl=ωlω1\Delta\omega_{l}=\omega_{l}-\omega_{1} for l=1,,Ll=1,\dots,L and ΔωΔωL=ωLω1\Delta\omega\equiv\Delta\omega_{L}=\omega_{L}-\omega_{1}. When ΔωΩ\Delta\omega\ll\Omega, we carry out Taylor expansion of 𝒂k(ω)\bm{a}_{k}(\omega) in (44) on ω=ω1\omega=\omega_{1} as

𝒂k(ωl)\displaystyle\bm{a}_{k}(\omega_{l}) =𝒂k(ω1)+𝒂k(1)(ω1)Δωl+𝒂k(2)(ω1)Δωl22!+,\displaystyle=\bm{a}_{k}(\omega_{1})+\bm{a}_{k}^{(1)}(\omega_{1})\Delta\omega_{l}+\bm{a}_{k}^{(2)}(\omega_{1})\frac{\Delta\omega_{l}^{2}}{2!}+\cdots,
=𝒂k(ω1)+𝒂~k(1)(ω1)Δω+𝒂~k(2)(ω1)Δω22!+,\displaystyle=\bm{a}_{k}(\omega_{1})+\tilde{\bm{a}}_{k}^{(1)}(\omega_{1})\Delta\omega+\tilde{\bm{a}}_{k}^{(2)}(\omega_{1})\frac{\Delta\omega^{2}}{2!}+\cdots, (45)

where 𝒂~k(p)(ω0)𝒂k(p)(ω0)(Δωl/Δω)p\tilde{\bm{a}}_{k}^{(p)}(\omega_{0})\equiv\bm{a}_{k}^{(p)}(\omega_{0})\cdot(\Delta\omega_{l}/\Delta\omega)^{p} and ()(p)(\cdot)^{(p)} denotes the pp-order derivative of \cdot for p=1,2,p=1,2,\dots. By substituting (B) to (44), we have

𝑩~𝝃k=𝒄ξk+O(Δω),\displaystyle\widetilde{\bm{B}}_{\bm{\xi}}^{k}=\bm{c}_{\xi}^{k}+O(\Delta\omega), (46)

where 𝒄ξkjl=1Lslω1𝒂k(ω1)\bm{c}_{\xi}^{k}\equiv j\cdot\sum_{l=1}^{L}\ s_{l}\cdot\omega_{1}\cdot\bm{a}_{k}(\omega_{1}).

From the proof of Lemma 1 [25], 𝑫\bm{D} in (41) and 𝚷𝑨\bm{\Pi}_{\bm{A}}^{\perp} in (40) w.r.t. Δω\Delta\omega are expressed as follows:

𝑫\displaystyle\bm{D} =(Δω)L1𝑪D+O((Δω)L),\displaystyle=(\Delta\omega)^{L-1}\bm{C}_{D}+O((\Delta\omega)^{L}), (47)
𝚷𝑨\displaystyle\bm{\Pi}_{\bm{A}}^{\perp} =𝑪A+O(Δω),\displaystyle=\bm{C}_{A}+O(\Delta\omega), (48)

where 𝑪D\bm{C}_{D} and 𝑪A\bm{C}_{A} are constants w.r.t. Δω\Delta\omega. Since 𝚷𝑨\bm{\Pi}_{\bm{A}}^{\perp} in (40) is a symmetric projection matrix satisfying 𝚷𝑨=(𝚷𝑨)H=𝚷𝑨𝚷𝑨\bm{\Pi}_{\bm{A}}^{\perp}=(\bm{\Pi}_{\bm{A}}^{\perp})^{H}=\bm{\Pi}_{\bm{A}}^{\perp}\bm{\Pi}_{\bm{A}}^{\perp}, we rewrite 𝑴\bm{M} in (38) and 𝑮\bm{G} in (39) respectively as

𝑴\displaystyle\bm{M} =𝑫H𝚷𝑨𝑯=(𝚷𝑨𝑫)H𝚷𝑨𝑯,\displaystyle=\bm{D}^{H}\bm{\Pi}_{\bm{A}}^{\perp}\bm{H}=(\bm{\Pi}_{\bm{A}}^{\perp}\bm{D})^{H}\bm{\Pi}_{\bm{A}}^{\perp}\bm{H}, (49)
𝑮\displaystyle\bm{G} =𝑯H𝚷𝑨𝑯=(𝚷𝑨𝑯)H𝚷𝑨𝑯.\displaystyle=\bm{H}^{H}\bm{\Pi}_{\bm{A}}^{\perp}\bm{H}=(\bm{\Pi}_{\bm{A}}^{\perp}\bm{H})^{H}\bm{\Pi}_{\bm{A}}^{\perp}\bm{H}. (50)

By substituting (43), (48) and (46) to 𝚷𝑨𝑯\bm{\Pi}_{\bm{A}}^{\perp}\bm{H}, we have

𝚷𝑨𝑯=𝑪H+O(Δω),\displaystyle\bm{\Pi}_{\bm{A}}^{\perp}\bm{H}=\bm{C}_{H}+O(\Delta\omega), (51)

and 𝑪H=[𝑪A2𝒄ξ2,,𝑪AK𝒄ξK]\bm{C}_{H}=[\bm{C}_{A}^{2}\bm{c}_{\xi}^{2},\dots,\bm{C}_{A}^{K}\bm{c}_{\xi}^{K}] is a constant w.r.t. Δω\Delta\omega, where 𝑪A=[𝑪A1,,𝑪AK]\bm{C}_{A}=[\bm{C}_{A}^{1},\dots,\bm{C}_{A}^{K}] and 𝑪Ak\bm{C}_{A}^{k} denotes the n𝒩kn\in\mathcal{N}_{k} columns of 𝑪A\bm{C}_{A} for k=1,,Kk=1,\dots,K.

