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Research article

Linearized active circuits: transfer functions and stability

  • We study the properties of electronic circuits after linearization around a fixed operating point in the context of closed-loop stability analysis. When distributed elements, like transmission lines, are present in the circuit it is known that unstable circuits can be created without poles in the complex right half-plane. This undermines existing closed-loop stability analysis techniques that determine stability by looking for right half-plane poles. We observed that the problematic circuits rely on unrealistic elements with an infinite bandwidth. In this paper, we therefore define a class of realistic linearized components and show that a circuit composed of realistic elements is only unstable with poles in the complex right half-plane. Furthermore, we show that the amount of right half-plane poles in a realistic circuit is finite, even when distributed elements are present. In the second part of the paper, we provide examples of component models that are realistic and show that the class includes many existing models, including ones for passive devices, active devices and transmission lines.

    Citation: Laurent Baratchart, Sylvain Chevillard, Adam Cooman, Martine Olivi, Fabien Seyfert. Linearized active circuits: transfer functions and stability[J]. Mathematics in Engineering, 2022, 4(5): 1-18. doi: 10.3934/mine.2022039

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  • We study the properties of electronic circuits after linearization around a fixed operating point in the context of closed-loop stability analysis. When distributed elements, like transmission lines, are present in the circuit it is known that unstable circuits can be created without poles in the complex right half-plane. This undermines existing closed-loop stability analysis techniques that determine stability by looking for right half-plane poles. We observed that the problematic circuits rely on unrealistic elements with an infinite bandwidth. In this paper, we therefore define a class of realistic linearized components and show that a circuit composed of realistic elements is only unstable with poles in the complex right half-plane. Furthermore, we show that the amount of right half-plane poles in a realistic circuit is finite, even when distributed elements are present. In the second part of the paper, we provide examples of component models that are realistic and show that the class includes many existing models, including ones for passive devices, active devices and transmission lines.



    In this paper, we mainly focus on the random inverse problems associated with the following time-harmonic Schrödinger system

    (ΔE+potential)u(x)=source,xRn, (1.1)

    where E is the energy level, n is the dimension, and "source" and the "potential" in (1.1) shall be specified later. In some cases we may impose incident waves to the system in order to obtain more useful information, thus

    u(x)=αuin(x)+usc(x) (1.2)

    where α takes the value of either 0 or 1 corresponding to impose or suppress the incident wave, respectively. The corresponding data are thus called passive or active measurements. Moreover, we shall impose the Sommerfeld radiation condition [10]

    limrr(uscriEusc)=0,r:=|x|, (1.3)

    that characterizes the outgoing nature of the scattered field usc. The system (1.1)-(1.3) describes the quantum scattering [13,14] associated with a source and a potential at the energy level E. Later we follow the convention to use k:=E to signify the frequency at which the system is acting on.

    Under different assumptions of the potential and source, of the dimension, and of the incident wave, the regularity of the Schrödinger system (1.1)-(1.3) behaves differently and calls for different techniques for the recovery procedure. The randomness of the Schrödinger system (1.1)-(1.3) can present either in the potential, or in the source, or in both. In this paper we shall investigate all of these three cases, survey the results in the literature and give details of part of the proofs.

    There are rich literature on the inverse scattering problem using either passive or active measurements as data. For a fixed potential, the recovery of the deterministic unknown source of the system is called the inverse source problem. For the theoretical analysis and computational methods of the inverse source problems, readers may refer to [3,4,5,9,31,34] and references therein. The simultaneous recovery of the deterministic unknown source and potential are also studied in the literature. In [17,26], the authors considered the simultaneous recovery of an unknown source and its surrounding medium parameter. This type of inverse problems also arises in the deterministic magnetic anomaly detections using geomagnetic monitoring [11,12] with passive measurements. While [11,12,17,26] focus on deterministic setting with passive measurements, the works [2,6,7,18,19,20,27,33] pay attention to random settings. We are particularly interested in the case with a single realization of the random sample. The single-realization recovery has been studied in the literature. In this paper we mainly focus on [8,18,19,20,21,22,23,24,25].

    In [18,19], Lassas et. al. considered the inverse scattering problem for the two-dimensional random Schrödinger system (Δk2q(x,ω))u(x,k,ω)=δy, xR2 which is incited by point sources uin(x)=i4H(1)0(k|xy|); the H(1)0 is the Hankel function for the first kind, and the origin y of this source are located outside the support of the potential. The potential q(x,ω) is a micro-locally isotropic generalized Gaussian field (migr field) with compact support. The definition of the migr field can be found in Definition 1.1. They introduced the so-called rough strength μ(x), which is the informative part of the principal symbol μ(x)|ξ|m of the covariance operator. The m in μ(x)|ξ|m is the rough order of the random potential. The main result in their work states that under a single measurement of the random field inside a measurement domain, the rough strength can be recovered.

    In 2019, Caro et. al. [8] considered an inverse scattering problem for an n-dimensional (n2) random Schrödinger system (Δk2q(x,ω))u(x,k,ω)=0, xRn with incident wave being the plane wave, i.e. u is incited by the point sources uin(x)=eikdx; d is the incident direction. Again, the potential q is assumed to be a migr field with compact support. The main result is as follows: they used the backscattering far-field pattern and recovered the rough strength μ(x) almost surely, under a single realization of the randomness.

    In [20], Li, et. al. studied the case where the potential is zero and the source is migr field. In [24] Li, et. al. studied the same setting but with the energy level E replaced by (k2+iσk) where the σ is the attenuation parameter. The random source term considered is constructed as a migr field. The system has been changed to Helmholtz system in [24] but the underlying equation is uniform with the Schrödinger's equation. The authors studied the regularity of the random source and gave the well-posedness of the direct problem. Then they represented the solution as the convolution between the fundamental solution and the random source. By truncating the fundamental solution, they indicated that the rough strength can be recovered by utilizing the correspondingly truncated solution. Further, the authors used calculus of symbols to recover the rough strength.

    Then in [23], Li, et. al. further extended their study to Maxwell's equation. The recovery procedure in these three works share the same idea–the leading order term in the Bonn expansion gives the recovery of the desired statistics while the higher order terms converge to zero. The proof of these converges involve the utilization of Fourier integral operator. We shall give detailed explanations in Section 3.

    In [21], the authors consider the direct and inverse scatterings for (1.1)–(1.3) with a deterministic potential and a random source. The random source is a generalized Gaussian random field with local mean value function and local variance function, which are assumed to be bounded and compactly supported. The well-posedness of the direct scattering has been formulated in some weighted L2 space. Then the inverse scattering is studied and a recovery formula of the variance function is obtained, and the uniqueness recovery of the potential is given. The authors used both passive and active measurements to recover the unknowns. The passive measurements refer to the scattering data generated only by the unknown source (α is set to be 0 in (1.2)); active measurements refer to the scattering data generated by both the source and the incident wave (α is set to be 1 in (1.2)). To recover the variance function, only the passive measurements are needed, while the unique recovery of the potential needs active measurements.

    In [25], the authors extended the work [21] to the case where the source is a migr field. The direct scattering problem is formulated in a similar manner as in [21], while the technique used in the inverse scattering problem differs from that of [21]. In order to analyze the asymptotics of higher order terms in the Bonn expansion corresponding to the migr fields, stationary phase lemma and pseudodifferential operator are utilized.

    Then the authors extended the work [25] to the case where both the potential and the source are random (of migr type), and the extended result is presented in [22]. The results between [21] and [22,25] have two major differences. First, in [21] the random part of the source is assumed to be a Gaussian white noise, while in [22] the potential and the source are assumed to be migr fields. The migr field can fit larger range of randomness by tuning its rough order and rough strength. Second, in [22] both the source and potential are random, while in [25] the potential is assumed to be deterministic. These two facts make [22] much more challenging than that in [25]. The techniques used in the estimates of higher order terms in [22] are pseudodifferential operators and microlocal analysis and we shall give a detailed treatment in Section 4.

    Although the techniques used in [21,22,25] are different, the recovery formulae fall into the same pattern. The thesis [28] partially collected these three works[21,22,25] and readers may refer to the thesis for a more coherent discussion on this topic.

    In this paper we mainly pay attention to two types of random model, the Gaussian white noise and the migr field. The Gaussian white noise is well-known and readers may refer to [21,Section 2.1] for more details. Here we give a brief introduction to the migr field. We assume f to be a generalized Gaussian random distribution of the microlocally isotropic type (cf. Definition 1.1). It means that f(,ω) is a random distribution and the mapping

    ωΩ  f(,ω),φC,φS(Rn),

    is a Gaussian random variable whose probabilistic measure depends on the test function φ. Here and also in what follows, S(Rn) stands for the Schwartz space. Since both f(,ω),φ and f(,ω),ψ are random variables for φ, ψS(Rn), from a statistical point of view, the covariance between these two random variables,

    Eω(¯f(,ω)E(f(,ω)),φf(,ω)E(f(,ω)),ψ), (1.4)

    can be understood as the covariance of f. Here Eω means to take expectation on the random variable ω. Hence, formula (1.4) defines an operator Cf,

    Cf:φS(Rn)  Cf(φ)S(Rn),

    in a way that \(\mathfrak C_f (\varphi) \colon \psi \in \mathscr{S}({\mathbb{R}^n}) \ \mapsto \ (\mathfrak C_f (\varphi))(\psi) \in \mathbb C\) where

    (Cf(φ))(ψ):=Eω(¯f(,ω)E(f(,ω)),φf(,ω)E(f(,ω)),ψ).

    The operator Cf is called the covariance operator of f.

    Definition 1.1 (Migr field). A generalized Gaussian random distribution f on Rn is called microlocally isotropic with rough order m and rough strength μ(x) in a bounded domain D, if the following conditions hold:

    1. the expectation E(f) is in Cc(Rn) with suppE(f)D;

    2. f is supported in D a.s. (almost surely);

    3. the covariance operator Cf is a classical pseudodifferential operator of order m;

    4. Cf has a principal symbol of the form μ(x)|ξ|m with μCc(Rn;R), suppμD and μ(x)0 for all xRn.

    We call a microlocally isotropic Gaussian random distribution as an migr field.

    For the case where both the source and the potential are deterministic and are L functions with compact supports, the well-posedness of the direct problem of system (1.1)–(1.3) is known; see, e.g., [10,13,29]. Moreover, there holds the following asymptotic expansion of the outgoing radiating field usc as |x|+,

    usc(x)=eik|x||x|(n1)/2u(ˆx,k,d)+o(|x|(n1)/2),xRn.

    u(ˆx,k,d) is referred to as the far-field pattern, which encodes information of the potential and the source. ˆx:=x/|x| and d in u(ˆx,k,d) are unit vectors and they respectively stand for the observation direction and the impinging direction of the incident wave. When d=ˆx, u(ˆx,k,ˆx) is called the backscattering far-field pattern. We shall see very soon that both the near-field usc and the far-field u can be used to achieve the recovery.

    In (1.1), let us denote the source term as f and the potential term as q. In our study, both the source f and the potential q are assumed to be compactly supported. We shall treat [8,18,19,20,21,22,23,24,25] in more details. In [8,18,19], q is assumed to be a migr field while f is either zero or point a point source, i.e. δy(x). In [20,23,24], q is assumed to be zero and f is assumed to be a migr field. In [21], q is assumed to be unknown and deterministic and f is assumed to be a Gaussian white noise, while in [22,25], q is assumed to be deterministic or migr type and f is assumed to be a migr field.

    In [18,19] the authors considered the inverse scattering problem for the two-dimensional random Schrödinger system (Δk2q(x,ω))u(x,k,ω)=δy(x)(xR2) which is incited by point sources uin(x)=i4H(1)0(k|xy|); the H(1)0 is the Hankel function for the first kind, and the origin y of this source is located in U. The potential q(x,ω) is a migr field with compact support D and ¯U¯D=. The main result is presented as follows (cf. [19,Theorem 7.1]).

    Theorem 1.1. In [18,19], for x,yU the limit

    R(x,y)=limK+1K1K1k2+m|usc(x,y,k,ω)|2dk

    holds almost surely where

    R(x,x):=126+mπ2R2μq(z)|xz|2dz,xU.

    and the μq is the rough strength and m is the rough order of q.

    In [8], the authors considered (Δk2q(x,ω))u(x,k,ω)=0, xRn with incident plane wave uin(x)=eikds. The potential q is assumed to be a migr field with compact support. The main result (cf. [8,Corollary 4.4]) is as follows.

    Theorem 1.2. In [8], the limit

    ˆμq(2τˆx)limK+1K2KKkmu(ˆx,ˆx,k)¯u(ˆx,ˆx,k+τ)dk,ˆxS2, τ>0.

    holds almost surely.

    We note that the near-field data are used in [18,19], while in [8], the authors used the far-field data.

    Part of the results in [20] and [23,24] are similar to each other and we only survey the first result in [20]. In [20] the authors studied the Helmholtz equation (Δk2)u(x)=f where f is a source of migr type. Note that the potential equals zero. The main result (cf. [20,Theorem 3.9]) is similar to Theorem 1.1.

    Theorem 1.3. In [20], the limit

    μf(z)|xz|dzlimK+1K1K1k1+m|usc(x,k,ω)|2dk,xU,

    holds almost surely.

    In [21], the authors considered direct and inverse scattering for (1.1)–(1.3) with an unknown deterministic potential and a Gaussian noise source of the form σ(x)˙Bx(ω), where σ(x) is the variance and ˙Bx(ω) is the Gaussian white noise. The main result (cf. [21,Lemma 4.3]) is

    Theorem 1.4. In [21], the identity

    ^σ2(x)=42πlimj+1Kj2KjKj¯u(ˆx,k,ω)u(ˆx,k+τ,ω)dk.

    holds almost surely.