If 𝑪H𝟎\bm{C}_{H}\neq\bm{0} (to be proved later), we substitute (47), (48) and (51) to (49) and (50), and have

𝑴\displaystyle\bm{M} =(Δω)L1Re{𝑪DH𝑪AH𝑪H}+O((Δω)L),\displaystyle=(\Delta\omega)^{L-1}{\rm Re}\{\bm{C}^{H}_{D}\bm{C}_{A}^{H}\bm{C}_{H}\}+O((\Delta\omega)^{L}), (52)
𝑮\displaystyle\bm{G} =Re{(𝑪H+O(Δω))H(𝑪H+O(Δω))},\displaystyle={\rm Re}\left\{(\bm{C}_{H}+O(\Delta\omega))^{H}(\bm{C}_{H}+O(\Delta\omega))\right\}, (53)

yielding that

𝑴𝑮1𝑴T=(Δω)2(L1)𝑪U+O((Δω)2(L1)+1),\displaystyle\bm{M}\bm{G}^{-1}\bm{M}^{T}=(\Delta\omega)^{2(L-1)}\bm{C}_{U}+O((\Delta\omega)^{2(L-1)+1}), (54)

where 𝑪U\bm{C}_{U} is a constant w.r.t. Δω\Delta\omega. Based on (54) and Lemma 1, we have (9) with

𝑪G=σ22(𝑪URe{𝑪DH𝑪A𝑪D})1,\displaystyle\bm{C}_{G}=\frac{\sigma^{2}}{2}\left(\bm{C}_{U}-{\rm Re}\{\bm{C}_{D}^{H}\bm{C}_{A}\bm{C}_{D}\}\right)^{-1}, (55)

completing the proof.

Here we prove that any column of 𝑪H\bm{C}_{H} is not 𝟎\bm{0}, hence 𝑪H𝟎\bm{C}_{H}\neq\bm{0}: Consider if there is one column of 𝑪H\bm{C}_{H} equal to 𝟎\bm{0}. We assume that the 1-st column of 𝑪H\bm{C}_{H} is 𝟎\bm{0} without loss of generality, given by 𝑪A2𝒄ξ2=𝟎\bm{C}_{A}^{2}\bm{c}_{\xi}^{2}=\bm{0}. In this case, we construct the following vector,

𝒂¯=[𝟎T,(𝒄ξ2)T,𝟎T]TN×1,\displaystyle\bar{\bm{a}}=\left[\bm{0}^{T},(\bm{c}_{\xi}^{2})^{T},\bm{0}^{T}\right]^{T}\in\mathbb{C}^{N\times 1}, (56)

such that 𝑪A𝒂¯=𝟎\bm{C}_{A}\bar{\bm{a}}=\bm{0}, where the the first 𝟎|𝒩1|×1\bm{0}\in\mathbb{R}^{|\mathcal{N}_{1}|\times 1}, the second 𝟎(N|𝒩1||𝒩2|)×1\bm{0}\in\mathbb{R}^{(N-|\mathcal{N}_{1}|-|\mathcal{N}_{2}|)\times 1}, and 𝑪A\bm{C}_{A} is expressed as [4]

𝑪A=𝑰𝑨˙(𝑨˙H𝑨˙)1𝑨˙H,\displaystyle\bm{C}_{A}=\bm{I}-\dot{\bm{A}}(\dot{\bm{A}}^{H}\dot{\bm{A}})^{-1}\dot{\bm{A}}^{H}, (57)

with

𝑨˙\displaystyle\dot{\bm{A}} =[𝒂(ω1),𝒂(1)(ω1),,𝒂(L1)(ω1)],\displaystyle=\left[\bm{a}(\omega_{1}),\bm{a}^{(1)}(\omega_{1}),\dots,\bm{a}^{(L-1)}(\omega_{1})\right], (58)
𝒂(l)(ω1)\displaystyle\bm{a}^{(l)}(\omega_{1}) =[lωl𝒂(ω)]ω=ω1.\displaystyle=\left[\frac{\partial^{l}}{\partial\omega^{l}}\bm{a}(\omega)\right]_{\omega=\omega_{1}}. (59)

Since 𝑪A𝒂¯=𝟎\bm{C}_{A}\bar{\bm{a}}=\bm{0} and 𝑪A\bm{C}_{A} in (57) is a projection matrix, 𝒂¯\bar{\bm{a}} should be in the column space of 𝑨˙\dot{\bm{A}}. However, we then explain that 𝒂¯\bar{\bm{a}} could not be in the column space of 𝑨˙\dot{\bm{A}}, i.e., there is no 𝒚L×1\bm{y}\in\mathbb{C}^{L\times 1} such that 𝒂¯=𝑨˙𝒚\bar{\bm{a}}=\dot{\bm{A}}\bm{y}, yielding a contradiction. Particularly, define 𝑨˙=[𝑨˙1T,,𝑨˙KT]T\dot{\bm{A}}=[\dot{\bm{A}}_{1}^{T},\dots,\dot{\bm{A}}_{K}^{T}]^{T} and 𝑨˙k\dot{\bm{A}}_{k} denotes the n𝒩kn\in\mathcal{N}_{k} rows of 𝑨˙\dot{\bm{A}} for k=1,,Kk=1,\dots,K. We find that 𝑨˙1|𝒩1|×L,|𝒩1|>L\dot{\bm{A}}_{1}\in\mathbb{C}^{|\mathcal{N}_{1}|\times L},|\mathcal{N}_{1}|>L has full column rank, given by

𝑨˙1=𝑫A[1jφ1(jφ1)L11jφ|𝒩1|(jφ|𝒩1|)L1],\displaystyle\dot{\bm{A}}_{1}=\bm{D}_{A}\begin{bmatrix}1&j\varphi_{1}&\dots&(j\varphi_{1})^{L-1}\\ &&\vdots&\\ 1&j\varphi_{|\mathcal{N}_{1}|}&\dots&(j\varphi_{|\mathcal{N}_{1}|})^{L-1}\end{bmatrix}, (60)

where 𝑫A=diag([ejω0φ1,,ejω0φ|𝒩1|]T)\bm{D}_{A}={\rm diag}([e^{j\omega_{0}\varphi_{1}},\dots,e^{j\omega_{0}\varphi_{|\mathcal{N}_{1}|}}]^{T}). Therefore, there is no nonzero 𝒚L×1\bm{y}\in\mathbb{C}^{L\times 1} such that [𝑨˙]1𝒚=𝟎[\dot{\bm{A}}]_{1}\bm{y}=\bm{0}, yielding 𝒂¯𝑨˙𝒚\bar{\bm{a}}\neq\dot{\bm{A}}\bm{y} for any nonzero 𝒚L×1\bm{y}\in\mathbb{C}^{L\times 1}. This contradiction implies any column of 𝑪H\bm{C}_{H} is not 𝟎\bm{0} and hence 𝑪H𝟎\bm{C}_{H}\neq\bm{0}.