    The paper [25] extended the work [21] to the case where the source is a migr field f with μf as its rough strength and m as its rough order. For notational convenience, we shall use {Kj}P(t) to signify a sequence {Kj}jN satisfying KjCjt(jN) for some fixed constant C>0. Throughout the rest of the paper, γ stands for a fixed positive real number. The main result (cf. [25,Theorem 4.3]) is presented below.

    Theorem 1.5. In [25], assume 2<m<3 and let m=max{2/3,(3m)1/2}. Assume that {Kj}P(m+γ). Then Ω0Ω:P(Ω0)=0, Ω0 depending only on {Kj}jN, such that for any ωΩΩ0, there exists SωR3:|Sω|=0, it holds that for τR+ and ˆxS2 satisfying τˆxR3Sω,

    ˆμ(τˆx)=42πlimj+1Kj2KjKjkm¯u(ˆx,k,ω)u(ˆx,k+τ,ω)dk,

    holds for τR+ and ˆxS2 satisfying τˆxR3Sω.

    Then in [22] the authors further extended the work [25] to the case where both the potential q and the source f are random of migr type. The f (resp. q) is assumed to be supported in the domain Df (resp. Dq). In what follows, we assume that there is a positive distance between the convex hulls of the supports of f and q, i.e.,

    dist(CH(Df),CH(Dq)):=inf{|xy|;xCH(Df),yCH(Dq)}>0, (1.5)

    where CH means taking the convex hull of a domain. Therefore, one can find a plane which separates Df and Dq. In order to simplify the exposition, we assume that Df and Dq are convex domains and hence CH(Df)=Df and CH(Dq)=Dq. Moreover, we let n denote the unit normal vector of the aforementioned plane that separates Df and Dq, pointing from the half-space containing Df into the half-space containing Dq. Then the result of this work (cf. [22,Theorems 1.1 and 1.2]) is as follows.

    Theorem 1.6. In [22], suppose that f and q in system (1.1)-(1.3) are migr fields of order mf and mq, respectively, satisfying

    2<mf<4, mf<5mq11.

    Assume that (1.5) is satisfied and n is defined as above. Then, independent of μq, μf can be uniquely recovered almost surely and the recovering formula of μf is given by

    ˆμf(τˆx)={limK+42πK2KKkmf¯u(ˆx,k,ω)u(ˆx,k+τ,ω)dk,ˆxn0, ¯ˆμf(τˆx),ˆxn<0, (1.6)

    where τ0 and u(ˆx,k,ω)Mf(ω):={u(ˆx,k,ω);ˆxS2,kR+}.

    When mq<mf, μq can be uniquely recovered almost surely by the data set Mq(ω) for a fixed ωΩ. Moreover, the recovering formula is given by

    ˆμq(τˆx)={limK+42πK2KKkmq¯u(ˆx,k,ˆx,ω)u(ˆx,k+τ2,ˆx,ω)dk, ˆxn0, ¯ˆμf(τˆx),ˆxn<0, (1.7)

    where τ0 and u(ˆx,k,ˆx,ω)Mq(ω):={u(ˆx,k,ˆx,ω);ˆxS2,kR+}.

    Remark 1.1. In Theorem 1.6, the data sets Mf(ω) and Mf(ω) correspond to the case where the incident wave is passive and active, respectively. Readers may refer to [22,Section 1] for more details.

    Readers should note that the recovery formulae in Theorems 1.1–1.6 only use a single realization of the randomness; the terms on the left-hand-sides are independent of the random sample ω, while these on the right-hand-sides are limits of terms depending on ω. This feature is also described as "statistically stable" in the literature. The key ingredient of making this single-realization recovery possible is ergodicity; on the right-hand-sides of these recoveries formulae in Theorems 1.1–1.6, the probabilistic expectation operation are replaced by the average in the frequency variable and then taking to the infinity of the frequency variable. Theorems 1.1 and 1.3 utilize the near-field data to achieve the recovery, while Theorem 1.2 and 1.4–1.6 use the far-field data. Due to this difference, the corresponding techniques required in the proofs are also different. We shall present these techniques separately in Sections 3 and 4.

    The rest of this paper is organized as follows. In Section 2, we first give some preliminaries and present the well-posedness of the direct problems. In Section 3, we give the sketch of the proofs in [8,18,19,20,23,24]. Section 4 is devoted to the details of the works [22,25]. We conclude the paper in Section 5 with some remarks and open problems.

    Due to the presence of the randomness, the regularity of the potential and/or the source may be too bad to fall into the scenarios of standard PDEs techniques. In this section, we show some details used in reformulating the direct problems of (1.1)-(1.3) in a proper sense. Before that, we first present some preliminaries as well as some facts related to the migr field for the subsequent use.

    For convenient reference and self- containedness, we first present some preliminary and auxiliary results. In this paper we mainly focus on the two- and three-dimensional cases. Nevertheless, some of the results derived also hold for higher dimensions and in those cases, we choose to present the results in the general dimension n3 since they might be useful in other studies. Here we follow closely [22].

    Throughout the paper, we write L(A,B) to denote the set of all the bounded linear mappings from a normed vector space A to a normed vector space B. For any mapping KL(A,B), we denote its operator norm as KL(A,B). We also use C and its variants, such as CD, CD,f, to denote some generic constants whose particular values may change line by line. For two quantities, we write PQ to signify PCQ and PQ to signify ˜CQPCQ, for some generic positive constants C and ˜C. We write "almost everywhere" as "a.e." and "almost surely" as "a.s." for short. We use |S| to denote the Lebesgue measure of any Lebesgue-measurable set S.

    The Fourier transform and inverse Fourier transform of a function φ are respectively defined as

    Fφ(ξ)=ˆφ(ξ):=(2π)n/2eixξφ(x)dx,F1φ(ξ):=(2π)n/2eixξφ(x)dx.

    Set

    Φ(x,y)=Φk(x,y):=eik|xy|4π|xy|,xR3{y}.

    Φk is the outgoing fundamental solution, centered at y, to the differential operator Δk2. Define the resolvent operator Rk,

    (Rkφ)(x):=R3Φk(x,y)φ(y)dy,xR3, (2.1)

    where φ can be any measurable function on R3 as long as (2.1) is well-defined for almost all x in R3.

    Write x:=(1+|x|2)1/2 for xRn, n1. We introduce the following weighted Lp-norm and the corresponding function space over Rn for any δR,

    φLpδ(Rn):= δφ()Lp(Rn)=(Rnxpδ|φ|pdx)1p,Lpδ(Rn):= {φL1loc(Rn);φLpδ(Rn)<+}. (2.2)

    We also define Lpδ(S) for any subset S in Rn by replacing Rn in (2.2) with S. In what follows, we may write L2δ(Rn) as L2δ for short without ambiguities. Let I be the identity operator and define

    fHs,pδ(Rn):=(IΔ)s/2fLpδ(Rn), Hs,pδ(Rn)={fS;fHs,pδ(Rn)<+},

    where S stands for the dual space of the Schwartz space S(Rn). The space Hs,2δ(Rn) is abbreviated as Hsδ(Rn), and Hs,p0(Rn) is abbreviated as Hs,p(Rn). It can be verified that

    fHsδ(Rn)=sˆf()Hδ(Rn). (2.3)

    Let m(,+). We define Sm to be the set of all functions σ(x,ξ)C(Rn,Rn;C) such that for any two multi-indices α and β, there is a positive constant Cα,β, depending on α and β only, for which

    |(DαxDβξσ)(x,ξ)|Cα,β(1+|ξ|)m|β|,x,ξRn.

    We call any function σ in mRSm a symbol. A principal symbol of σ is an equivalent class [σ]={˜σSm;σ˜σSm1}. In what follows, we may use one representative ˜σ in [σ] to represent the equivalent class [σ]. Let σ be a symbol. Then the pseudo-differential operator T, defined on S(Rn) and associated with σ, is defined by

    (Tσφ)(x):=(2π)n/2Rneixξσ(x,ξ)ˆφ(ξ)dξ =(2π)nRn×Rnei(xy)ξσ(x,ξ)φ(y)dydξ,φS(Rn).

    Recall Definition 1.1. Lemma 2.1 below shows how the rough order of a migr field is related to its Sobolev regularity.

    Lemma 2.1. Let h be an migr distribution of rough order m in Dh. Then, hHs,p(Rn) almost surely for any 1<p<+ and s>(nm)/2.

    Proof of Lemma 2.1. See [8,Proposition 2.4].

    By the Schwartz kernel theorem (see [15,Theorem 5.2.1]), there exists a kernel Kh(x,y) with suppKhDh×Dh such that

    (Chφ)(ψ)=Eω(¯h(,ω),φh(,ω),ψ)=Kh(x,y)φ(x)ψ(y)dxdy, (2.4)

    for all φ, ψS(Rn). It is easy to verify that Kh(x,y)=¯Kh(y,x). Denote the symbol of Ch as ch, then it can be verified (see [8]) that the equalities

    {Kh(x,y)=(2π)nei(xy)ξch(x,ξ)dξ,(2.5a)ch(x,ξ)=eiξ(xy)Kh(x,y)dx,(2.5b)

    hold in the distributional sense, and the integrals in (2.5) shall be understood as oscillatory integrals. {Despite} the fact that h usually is not a function, intuitively speaking, however, it is helpful to keep in mind the following correspondence,

    Kh(x,y)Eω(¯h(x,ω)h(y,ω)).

    One way to study the direct problem of (1.1)-(1.3) is to transform it into the Lippmann-Schwinger equation, and then use the Bonn expansion to define a solution. To that end, the estimate of the operator norm of the resolvent Rk is crucial. Among different types of the estimates in the literature, one of them is known as Agmon's estimate (cf. [13,§29]). Reformulating (1.1) into the Lippmann-Schwinger equation formally (cf. [10]), we obtain

    (IRkq)usc=αRkquinRkf.

    We demonstrate two lemmas dealing with the lack of regularity when utilizing Agmon's estimates. Lemma 2.2 (cf. [25,Lemma 2.2]) shows the resolvent can take a migr field as an input without any trouble, while Lemma 2.3 (cf. [22,Theorem 2.1]) gives a variation of Agmon's estimate to fit our own problem settings.

    Lemma 2.2. Assume f is a migr field with rough order m and suppfDf almost surely, then we have RkfL21/2ϵ for any ϵ>0 almost surely.

    Proof. We split Rkf into two parts, Rk(Ef) and Rk(fEf). [21,Lemma 2.1] gives Rk(Ef)L21/2ϵ. For Rk(fEf), by using (2.4), (2.5) and (2.1), one can compute

    E(Rk(fEf)(,ω)2L21/2ϵ)=R3x12ϵE(¯fEf,Φk,xfEf,Φk,x)dx=R3x12ϵCfΦk,x,Φk,xdxx12ϵDf(DfI(y,z)eik|xz||xz||yz|2dz)eik|xy||xy|dydx, (2.6)

    where cf(y,ξ) is the symbol of the covariance operator Cf and

    I(y,z):=R3|yz|2ei(yz)ξcf(y,ξ)dξ.

    When y=z, we know I(y,z)=0 because the integrand is zero. Thanks to the condition m>2, when yz we have

    |I(y,z)|=|3j=1R3ei(yz)ξ(2ξjcf)(y,ξ)dξ|3j=1R3Cjξm2dξC0<+, (2.7)

    for some constant C0 independent of y and z. Note that if Df is bounded, then for j=1,2 we have

    Df|xy|jdyCf,jxj,xR3, (2.8)

    for some constant Cf,j depending only on f,j and the dimension. The notation x in (2.8) stands for (1+|x|2)1/2 and readers may note the difference between the and the , appeared in (2.1). With the help of (2.7) and (2.8) and Hölder's inequality, we can continue (2.6) as

    E(Rk(fEf)(,ω)2L21/2ϵ)x12ϵ(Df×Df(|xz||yz|2|xy|)1dzdy)dxx12ϵCfx2dxCf<+,

    which gives

    E(Rk(fEf)(,ω)2L21/2ϵ)Cf<+. (2.9)

    By using the Hölder inequality applied to the probability measure, we obtain from (2.9) that

    ERk(fEf)L21/2ϵ[E(Rk(fEf)2L21/2ϵ)]1/2C1/2f<+, (2.10)

    for some constant Cf independent of k. The formula (2.10) gives that \({\mathcal{R}_{k}} (f - \mathbb{E} f) \in L_{-1/2-\epsilon}^2 \) almost surely, and hence \({\mathcal{R}_{k}} f \in L_{-1/2-\epsilon}^2 \) almost surely.

    The proof is complete.

    Lemma 2.3. For any 0<s<1/2 and ϵ>0, when k>2,

    RkφHs1/2ϵ(R3)Cϵ,sk(12s)φHs1/2+ϵ(R3),φHs1/2+ϵ(R3).

    Proof. We adopt the concept of Limiting absorption principle to first show desired results on a family of operator Rk,τ controlled by a parameter τ, and then show that Rk,τ converges in a proper sense as τ approaches zero. We sketch out the key steps in the proof and readers may refer to the proof of [22,Theorem 2.1] for complete details.

    Define an operator

    Rk,τφ(x):=(2π)3/2R3eixξˆφ(ξ)|ξ|2k2iτdξ, (2.11)

    where τR+. Fix a function χ satisfying

    {χCc(Rn),0χ1,χ(x)=1 when |x|1,χ(x)=0 when |x|2. (2.12)

    Write Rψ(x):=ψ(x). We have

     (Rk,τφ,ψ)L2(R3)=  R3Rk,τφ(x)¯ψ(x)dx=R3F{Rk,τφ}(ξ)F{R¯ψ}(ξ)dξ=  0(1χ2(rk))r2k2iτdr|ξ|=rˆφ(ξ)^R¯ψ(ξ)dS(ξ) +0r1/pr2χ2(rk)r2k2iτdr×S2[k12pˆφ(kω)][k12p^R¯ψ(kω)]dS(ω) +0r1/pr2χ2(rk)r2k2iτdrS2{[r12pˆφ(rω)][r12p^R¯ψ(rω)][k12pˆφ(kω)][k12p^R¯ψ(kω)]}dS(ω)=: I1(τ)+I2(τ)+I3(τ). (2.13)

    Here we divide (Rk,τφ,ψ)L2(R3) into three parts in order to deal with the singularity happened in the integral when |ξ| is close to k. The integral in I1 has avoided this singularity by the cutoff function χ. The singularity in I2 is only contained in the integration w.r.t. r, and it can be shown that by using Cauchy's integral theorem and choosing a proper integral path w.r.t. r, the norm of the denominator τ2k2iτ can always be bounded below by k, e.g. |τ2k2iτ|k. The singularity in I3 is compensated by the difference [] inside the integration S2[]dS(ω). In the following, we only show how to deal with I2.