Appendix C Proof of Lemma 2

Lemma 2 in Subsection V-B is a rough representation, and we introduce its rigorous expression here, given by Lemma 2.1 and Lemma 2.2. For Qi,iQ_{i},i\in\mathbb{N}, we take Q0Q_{0} as an example and the other cases are its direct extension with minor modifications.

For |Q0(Δω)|0|Q_{0}(\Delta\omega)|\approx 0 in Lemma 2, the rigorous expression is as follows:

Lemma 2. 1.

Under assumptions A1-A3, for any t>0t>0, define t1,t2t_{1},t_{2} as

t1\displaystyle t_{1} max{|t+sinΔωDΔωD|,|t+sinΔωDΔωD|},\displaystyle\equiv\max\left\{\left|t+\frac{\sin\Delta\omega D}{\Delta\omega D}\right|,\left|-t+\frac{\sin\Delta\omega D}{\Delta\omega D}\right|\right\}, (61)
t2\displaystyle t_{2} |t+1cosΔωDΔωD|.\displaystyle\equiv\left|t+\frac{1-\cos\Delta\omega D}{\Delta\omega D}\right|. (62)

When ΔωΩ\Delta\omega\geqslant\Omega, we have

P(|Q0|t12+t22)4eNt22.\displaystyle P\left(|Q_{0}|\geqslant\sqrt{t_{1}^{2}+t_{2}^{2}}\right)\leqslant 4e^{-\frac{Nt^{2}}{2}}. (63)
Proof.

First, we rewrite Q0Q_{0} in (18) as

Q0=n=1NcosΔωφn+jn=1NsinΔωφnN.\displaystyle Q_{0}=\frac{\sum_{n=1}^{N}\cos\Delta\omega\varphi_{n}+j\sum_{n=1}^{N}\sin\Delta\omega\varphi_{n}}{N}. (64)

When φn𝒰[0,D]\varphi_{n}\in\mathcal{U}[0,D] in the A2 assumption, we have

𝔼(1Nn=1NcosΔωφn)\displaystyle\mathbb{E}\left(\frac{1}{N}\sum_{n=1}^{N}\cos\Delta\omega\varphi_{n}\right) =sinΔωDΔωD,\displaystyle=\frac{\sin\Delta\omega D}{\Delta\omega D}, (65)
𝔼(1Nn=1NsinΔωφn)\displaystyle\mathbb{E}\left(\frac{1}{N}\sum_{n=1}^{N}\sin\Delta\omega\varphi_{n}\right) =1cosΔωDΔωD.\displaystyle=\frac{1-\cos\Delta\omega D}{\Delta\omega D}. (66)

Through the Hoeffding inequality [39] and some straightforward derivation, we have

P1P(|1Nn=1NcosΔωφn|t1)2eNt22,\displaystyle P_{1}\equiv P\left(\left|\frac{1}{N}\sum_{n=1}^{N}\cos\Delta\omega\varphi_{n}\right|\geqslant t_{1}\right)\leqslant 2e^{-\frac{Nt^{2}}{2}}, (67)
P2P(|1Nn=1NsinΔωφn|t2)2eNt22,\displaystyle P_{2}\equiv P\left(\left|\frac{1}{N}\sum_{n=1}^{N}\sin\Delta\omega\varphi_{n}\right|\geqslant t_{2}\right)\leqslant 2e^{-\frac{Nt^{2}}{2}}, (68)

where t1,t2t_{1},t_{2} are defined in (61) and (62), respectively. For Q0Q_{0} in (64), we have

P(|Q0|t12+t22)P1+P24eNt22,\displaystyle P\left(|Q_{0}|\geqslant\sqrt{t_{1}^{2}+t_{2}^{2}}\right)\leqslant P_{1}+P_{2}\leqslant 4e^{-\frac{Nt^{2}}{2}}, (69)

completing the proof. ∎

For |Q0(Δω)/Δω|0\left|\partial Q_{0}(\Delta\omega)/\partial\Delta\omega\right|\approx 0 in Lemma 2, the rigorous expression is as follows:

Lemma 2. 2.

Under assumptions A1-A3, for any t>0t>0, when ΔωΩ\Delta\omega\geqslant\Omega, we have

P(|Q0(Δω)Δω|n=1NφnNt¯12+t¯22)4eNt22,\displaystyle P\left(\left|\frac{\partial Q_{0}(\Delta\omega)}{\partial\Delta\omega}\right|\geqslant\frac{\sum_{n=1}^{N}\varphi_{n}}{N}\sqrt{\bar{t}_{1}^{2}+\bar{t}_{2}^{2}}\right)\leqslant 4e^{-\frac{Nt^{2}}{2}}, (70)

where t¯1,t¯2\bar{t}_{1},\bar{t}_{2} are calculated for Q1Q_{1} similar with t1,t2t_{1},t_{2} for Q0Q_{0} in Lemma 2. 1.

Proof.

The partial derivative of Q0(Δω)Q_{0}(\Delta\omega) w.r.t. Δω\Delta\omega is

|Q0(Δω)Δω|\displaystyle\left|\frac{\partial Q_{0}(\Delta\omega)}{\partial\Delta\omega}\right| =|n=1NφnejΔωφnN|\displaystyle=\left|\frac{\sum_{n=1}^{N}\varphi_{n}e^{j\Delta\omega\varphi_{n}}}{N}\right|
=n=1NφnN|Q1|,\displaystyle=\frac{\sum_{n=1}^{N}\varphi_{n}}{N}\cdot\left|Q_{1}\right|, (71)

completing the proof. ∎

Appendix D Proof of Lemma 3

CRBPC{\rm CRB}_{\rm PC} in (36) can be divided into 𝑭\bm{F} and 𝑴𝑮1𝑴T\bm{M}\bm{G}^{-1}\bm{M}^{T}. The former is transformed into a function of QiQ_{i} in Lemma 4, and we consider the later one here.

To simply the derivation, we use the approximation |Q0|0|Q_{0}|\approx 0 in Lemma 2, and then substituting (94) to (38) and (39),

𝑴\displaystyle\bm{M} 𝑴~Re{𝑫H𝑯𝑫H𝑨𝑨H𝑯N},\displaystyle\approx\widetilde{\bm{M}}\equiv{\rm Re}\left\{\bm{D}^{H}\bm{H}-\frac{\bm{D}^{H}\bm{A}\bm{A}^{H}\bm{H}}{N}\right\}, (72)
𝑮\displaystyle\bm{G} 𝑮~Re{𝑯H𝑯𝑯H𝑨𝑨H𝑯N},\displaystyle\approx\widetilde{\bm{G}}\equiv{\rm Re}\left\{\bm{H}^{H}\bm{H}-\frac{\bm{H}^{H}\bm{A}\bm{A}^{H}\bm{H}}{N}\right\}, (73)

where 𝑯H𝑯\bm{H}^{H}\bm{H} is a diagonal matrix denoted by 𝑯H𝑯=diag(𝒉)\bm{H}^{H}\bm{H}={\rm diag}(\bm{h}).

Based on |Q1|0|Q_{1}|\approx 0 in Lemma 2 and Q1kQ0kQ_{1}^{k}\approx Q_{0}^{k} in the A3 assumption (let f(x)=g(x)=xf(x)=g(x)=x), by substituting (41) and (43) to (72), we approximate 𝑴\bm{M} as

[𝑴]k1\displaystyle[\bm{M}]_{k-1} [𝑴^]k1\displaystyle\approx[\widehat{\bm{M}}]_{k-1}
γMkω0[|s1|2+|s1s2|s0kμ|s1s2|s0k+|s2|2μ],\displaystyle\equiv\gamma_{M}^{k}\cdot\omega_{0}\cdot\begin{bmatrix}|s_{1}|^{2}+|s_{1}s_{2}|s_{0}^{k}\mu\\ |s_{1}s_{2}|s_{0}^{k}+|s_{2}|^{2}\mu\end{bmatrix}, (74)

where γMk=|𝒩k|(φ¯kφ¯)\gamma_{M}^{k}=|\mathcal{N}_{k}|\cdot(\bar{\varphi}_{k}-\bar{\varphi}), s0k=Re{s1Hs2Q0k}|s1s2|s_{0}^{k}=\frac{{\rm Re}\{s_{1}^{H}s_{2}Q_{0}^{k}\}}{|s_{1}s_{2}|}, μ=1+Δωω0\mu=1+\frac{\Delta\omega}{\omega_{0}} and φ¯=n=1NφnN\bar{\varphi}=\frac{\sum_{n=1}^{N}\varphi_{n}}{N} for k=2,,Kk=2,\dots,K.

Then, we approximate 𝑮1\bm{G}^{-1} by 𝑮^1\widehat{\bm{G}}^{-1}, which is shown in the following lemma:

Lemma 5.

Based on Assumption A2, we have

𝑮1\displaystyle\bm{G}^{-1} 𝑮^1𝑮^1+𝑮^2\displaystyle\approx\widehat{\bm{G}}^{-1}\equiv\widehat{\bm{G}}_{1}+\widehat{\bm{G}}_{2}
=[1B2001Bk]+Re{[𝒃2HB2𝒃KHBK][𝒃2B2𝒃KBK]},\displaystyle=\begin{bmatrix}\frac{1}{B_{2}}&&0\\ &\ddots&\\ 0&&\frac{1}{B_{k}}\end{bmatrix}+{\rm Re}\left\{\begin{bmatrix}\frac{\bm{b}_{2}^{H}}{B_{2}}\\ \vdots\\ \frac{\bm{b}_{K}^{H}}{B_{K}}\end{bmatrix}\begin{bmatrix}\frac{\bm{b}_{2}}{B_{2}}&\cdots&\frac{\bm{b}_{K}}{B_{K}}\end{bmatrix}\right\}, (75)

where Bk=[𝐡]k1>0B_{k}=[\bm{h}]_{k-1}>0 and 𝐛k=1N[𝐀H𝐇]k1\bm{b}_{k}=\frac{1}{\sqrt{N}}[\bm{A}^{H}\bm{H}]_{k-1}.

Proof.

See Appendix F. ∎

Now, we approximate 𝑴𝑮1𝑴T\bm{M}\bm{G}^{-1}\bm{M}^{T} by

𝑴𝑮1𝑴T𝑴^𝑮^1𝑴^T=𝑴^(𝑮^1+𝑮^2)𝑴^T.\displaystyle\bm{M}\bm{G}^{-1}\bm{M}^{T}\approx\widehat{\bm{M}}\widehat{\bm{G}}^{-1}\widehat{\bm{M}}^{T}=\widehat{\bm{M}}(\widehat{\bm{G}}_{1}+\widehat{\bm{G}}_{2})\widehat{\bm{M}}^{T}. (76)

Define 𝒢1=𝑴^𝑮^1𝑴^T\mathcal{G}_{1}=\widehat{\bm{M}}\widehat{\bm{G}}_{1}\widehat{\bm{M}}^{T} and 𝒢2=𝑴^𝑮^2𝑴^T\mathcal{G}_{2}=\widehat{\bm{M}}\widehat{\bm{G}}_{2}\widehat{\bm{M}}^{T}. In the sequel, we discuss how 𝒢1\mathcal{G}_{1} and 𝒢2\mathcal{G}_{2} are recast as functions of QiQ_{i}, respectively. Based on the A1 assumption, L=2L=2 and 𝒢1,𝒢22×2\mathcal{G}_{1},\mathcal{G}_{2}\in\mathbb{R}^{2\times 2}. We take the (1,1)(1,1)-th entry as an example, and the other entries can be directly derived. This is because the rows of 𝑴\bm{M} have similar form, i.e.,

[𝑴]2,k1(s1,s2,μ)=μ[𝑴]1,k1(s2H,s1H,1/μ),\displaystyle[\bm{M}]_{2,k-1}(s_{1},s_{2},\mu)=\mu\cdot[\bm{M}]_{1,k-1}(s_{2}^{H},s_{1}^{H},1/\mu), (77)

for k=2,,Kk=2,\dots,K.