    Now we estimate I1(τ). By Young's inequality abap/p+bq/q, for a,b>0,p,q>1,1/p+1/q=1 we have

    (p1/pq1/q)a1/pb1/qa+b. (2.14)

    Note that |rk|>1 in the support of the function 1χ2(rk) and |^R¯ψ(ξ)|=|ˆψ(ξ)|, one can compute

    |I1(τ)|01χ2(rk)1p1/pq1/q(r+1)1/p(k1)1/qdr|ξ|=r|ˆφ(ξ)||ˆψ(ξ)|dS(ξ)(by (2.14))Cpk1/p1φH1/(2p)δ(R3)ψH1/(2p)δ(R3), (2.15)

    where 1<p<+ and δ>0 and the Cp is independent of τ.

    We next estimate I2(τ). One has

    I2(τ)=S2[k12pˆφ(kω)][k12p^R¯ψ(kω)]0r1pr2χ2(rk)drr2k2iτdS(ω). (2.16)

    It can be shown that, by choosing a fixed τ0(0,1) carefully, we can show that the denominator pτ(r):=r2k2iτ could satisfy

    |pτ(r)|τ0kand|r|k, r{r;2|rk|τ0}Γk,τ0,τ(0,τ0), (2.17)

    where Γk,τ0:={rC;|rk|=τ0,r0}. It is obvious that the purpose of (2.17) is to use Cauchy's integral theorem. By combining (2.17) with Cauchy's integral theorem, we can continue (2.16) as

    |I2(τ)||ξ|=kξ12p|ˆφ(ξ)|ξ12p|ˆψ(ξ)|({rR+;2|rk|τ0}r1p(r/k)2τ0kdr)dS(ξ)   +|ξ|=kξ12p|ˆφ(ξ)|ξ12p|ˆψ(ξ)|(Γk,τ0(1+|r|2)12p(|r|/k)2τ0kdr)dS(ξ)Cτ0|ξ|=kξ12p|ˆφ(ξ)|ξ12p|ˆψ(ξ)|(Γk,τ0{rR+;2|rk|τ0}k1/pτ0kdr)dS(ξ)   +Cτ0|ξ|=kξ12p|ˆφ(ξ)|ξ12p|ˆψ(ξ)|(Γk,τ0k1/pτ0kdr)dS(ξ)Cτ0k1/p1(|ξ|=k|ξ12pˆh(ξ)|2dS(ξ))12(|ξ|=k|ξ12pˆψ(ξ)|2dS(ξ))12Cτ0,ϵk1/p1φH1/(2p)1/2+ϵ(R3)ψH1/(2p)1/2+ϵ(R3), (2.18)

    where the constant Cτ0,ϵ is independent of τ. Here, in deriving the last inequality in (2.18), we have made use of (2.3).

    Finally, we estimate I3(τ). Denote F(rω)=Fr(ω):=r1/(2p)ˆφ(rω) and G(rω)=Gr(ω):=r1/(2p)^Rˉψ(rω). One can compute

    |I3(τ)|0r1/pχ2(rk)|r2k2|FrL2(S2r)(r2S2|GrGk|2dS(ω))12dr   +0r1/pχ2(rk)|r2k2|(r2S2|FrFk|2dS(ω))12(rk)2GkL2(S2k)dr, (2.19)

    where S2r signifies the central sphere of radius r. Combining [13,Remark 13.1 and (13.28)] and (2.3) and (2.14), we can continue (2.19) as

    |I3(τ)|Cα,ϵ0r1/pχ2(rk)|rk|(r+k)FH1/2+ϵ(R3)|rk|αGH1/2+ϵ(R3)drCα,ϵ,p0r1/pχ2(rk)|rk|1α(r+1)1/p(k1)11/pdrFH1/2+ϵ(R3)GH1/2+ϵ(R3)Cα,ϵ,pk1/p1φH1/(2p)1/2+ϵ(R3)ψH1/(2p)1/2+ϵ(R3), (2.20)

    where the ϵ can be any positive real number and the α satisfies 0<α<ϵ, and the constant Cα,ϵ,p is independent of τ.

    Combining (2.13), (2.15), (2.18) and (2.20), we arrive at

    |(Rk,τφ,ψ)L2(R3)||I1(τ)|+|I2(τ)|+|I3(τ)|Ck1/p1φH1/(2p)1/2+ϵ(R3)ψH1/(2p)1/2+ϵ(R3),

    which implies that

    Rk,τφH1/(2p)1/2ϵ(R3)Ck1/p1φH1/(2p)1/2+ϵ(R3) (2.21)

    for some constant C independent of τ.

    Next we investigate the limiting case limτ0+Rk,τφ. Following similar steps when dealing with I1, I2 and I3, it can be shown that for any ˜τ>0, we have

    |Ij(τ1)Ij(τ2)|˜τβk1/p1φH1/(2p)1/2+ϵ(R3)ψH1/(2p)1/2+ϵ(R3),(j=1,2,3)

    holds for τ1,τ2(0,˜τ). Therefore, we can conclude

    Rk,τ1φRk,τ2φH1/(2p)1/2ϵ(R3)˜τφH1/(2p)1/2+ϵ(R3),τ1,τ2(0,˜τ),

    and thus Rk,˜τφ converges and

    lim˜τ0+Rk,˜τφ=Rkφ in H1/(2p)1/2ϵ(R3). (2.22)

    Hence from (2.21) and (2.22) we conclude that

    RkφH1/(2p)1/2ϵ(R3)Cϵ,pk(11/p)φH1/(2p)1/2+ϵ(R3)

    holds for any 1<p<+ and any ϵ>0.

    The proof is complete.

    With the help of Lemmas 2.2 and 2.3, the direct problems can be reformulated. Readers may refer to [25,Theorem 2.1], [22,Theorem 2.3], [19,Theorem 4.3], [20,Theorem 3.3], and [24,Theorem 3.3] as examples of how to formulate the direct problems, and we omit the details here.

    In this section we consider key steps in the works [8,18,19,20,23,24]. Lemma 3.3 is crucial in the key steps of the works, and its proof relies on Lemmas 3.1 and 3.2. We shall first investigate these useful lemmas.

    Lemma 3.1 is a standard result in the field of oscillatory integral and microlocal analysis.