For [𝒢1]1,1[\mathcal{G}_{1}]_{1,1}, substituting (D) and (5) to 𝒢1\mathcal{G}_{1} yields

[𝒢1]1,1=|s1|2k=2K(γMk)2|𝒩k|(1s~(1(s0k)2)μ2s~1+s~μ2+2s0kμ),\displaystyle[\mathcal{G}_{1}]_{1,1}=|s_{1}|^{2}\sum_{k=2}^{K}\frac{(\gamma_{M}^{k})^{2}}{|\mathcal{N}_{k}|}\left(1-\frac{\tilde{s}(1-(s_{0}^{k})^{2})\mu^{2}}{\tilde{s}^{-1}+\tilde{s}\mu^{2}+2s_{0}^{k}\mu}\right), (78)

where s~=|s2/s1|>0\tilde{s}=\left|s_{2}/s_{1}\right|>0. Due to |Q0k|<1|Q_{0}^{k}|<1 in (20), we have |s0k|<1|s_{0}^{k}|<1, yielding that

s~1+s~μ2+2s0kμ>0.\displaystyle\tilde{s}^{-1}+\tilde{s}\mu^{2}+2s_{0}^{k}\mu>0. (79)

Consider the Taylor expansion of 1s~1+s~μ2+2s0kμ\frac{1}{\tilde{s}^{-1}+\tilde{s}\mu^{2}+2s_{0}^{k}\mu} at 2s0kμ=02s_{0}^{k}\mu=0, given by

1s~1+s~μ2+2s0kμ\displaystyle\frac{1}{\tilde{s}^{-1}+\tilde{s}\mu^{2}+2s_{0}^{k}\mu} =p=0(2s0kμ)p(s~1+s~μ2)p+1.\displaystyle=\sum_{p=0}^{\infty}\frac{(-2s_{0}^{k}\mu)^{p}}{(\tilde{s}^{-1}+\tilde{s}\mu^{2})^{p+1}}. (80)

By substituting (80) to (78), we have

[𝒢1]1,1=|s1|2k=2K(γMk)2|𝒩k|(1s~(1(s0k)2)p=0up(s0k)p),\displaystyle[\mathcal{G}_{1}]_{1,1}=|s_{1}|^{2}\sum_{k=2}^{K}\frac{(\gamma_{M}^{k})^{2}}{|\mathcal{N}_{k}|}\left(1-\tilde{s}(1-(s_{0}^{k})^{2})\sum_{p=0}^{\infty}u_{p}(s_{0}^{k})^{p}\right), (81)

where upu_{p} is denoted by

up(μ)=(2)pμp+2(s~1+s~μ2)p+1.\displaystyle u_{p}(\mu)=\frac{(-2)^{p}\mu^{p+2}}{(\tilde{s}^{-1}+\tilde{s}\mu^{2})^{p+1}}. (82)

The effect of Δω\Delta\omega on [𝒢1]1,1[\mathcal{G}_{1}]_{1,1} in (81) is embodied in both s0ks_{0}^{k} and upu_{p}. In the sequel, we explain that upu_{p} is almost constant w.r.t. Δω\Delta\omega, which is detailed in the following lemma.

Lemma 6.

The gradient of upu_{p} w.r.t. μ\mu, up=dupdμu_{p}^{\prime}=\frac{{\rm d}u_{p}}{{\rm d}\mu}, satisfies

1.|up|1,p=0,1,2,3.\displaystyle 1.\ |u_{p}^{\prime}|\leqslant 1,\ p=0,1,2,3. (83)
2.Lim|μ||up|=0,p=0,1,2,.\displaystyle 2.\ \underset{|\mu|\rightarrow\infty}{\rm Lim}\ |u_{p}^{\prime}|=0,\ p=0,1,2,\dots. (84)
Proof.

See Appendix G. ∎

Based on Lemma 6, when ΔωΩ\Delta\omega\geqslant\Omega, we approximate upu_{p} by the constant up(μ¯){u}_{p}(\bar{\mu}), where μ¯μ(Ω)=1+Ωω0\bar{\mu}\equiv\mu(\Omega)=1+\frac{\Omega}{\omega_{0}}. Since |s0k|<1|s_{0}^{k}|<1, we ignore the high-order terms of (s0k)p(s_{0}^{k})^{p} and approximate the infinite summation in (81) by its p=0,1,2,3p=0,1,2,3 terms as

[𝒢1]1,1\displaystyle[\mathcal{G}_{1}]_{1,1} |s1|2k=2K(γMk)2|𝒩k|(1s~(1(s0k)2)p=03u¯p(s0k)p)\displaystyle\approx|s_{1}|^{2}\sum_{k=2}^{K}\frac{(\gamma_{M}^{k})^{2}}{|\mathcal{N}_{k}|}\left(1-\tilde{s}(1-(s_{0}^{k})^{2})\sum_{p=0}^{3}\bar{u}_{p}(s_{0}^{k})^{p}\right)
=k=2K(γMk)2|𝒩k|(p=05vp(s0k)p),\displaystyle=\sum_{k=2}^{K}\frac{(\gamma_{M}^{k})^{2}}{|\mathcal{N}_{k}|}\left(\sum_{p=0}^{5}v_{p}(s_{0}^{k})^{p}\right), (85)

where vp/|s1|2v_{p}/|s_{1}|^{2} for p=0,1,,5p=0,1,\dots,5 are given by 1s~u¯01-\tilde{s}\bar{u}_{0}, s~u¯1-\tilde{s}\bar{u}_{1}, s~u¯2+s~u¯0-\tilde{s}\bar{u}_{2}+\tilde{s}\bar{u}_{0}, s~u¯3+s~u¯1-\tilde{s}\bar{u}_{3}+\tilde{s}\bar{u}_{1}, s~u¯2\tilde{s}\bar{u}_{2}, s~u¯3\tilde{s}\bar{u}_{3}, respectively. Note that s0ks_{0}^{k} can be recast as

s0k=12|s1s2|(s1Hs2Q0k+(s1Hs2Q0k)H).\displaystyle s_{0}^{k}=\frac{1}{2|s_{1}s_{2}|}\left(s_{1}^{H}s_{2}Q_{0}^{k}+(s_{1}^{H}s_{2}Q_{0}^{k})^{H}\right). (86)

Substituting (86) to (D) yields

[𝒢1]1,1k=2K|𝒩k|f~(φ¯k)g~(Q0k),\displaystyle[\mathcal{G}_{1}]_{1,1}\approx\sum_{k=2}^{K}|\mathcal{N}_{k}|\cdot\tilde{f}(\bar{\varphi}_{k})\cdot\tilde{g}(Q_{0}^{k}), (87)

where f~(x)=(xφ¯)2\tilde{f}(x)=(x-\bar{\varphi})^{2} and g~(x)\tilde{g}(x) is a polynomial function w.r.t. xpx^{-p} and xpx^{p} for p=0,1,,5p=0,1,\dots,5, the specific form of which is omitted. Based on (16) in Assumption A3, we have

[𝒢1]1,1\displaystyle[\mathcal{G}_{1}]_{1,1} k=2Kn𝒩kf~(φn)g~(ejΔωφn)\displaystyle\approx\sum_{k=2}^{K}\sum_{n\in\mathcal{N}_{k}}\tilde{f}(\varphi_{n})\cdot\tilde{g}(e^{j\Delta\omega\varphi_{n}})
n=1Nf~(φn)g~(ejΔωφn),\displaystyle\approx\sum_{n=1}^{N}\tilde{f}(\varphi_{n})\cdot\tilde{g}(e^{j\Delta\omega\varphi_{n}}), (88)

which can be directly recast as a polynomial function of Qi(pΔω)Q_{i}(p\Delta\omega) for i=0,1,2i=0,1,2 and p=5,4,,5p=-5,-4,\dots,5, given by

[𝒢1]1,1i=02p=55cpiQi(pΔω),\displaystyle[\mathcal{G}_{1}]_{1,1}\approx\sum_{i=0}^{2}\sum_{p=-5}^{5}c_{p}^{i}\cdot Q_{i}(p\Delta\omega), (89)

where cpic_{p}^{i} is a constant unrelated to Δω\Delta\omega, completing the proof of the part of 𝒢1\mathcal{G}_{1}.

For [𝒢2]1,1[\mathcal{G}_{2}]_{1,1}, substituting (5) to 𝒢2\mathcal{G}_{2} yields

[𝒢2]1,1\displaystyle[\mathcal{G}_{2}]_{1,1} =k1=2Kk2=2K[𝑴^]1,k11[𝑴^]1,k21N[𝒉]k11[𝒉]k21\displaystyle=\sum_{k_{1}=2}^{K}\sum_{k_{2}=2}^{K}\frac{[\widehat{\bm{M}}]_{1,k_{1}-1}[\widehat{\bm{M}}]_{1,k_{2}-1}}{N[\bm{h}]_{k_{1}-1}[\bm{h}]_{k_{2}-1}}
(l=1,2Re{[𝑨H𝑯]l,k11H[𝑨H𝑯]l,k21}).\displaystyle\cdot\Big{(}\sum_{l=1,2}{\rm Re}\left\{[\bm{A}^{H}\bm{H}]_{l,k_{1}-1}^{H}[\bm{A}^{H}\bm{H}]_{l,k_{2}-1}\right\}\Big{)}. (90)

Due to Re(xHy)=Re(x)Re(y)+Im(x)Im(y){\rm Re}(x^{H}y)={\rm Re}(x){\rm Re}(y)+{\rm Im}(x){\rm Im}(y) for any x,yx,y\in\mathbb{C}, (D) can be recast as

[𝒢2]1,1\displaystyle[\mathcal{G}_{2}]_{1,1} =l=1,2(k=2K[𝑴^]1,k1Re{[𝑨H𝑯]l,k1}N[𝒉]k1)2\displaystyle=\sum_{l=1,2}\left(\sum_{k=2}^{K}\frac{[\widehat{\bm{M}}]_{1,k-1}{\rm Re}\left\{[\bm{A}^{H}\bm{H}]_{l,k-1}\right\}}{\sqrt{N}[\bm{h}]_{k-1}}\right)^{2}
+l=1,2(k=2K[𝑴^]1,k1Im{[𝑨H𝑯]l,k1}N[𝒉]k1)2.\displaystyle+\sum_{l=1,2}\left(\sum_{k=2}^{K}\frac{[\widehat{\bm{M}}]_{1,k-1}{\rm Im}\left\{[\bm{A}^{H}\bm{H}]_{l,k-1}\right\}}{\sqrt{N}[\bm{h}]_{k-1}}\right)^{2}. (91)

Similar as [𝒢1]1,1[\mathcal{G}_{1}]_{1,1} in (81), we substitute (43) and (D) to (D) and have

[𝒢2]1,1=|s1|24Nr=14(K=2KγMkp=0up(s0k)pg¯rμ2)2,\displaystyle[\mathcal{G}_{2}]_{1,1}=\frac{|s_{1}|^{2}}{4N}\sum_{r=1}^{4}\left(\sum_{K=2}^{K}\gamma_{M}^{k}\sum_{p=0}^{\infty}\frac{u_{p}\cdot(s_{0}^{k})^{p}\cdot\bar{g}_{r}}{\mu^{2}}\right)^{2}, (92)

where g¯r\bar{g}_{r} for r=1,,4r=1,\dots,4 are expressed as (s1s1H)±μ(s2Q0k(s2Q0k)H)(s_{1}-s_{1}^{H})\pm\mu(s_{2}Q_{0}^{k}-(s_{2}Q_{0}^{k})^{H}) and (s1(Q0k)H+s2μ)±(s1HQ0k+s2Hμ)(s_{1}(Q_{0}^{k})^{H}+s_{2}\mu)\pm(s_{1}^{H}Q_{0}^{k}+s_{2}^{H}\mu). Similar to the approximation on [𝒢1]1,1[\mathcal{G}_{1}]_{1,1}, we apply the procedures from (D) to (89) to [𝒢2]1,1[\mathcal{G}_{2}]_{1,1} in (D) and have

[𝒢2]1,1r=14(i=02p=55dr,piQi(pΔω))2,\displaystyle[\mathcal{G}_{2}]_{1,1}\approx\sum_{r=1}^{4}\left(\sum_{i=0}^{2}\sum_{p=-5}^{5}d_{r,p}^{i}\cdot Q_{i}(p\Delta\omega)\right)^{2}, (93)

where dr,pid_{r,p}^{i} is a constant unrelated to Δω\Delta\omega, completing the proof of the part of 𝒢2\mathcal{G}_{2}.

By combining the proofs on 𝒢1\mathcal{G}_{1} and 𝒢2\mathcal{G}_{2}, we complete the proof of this lemma.