    Lemma 3.1. Assume α and β are multi-indexes, then the following identities hold in the oscillatory integral sense,

    Rnx×Rnξeixξdxdξ=(2π)n, (3.1)
    Rnx×Rnξeixξxαξβdxdξ=(2π)ni|α|α!δαβ. (3.2)

    Here δαβ equals to 1 when α=β and equals to 0 otherwise.

    Proof. The integral in (3.1) should be understood as oscillatory integral. Fix a cutoff function χCc(Rn) with χ(0)=1, we can compute

    Rnx×Rnξeixξdxdξ=limϵ0+eixξχ(ϵx)χ(ϵξ)dxdξ=(2π)n/2limϵ0+χ(ϵ2ξ)ˆχ(ξ)dξ. (3.3)

    Denote M=supRnχ. We have |χ(ϵ2ξ)|M<. Note that χCc(Rn), so ˆχ is rapidly decaying, thus ˆχ(ξ) is Lebesgue integrable. Therefore, we can see that ˆχ(ξ)χ(ϵ2ξ) is dominated by a Lebesgue integrable function. Thus by using Lebesgue Dominated Convergence Theorem, we can continue (3.3) as

    Rnx×Rnξeixξdxdξ=(2π)n/2ˆχ(ξ)dξ=(2π)nχ(0)=(2π)n.

    We arrive at (3.1).

    To show (3.2), we first show that

    (2π)neiyηyαηβdydη=(2π)neiyηDαη(ηβ)dydη, (3.4)

    where Dηj:=1iηj. Both the LHS and RHS in (3.4) should be understood as a oscillatory integral. Thus fix some χD(Rn) such that χ(x)1 when |x|1, we have

    \begin{align} & \iint e^{-iy\cdot \eta} y^\alpha \eta^\beta \,\mathrm{d}{y} \,\mathrm{d}{\eta} = \lim\limits_{\epsilon \to 0^+} \iint e^{-iy\cdot \eta} y^\alpha \eta^\beta \chi(\epsilon y) \chi(\epsilon \eta) \,\mathrm{d}{y} \,\mathrm{d}{\eta} \\ = & \lim\limits_{\epsilon \to 0^+} \iint (-D_\eta)^\alpha(e^{-iy\cdot \eta})\, \eta^\beta \chi(\epsilon y) \chi(\epsilon \eta) \,\mathrm{d}{y} \,\mathrm{d}{\eta} \\ = & \lim\limits_{\epsilon \to 0^+} \iint e^{-iy\cdot \eta} \chi(\epsilon y) D_\eta^\alpha \big( \eta^\beta \chi(\epsilon \eta) \big) \,\mathrm{d}{y} \,\mathrm{d}{\eta} \\ = & \lim\limits_{\epsilon \to 0^+} \sum\limits_{0 < \gamma \leq \alpha} \epsilon^{|\gamma|} \binom{\alpha}{\gamma} \iint e^{-iy\cdot \eta} \chi(\epsilon y) \cdot D_\eta^{\alpha-\gamma}(\eta^\beta) \cdot \big( \partial^\gamma \chi \big) (\epsilon \eta) \,\mathrm{d}{y} \,\mathrm{d}{\eta} \\ & \ + \iint e^{-iy\cdot \eta} D_\eta^\alpha \big( \eta^\beta \big) \,\mathrm{d}{y} \,\mathrm{d}{\eta}. \end{align} (3.5)

    As \epsilon goes to zero, we have

    \begin{align*} \iint e^{-iy\cdot \eta} \chi(\epsilon y) \cdot D_\eta^{\alpha-\gamma}(\eta^\beta) \cdot \big( \partial^\gamma \chi \big) (\epsilon \eta) \,\mathrm{d}{y} \,\mathrm{d}{\eta} \to & \ D_\eta^{\alpha-\gamma}(\eta^\beta) \cdot \big( \partial^\gamma \chi \big) (\epsilon \eta) \big|_{\eta = 0} \quad (\epsilon \to 0^+). \end{align*}

    Because \gamma > 0 , \big( \partial^\gamma \chi \big) (\epsilon \eta) \big|_{\eta = 0} = 0 . Therefore, we have

    \begin{equation} \lim\limits_{\epsilon \to 0^+} \epsilon^{|\gamma|} \sum\limits_{0 < \gamma \leq \alpha} \binom{\alpha}{\gamma} \iint e^{-iy\cdot \eta} \chi(\epsilon y) \cdot D_\eta^{\alpha-\gamma}(\eta^\beta) \cdot \big( \partial^\gamma \chi \big) (\epsilon \eta) \,\mathrm{d}{y} \,\mathrm{d}{\eta} = 0. \end{equation} (3.6)

    Combining (3.5) and (3.6), we arrive at

    \iint e^{-iy\cdot \eta} y^\alpha \eta^\beta \,\mathrm{d}{y} \,\mathrm{d}{\eta} = \lim\limits_{\epsilon \to 0^+} \iint e^{-iy\cdot \eta} y^\alpha \eta^\beta \chi(\epsilon y) \chi(\epsilon \eta) \,\mathrm{d}{y} \,\mathrm{d}{\eta} = \iint e^{-iy\cdot \eta} D_\eta^\alpha \big( \eta^\beta \big) \,\mathrm{d}{y} \,\mathrm{d}{\eta}.

    We proved (3.4).

    Then, for multi-indexes \alpha and \beta , if there exists i such that \alpha_i \neq \beta_i , say, \alpha_i > \beta_i , then D_\xi^\alpha(\xi^\beta) = 0 and so

    \begin{equation*} \int e^{ix\cdot \xi} x^\alpha \xi^\beta \,\mathrm{d}{x} \,\mathrm{d}{\xi} = \int e^{ix\cdot \xi} (-D_\xi)^\alpha (\xi^\beta) \,\mathrm{d}{x} \,\mathrm{d}{\xi} = 0. \end{equation*}

    When \alpha = \beta , we have

    \begin{equation*} \int e^{ix\cdot \xi} x^\alpha \xi^\beta \,\mathrm{d}{x} \,\mathrm{d}{\xi} = \int e^{ix\cdot \xi} (-D_\xi)^\alpha (\xi^\alpha) \,\mathrm{d}{x} \,\mathrm{d}{\xi} = \int e^{ix\cdot \xi} i^{|\alpha|} \alpha! \,\mathrm{d}{x} \,\mathrm{d}{\xi} = (2\pi)^n i^{|\alpha|} \alpha!. \end{equation*}

    We have arrived at (3.2).

    We also need [16,Lemma 18.2.1] and we present a proof below.

    Lemma 3.2. If a \in S^m( {\mathbb{R}^n} \times \mathbb{R}^k) and u is defined by the oscillatory integral

    u(x) = \int e^{i 〈x',\xi'〉} a(x,\xi') \,\mathrm{d}{\xi}',

    then there exists \tilde a \in S^m( \mathbb{R}^{n-k} \times \mathbb{R}^k) such that

    u(x) = \int e^{i 〈x',\xi'〉} \tilde a(x'',\xi') \,\mathrm{d}{\xi}',

    and \tilde a has the asymptotic expansion

    \tilde a(x'',\xi') \sim \sum\limits_{\alpha} i^{|\alpha|} \partial_{x'}^\alpha \partial_{\xi'}^\alpha a(0,x'',\xi') / \alpha!.

    Remark 3.1. Note if a(x,\xi') = 0 near \{x' = 0\} , e.g. a(x,\xi) = (1 - \chi(x')) a'(x,\xi) for some a' and some cutoff function satisfying \chi(y) \equiv 1 near the origin, then Lemma 3.2 implies that \tilde a \in S^{-\infty} .

    Proof. The \tilde a(x'',\cdot) is the Fourier transform of u(\cdot,x'') with some constants, i.e.

    \tilde a(x'',\xi') = (2\pi)^{-k/2} \mathcal{F}_{x'} \{ u(x',x'') \}(\xi') = (2\pi)^{-k} \int e^{-ix' \cdot \xi'} u(x',x'') \,\mathrm{d}{x}'.

    Then we can have

    \begin{align*} \tilde a(x'',\xi') & = (2\pi)^{-k} \int e^{-ix' \cdot \xi'} u(x) \,\mathrm{d}{x}' = (2\pi)^{-k} \int e^{ix' \cdot \theta} a(x,\xi' + \theta) \,\mathrm{d}{\theta} \,\mathrm{d}{x}'. \end{align*}

    By adopting the way used in [1,§I.8.1] in computing the oscillatory integral, we can easily show that {|\partial_{x''}^\alpha \partial_{\xi'}^\beta \tilde a(x'',\xi)| \lesssim 〈\xi'〉^{m - |\beta|}} , and this can be seen by the fact that

    |\partial_{\xi'}^\alpha [\chi(x,\theta) a(2^k x',x'',\xi' + 2^k \theta)]| \lesssim 2^{mk} 〈\xi'〉^k,

    so \tilde a \in S^m( \mathbb{R}^{n-k} \times \mathbb{R}^k) .

    The idea of the proof is to expand a(x',x'', \xi' + \theta) in terms of x' and \theta by Taylor expansion

    \begin{align} a(x',x'',\xi' + \theta) & = \sum\limits_{|\alpha| + |\beta| \leq 2N} \frac {x'^\alpha \theta^\beta}{\alpha! \beta!} \partial_{x'}^\alpha \partial_{\xi'}^\beta a(0, x'',\xi') \\ & \quad + \sum\limits_{|\alpha| + |\beta| = 2N+1} \frac {x'^\alpha \theta^\beta}{\alpha! \beta!} \partial_{x'}^\alpha \partial_{\xi'}^\beta a(\eta x', x'',\xi' + \eta \theta), \quad 0 < \eta < 1, \end{align}

    and to use Lemma 3.1. We have

    \begin{align} \tilde a(x'', \xi') & = (2\pi)^{-k} \int e^{ix' \cdot \theta} a(x',x'',\xi' + \theta) \,\mathrm{d}{\theta} \,\mathrm{d}{x}' \\ \\ & = \sum\limits_{|\alpha| \leq N} i^{|\alpha|} \partial_{x'}^\alpha \partial_{\xi'}^\beta a(0, x'',\xi') / \alpha! \\ & \quad + \sum\limits_{\substack{|\alpha| + |\beta| = 2N+1 \\ \gamma \leq \alpha \leq \beta + \gamma}} C_{\alpha,\beta,\gamma} \int e^{ix' \cdot \theta} (\partial_{x'}^\alpha \partial_{\xi'}^{\beta + \gamma} a) (\eta^{|\gamma|}) \partial_\theta^{\alpha - \gamma} (\theta^\beta) \,\mathrm{d}{\theta} \,\mathrm{d}{x}' . \end{align} (3.7)

    Note that the constraint \alpha \leq \beta + \gamma in (3.7) comes from the fact that \partial_\theta^{\alpha - \gamma} (\theta^\beta) = 0 when \alpha > \beta + \gamma . Moreover, the constraint " |\alpha| + |\beta| = 2N+1,\, \gamma \leq \alpha \leq \beta + \gamma " gives

    \begin{equation*} 2N + 1 = |\alpha| + |\beta| \leq 2|\beta| + |\gamma| \leq 2(|\beta| + |\gamma|) \quad \Rightarrow \quad |\beta + \gamma| \geq N + 1. \end{equation*}

    Now we show that each remainder term in (3.7) is controlled by 〈\xi'〉^{m-N-1} . Denote b(x', x'', \theta; \xi',\eta) = \big( \partial_{x'}^\alpha \partial_{\xi'}^{\beta + \gamma} a(\eta x', x'', \xi' + \eta \theta) \big) (\eta^{|\gamma|}) \partial_\theta^{\alpha - \gamma} (\theta^\beta) with underlining assumptions \beta + \gamma \geq \alpha and |\beta + \gamma| \geq N + 1 , and we have

    \begin{align*} &\tilde a(x'', \xi') - \sum\limits_{|\alpha| \leq N} i^{|\alpha|} \partial_{x'}^\alpha \partial_{\xi'}^\beta a(0, x'',\xi') / \alpha!\\ & = \int e^{ix' \cdot \theta} \chi_0(x',\theta) b \,\mathrm{d}{\theta} \,\mathrm{d}{x}' \nonumber \\ & \quad + \sum\limits_{\ell \geq 1} \int e^{ix' \cdot \theta} \chi(x'/2^\ell,\theta/2^\ell) b(x', x'', \theta; \xi',\eta) \,\mathrm{d}{\theta} \,\mathrm{d}{x}', \end{align*}

    where \chi_0 and \chi is as in [1,§I.8.1]. Here we only show how the second term in the equation above is controlled by 〈\xi'〉^{m-N-1} . The computation is as follows,

    \begin{align} & \int e^{ix' \cdot \theta} \chi(x'/2^\ell,\theta/2^\ell) b(x', x'', \theta; \xi',\eta) \,\mathrm{d}{\theta} \,\mathrm{d}{x}' \\ \lesssim & \ 2^{2\ell k} \int \big( \frac {(\theta,x') \cdot \nabla_{(x',\theta)}} {i2^{2\ell} (|x'|^2+|\theta|^2)} \big)^L (e^{i 2^{2\ell} x' \cdot \theta}) \cdot \chi(x',\theta) b(x', x'', \theta; \xi', 2^\ell \eta) \,\mathrm{d}{\theta} \,\mathrm{d}{x}' \\ \lesssim & \ 〈\xi'〉^{m-N-1} \cdot 2^{\ell(2k + 1 - 2L)} \int_{ \mathop{{\rm{supp}}} \chi} C_L 2^{\ell (|m-N-1|+L)} \,\mathrm{d}{\theta} \,\mathrm{d}{x}' \\ \lesssim & \ 〈\xi'〉^{m-N-1} \cdot 2^{\ell(2k + 1 + |m-N-1| - L)}, \end{align}

    thus if we take L to be large enough such that 2k + 1 + |m-N-1| - L < 0 , we can have

    |\sum\limits_{\ell \geq 1} \int e^{ix' \cdot \theta} \chi(x'/2^\ell,\theta/2^\ell) b \,\mathrm{d}{\theta} \,\mathrm{d}{x}'| \lesssim \sum\limits_{\ell \geq 1} 〈\xi'〉^{m-N-1} 2^{\ell(2k + 1 + |m-N-1| - L)} \lesssim 〈\xi'〉^{m-N-1}.