Appendix E Proof pf Lemma 4

We rewrite CRBFC(Δω){\rm CRB}_{\rm FC}(\Delta\omega) in (35) as a function of Q(Δω)Q(\Delta\omega). Particularly, through substituting 𝑨=[𝒂(ω1),,𝒂(ωL)]\bm{A}=[\bm{a}(\omega_{1}),\dots,\bm{a}(\omega_{L})] and [𝒂(ωl)]n=ejωlφn[\bm{a}(\omega_{l})]_{n}=e^{j\omega_{l}\varphi_{n}} to 𝚷𝑨\bm{\Pi}_{\bm{A}}^{\perp} in (40), we have

𝚷𝑨\displaystyle\bm{\Pi}_{\bm{A}}^{\perp} =𝑰𝑨(𝑰𝑪Q)𝑨HN(1|Q0|2),\displaystyle=\bm{I}-\frac{\bm{A}(\bm{I}-\bm{C}_{Q})\bm{A}^{H}}{N(1-|Q_{0}|^{2})}, (94)

where 𝑪Q\bm{C}_{Q} is denoted by

𝑪Q=[0Q0Q0H0].\displaystyle\bm{C}_{Q}=\begin{bmatrix}0&Q_{0}\\ Q_{0}^{H}&0\end{bmatrix}. (95)

Through substituting 𝑫\bm{D} in (41) and 𝚷𝑨\bm{\Pi}_{\bm{A}}^{\perp} in (94) to 𝑭=Re{𝑫H𝚷𝑨𝑫}\bm{F}={\rm Re}\left\{\bm{D}^{H}\bm{\Pi}_{\bm{A}}^{\perp}\bm{D}\right\} in (37), we have

𝑭=\displaystyle\bm{F}= Re{(𝑭1+𝑭2+𝑭3)𝑺},\displaystyle{\rm Re}\left\{(\bm{F}_{1}+\bm{F}_{2}+\bm{F}_{3})\odot\bm{S}\right\}, (96)

where

𝑭1\displaystyle\bm{F}_{1} =n=1Nφn2[1Q2Q2H1],\displaystyle=\sum_{n=1}^{N}\varphi_{n}^{2}\cdot\begin{bmatrix}1&Q_{2}\\ Q_{2}^{H}&1\end{bmatrix}, (97)
𝑭2\displaystyle\bm{F}_{2} =γ0[1+|Q1|22Q12Q1H1+|Q1|2],\displaystyle=-\gamma_{0}\cdot\begin{bmatrix}1+|Q_{1}|^{2}&2Q_{1}\\ 2Q_{1}^{H}&1+|Q_{1}|^{2}\end{bmatrix}, (98)
𝑭3\displaystyle\bm{F}_{3} =γ0[Q0Q1H+Q0HQ1Q0HQ1Q1+Q0Q0Q1HQ1H+Q0HQ0Q1H+Q0HQ1],\displaystyle=\gamma_{0}\cdot\begin{bmatrix}Q_{0}Q_{1}^{H}+Q_{0}^{H}Q_{1}&Q_{0}^{H}Q_{1}Q_{1}+Q_{0}\\ Q_{0}Q_{1}^{H}Q_{1}^{H}+Q_{0}^{H}&Q_{0}Q_{1}^{H}+Q_{0}^{H}Q_{1}\end{bmatrix}, (99)

where γ0=(n=1Nφn)2N(1|Q0|2)\gamma_{0}=\frac{(\sum_{n=1}^{N}\varphi_{n})^{2}}{N(1-|Q_{0}|^{2})} and 𝑺\bm{S} is defined as

𝑺[|s1|2s1Hs2s2Hs1|s2|2],\displaystyle\bm{S}\equiv\begin{bmatrix}|s_{1}|^{2}&s_{1}^{H}s_{2}\\ s_{2}^{H}s_{1}&|s_{2}|^{2}\end{bmatrix}, (100)

completing the proof.

Appendix F Proof of Lemma 5

The following equation is satisfied, which can be directly verified by matrix multiplication:

𝑩~𝑩^=𝑰+𝑩¯,\displaystyle\widetilde{\bm{B}}\widehat{\bm{B}}=\bm{I}+\bar{\bm{B}}, (101)

where

𝑩~\displaystyle\widetilde{\bm{B}} =[B200Bk]Re{[𝒃2H𝒃KH][𝒃2𝒃K]},\displaystyle=\begin{bmatrix}B_{2}&&0\\ &\ddots&\\ 0&&B_{k}\end{bmatrix}-{\rm Re}\left\{\begin{bmatrix}\bm{b}_{2}^{H}\\ \vdots\\ \bm{b}_{K}^{H}\end{bmatrix}\begin{bmatrix}\bm{b}_{2}&\cdots&\bm{b}_{K}\end{bmatrix}\right\}, (102)
𝑩^\displaystyle\widehat{\bm{B}} =[1B2001Bk]+Re{[𝒃2HB2𝒃KHBK][𝒃2B2𝒃KBK]},\displaystyle=\begin{bmatrix}\frac{1}{B_{2}}&&0\\ &\ddots&\\ 0&&\frac{1}{B_{k}}\end{bmatrix}+{\rm Re}\left\{\begin{bmatrix}\frac{\bm{b}_{2}^{H}}{B_{2}}\\ \vdots\\ \frac{\bm{b}_{K}^{H}}{B_{K}}\end{bmatrix}\begin{bmatrix}\frac{\bm{b}_{2}}{B_{2}}&\cdots&\frac{\bm{b}_{K}}{B_{K}}\end{bmatrix}\right\}, (103)

where B2,,BK>0B_{2},\dots,B_{K}>0, and the matrix [𝑩¯]k11,k21=k=2KRe{𝒃k1H𝒃k}Re{𝒃kH𝒃k2}BkBk2[\bar{\bm{B}}]_{k_{1}-1,k_{2}-1}=-\sum_{k=2}^{K}\frac{{\rm Re}\{\bm{b}_{k_{1}}^{H}\bm{b}_{k}\}{\rm Re}\{\bm{b}_{k}^{H}\bm{b}_{k_{2}}\}}{B_{k}B_{k_{2}}} for k1,k2=2,,Kk_{1},k_{2}=2,\dots,K.

When Bk=[𝒉]k1B_{k}=[\bm{h}]_{k-1} and 𝒃k=1N[𝑨H𝑯]k1\bm{b}_{k}=\frac{1}{\sqrt{N}}[\bm{A}^{H}\bm{H}]_{k-1}, i.e., 𝑩~=𝑮~\widetilde{\bm{B}}=\widetilde{\bm{G}}, we have

limK[𝑩¯]k11,k21=0,\displaystyle\underset{K\rightarrow\infty}{\lim}\ [\bar{\bm{B}}]_{k_{1}-1,k_{2}-1}=0, (104)

yielding 𝑩¯𝟎\bar{\bm{B}}\approx\bm{0} when KK is large enough. The reason is shown as follows: Based on the A2 assumption, we have |𝒩k|/N=1/K|\mathcal{N}_{k}|/N=1/K and KK is large (1/K01/K\approx 0). By substituting (43) to 𝑩¯\bar{\bm{B}}, we have

[𝑩¯]k11,k21\displaystyle[\bar{\bm{B}}]_{k_{1}-1,k_{2}-1} =k=2K|𝒩k1||𝒩k|2|𝒩k2|N2|𝒩k||𝒩k2|fk1,k2(𝒔,𝝎,Q0k)\displaystyle=\sum_{k=2}^{K}\frac{|\mathcal{N}_{k_{1}}||\mathcal{N}_{k}|^{2}|\mathcal{N}_{k_{2}}|}{N^{2}|\mathcal{N}_{k}||\mathcal{N}_{k_{2}}|}\cdot f_{k_{1},k_{2}}(\bm{s},\bm{\omega},Q_{0}^{k})
|𝒩k1|Nfk1,k2(𝒔,𝝎,Q0k)\displaystyle\approx\frac{|\mathcal{N}_{k_{1}}|}{N}\cdot f_{k_{1},k_{2}}(\bm{s},\bm{\omega},Q_{0}^{k})
=1Kfk1,k2(𝒔,𝝎,Q0k),\displaystyle=\frac{1}{K}\cdot f_{k_{1},k_{2}}(\bm{s},\bm{\omega},Q_{0}^{k}), (105)

where fk1,k2(𝒔,𝝎,Q0k)f_{k_{1},k_{2}}(\bm{s},\bm{\omega},Q_{0}^{k}) denotes a function of 𝒔\bm{s}, 𝝎\bm{\omega} and Q0kQ_{0}^{k} for k1,k2=2,,Kk_{1},k_{2}=2,\dots,K, and the approximation in (F) is derived from k=2K|𝒩k|=K1KNN\sum_{k=2}^{K}|\mathcal{N}_{k}|=\frac{K-1}{K}N\approx N. When 1/K01/K\approx 0, we have the conclusion in (104).

Based on Assumption A2, we have 𝑩¯𝟎\bar{\bm{B}}\approx\bm{0}, which means

𝑩~𝑩^𝑰,\displaystyle\widetilde{\bm{B}}\widehat{\bm{B}}\approx\bm{I}, (106)

yielding 𝑮~1𝑩^\widetilde{\bm{G}}^{-1}\approx\widehat{\bm{B}} in (103) with Bk=[𝒉]k1B_{k}=[\bm{h}]_{k-1} and 𝒃k=1N[𝑨H𝑯]k1\bm{b}_{k}=\frac{1}{\sqrt{N}}[\bm{A}^{H}\bm{H}]_{k-1}, completing the proof.

Appendix G Proof of Lemma 6

The gradient of upu_{p} w.r.t. μ\mu is calculated as

up=dupdμ=(2)p(p+2)(μs~)1pμs~((μs~)1+μs~)p+2.\displaystyle u_{p}^{\prime}=\frac{{\rm d}u_{p}}{{\rm d}\mu}=(-2)^{p}\cdot\frac{(p+2)(\mu\tilde{s})^{-1}-p\mu\tilde{s}}{\left((\mu\tilde{s})^{-1}+\mu\tilde{s}\right)^{p+2}}. (107)

Since upu_{p} is either odd or even function of μ\mu, we assume μ>0\mu>0 without loss of generality.

We prove the 1-st item in Lemma 6. Based on (107), (83) is equivalent to

2p((p+2)(μs~)1pμs~)((μs~)1+μs~)p+2.\displaystyle 2^{p}\left((p+2)(\mu\tilde{s})^{-1}-p\mu\tilde{s}\right)\leqslant\left((\mu\tilde{s})^{-1}+\mu\tilde{s}\right)^{p+2}. (108)

Apply binomial expansion to the right part of (108), yielding

((μs~)1+μs~)p+2=i=0p+2Bi(μ),\displaystyle\big{(}(\mu\tilde{s})^{-1}+\mu\tilde{s}\big{)}^{p+2}=\sum_{i=0}^{p+2}B_{i}(\mu), (109)

where

Bi(μ)=(p+2i)2p+2i((μs~)1+μs~2)i.\displaystyle B_{i}(\mu)=\binom{p+2}{i}2^{p+2-i}\left((\mu\tilde{s})^{-1}+\mu\tilde{s}-2\right)^{i}. (110)

Since (μs~)1+μs~20(\mu\tilde{s})^{-1}+\mu\tilde{s}-2\geqslant 0, Bi(μ)0B_{i}(\mu)\geqslant 0 for i=0,,p+2i=0,\dots,p+2. Then, we prove that the left part of (108) is less than B0(μ)+B1(μ)B_{0}(\mu)+B_{1}(\mu) when p3p\geqslant 3, yielding the inequality of (108). Particularly, we have

2p\displaystyle 2^{p} ((p+2)(μs~)1pμs~)B0(μ)B1(μ)\displaystyle\left((p+2)(\mu\tilde{s})^{-1}-p\mu\tilde{s}\right)-B_{0}(\mu)-B_{1}(\mu)
=2p(4(p+1)(3p+4)s~μ(p+2)(s~μ)1)\displaystyle=2^{p}\left(4(p+1)-(3p+4)\tilde{s}\mu-(p+2)(\tilde{s}\mu)^{-1}\right)
2p(4(p+1)2(3p+4)(p+2))0,\displaystyle\leqslant 2^{p}\left(4(p+1)-2\sqrt{(3p+4)(p+2)}\right)\leqslant 0, (111)

for p3,pp\geqslant 3,p\in\mathbb{N}, completing the proof of the 1-st item in Lemma 6.

For the 2-nd item in Lemma 6, based on (107), we have

0Lim|μ||up|\displaystyle 0\leqslant\underset{|\mu|\rightarrow\infty}{\rm Lim}|u_{p}^{\prime}| Lim|μ|2p(p+2)(μs~)1(μs~)p+2\displaystyle\leqslant\underset{|\mu|\rightarrow\infty}{\rm Lim}\frac{2^{p}(p+2)(\mu\tilde{s})^{-1}}{(\mu\tilde{s})^{p+2}}
=Lim|μ|2p(p+2)(μs~)p+3=0,\displaystyle=\underset{|\mu|\rightarrow\infty}{\rm Lim}\frac{2^{p}(p+2)}{(\mu\tilde{s})^{p+3}}=0, (112)

completing the proof of the 2-nd item in Lemma 6.

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