    This shows |\tilde a(x'', \xi') - \sum_{|\alpha| \leq N} i^{|\alpha|} \partial_{x'}^\alpha \partial_{\xi'}^\alpha a(0,x'',\xi') / \alpha!| \lesssim 〈\xi'〉^{m-N-1} . Using the same procedure, we can show \big| \partial_{x''}^\kappa \partial_{\xi'}^\beta [\tilde a(x'', \xi') - \sum_{|\alpha| \leq N} i^{|\alpha|} \partial_{x'}^\alpha \partial_{\xi'}^\alpha a(0,x'',\xi') / \alpha!] \big| \lesssim 〈\xi'〉^{m-N-1 - |\beta|} , and hence

    \tilde a(x'', \xi') - \sum\limits_{|\alpha| \leq N} i^{|\alpha|} \partial_{x'}^\alpha \partial_{\xi'}^\alpha a(0,x'',\xi') / \alpha! \in S^{m-N-1}( \mathbb{R}^{n-k} \times \mathbb{R}^k).

    The proof is complete.

    We also need [16,Lemma 18.2.9] and we present a proof below.

    Lemma 3.3. Assume that a \in S^m and

    u(x) = \int e^{i 〈x', \xi'〉} a(x,\xi') \,\mathrm{d}{\xi}', \quad \xi' \in \mathbb{R}^k,

    and a C^\infty diffeomorphism \rho \colon y \in {\mathbb{R}^n} \mapsto \rho(y) = (\rho_1(y), \rho_2(y)) \in {\mathbb{R}^n} preserving the hyperplane S = \{ x \,;\, x' = 0 \} . The \rho_1 is k -dimensional while \rho_2 is (n-k) -dimensional. Assume u and the pull-back \rho^* u is C^\infty -smooth in {\mathbb{R}^n} \backslash S , then there exists \tilde a \in S^m( \mathbb{R}^{n-k} \times \mathbb{R}^k) such that \rho^* u can be represented as

    \rho^* u(y) = \int e^{i 〈y', \xi'〉} \tilde a(y'',\xi') \,\mathrm{d}{\xi}',

    and

    \tilde a(y'',\eta) - a(0,\rho_2(0,y''),(\psi(0,y''))^{T,-1} \eta) |\det\psi(0,y'')|^{-1} \in S^{m-1}( \mathbb{R}^{n-k} \times \mathbb{R}^k),

    where (*)^T and (*)^{T,-1} signify the transpose and transpose with inverse of a matrix, respectively.

    Remark 3.2. The condition " u and \rho^* u is C^\infty -smooth in {\mathbb{R}^n} \backslash S " is indispensable.

    Proof. Because \rho preserves the hyperplane \{ x \,;\, x' = 0 \} , there exists a C^\infty matrix-valued function \psi such that \rho_1(y',y'') = \psi(y) \cdot y' , where the dot operation " \cdot " here signifies the matrix multiplication. According to Lemma 3.2, there exist \bar a \in S^m such that \(u(x) = \int e^{i 〈x', \xi'〉} \bar a(x'', \xi') \, \mathrm{d}{\xi}'. \) Hence we have

    \begin{align*} \tilde u(y) & : = \rho^* u(y) = u(\rho(y)) = \int e^{i 〈\rho_1(y), \xi'〉} \bar a(\rho_2(y),\xi') \,\mathrm{d}{\xi}' \\ & = \int e^{i 〈\psi(y) \cdot y', \xi'〉} \bar a(\rho_2(y),\xi') \,\mathrm{d}{\xi}' = \int e^{i 〈y', (\psi(y) )^{T} \xi'〉} \bar a(\rho_2(y),\xi') \,\mathrm{d}{\xi}', \nonumber \end{align*}

    According to Remark 3.1, we could continue

    \begin{align*} \tilde u(y) & = \int e^{i 〈y', (\psi(y))^{T} \xi'〉} \chi(y') \bar a(\rho_2(y),(\psi(y))^{T,-1} (\psi(y))^{T} \xi') |\det\psi(y)|^{-1} {\rm{d}} ((\psi(y) )^{T} \xi') + v(y) \nonumber \\ & = \int e^{i 〈y', \eta〉} \chi(y') \bar a(\rho_2(y),(\psi(y))^{T,-1} \eta) |\det\psi(y)|^{-1} \,\mathrm{d}{\eta} + v(y), \nonumber \end{align*}

    where \chi \in C_c^\infty( \mathbb{R}^k) with \chi(y') \equiv 1 in a neighborhood 0 such that the matrix \psi(y) is invertible in \mathop{{\rm{supp}}} \psi , and v(y) = \int e^{i 〈y', \eta〉} b(y'',\eta) \,\mathrm{d}{\eta} with b \in S^{-\infty} . Using Lemma 3.2, we obtain \(\tilde u(y) = \int e^{i 〈y', \eta〉} \tilde a(y'', \eta) \, \mathrm{d}{\eta} \) where

    \tilde a(y'',\eta) - \bar a(\rho_2(0,y''),(\psi(0,y''))^{T,-1} \eta) |\det\psi(0,y'')|^{-1} \in S^{m-1}( \mathbb{R}^{n-k} \times \mathbb{R}^k).

    Note that \bar a satisfies \(\bar a(x'', \xi') - a(0, x'', \xi') \in S^{m-1}(\mathbb{R}^{n-k} \times \mathbb{R}^k), \) so

    \tilde a(y'',\eta) - a(0,\rho_2(0,y''),(\psi(0,y''))^{T,-1} \eta) |\det\psi(0,y'')|^{-1} \in S^{m-1}( \mathbb{R}^{n-k} \times \mathbb{R}^k).

    The proof is complete.

    Finally, we need Lemma 3.4.

    Lemma 3.4. For any stochastic process \{g(k,\omega)\}_{k \in \mathbb{R}_+} satisfying

    \begin{equation} \int_1^{+\infty} k^{m-1} \mathbb E (|g(k,\cdot)|) \,\mathrm{d}{k} < +\infty, \end{equation} (3.8)

    it holds that

    \begin{equation} \lim\limits_{K \to +\infty} \frac 1 K \int_K^{2K} k^m g(k,\omega) \,\mathrm{d}{k} = 0, \ \rm{\; a.s.\; } \omega \in \Omega. \end{equation} (3.9)

    Proof. Check [22,Lemma 4.1].

    Lemma 3.4 turns the justification of the ergodicity into the asymptotic analysis of the expectation of related terms.

    With the help of Lemma 3.4, the most difficult part of the work [18,19,20,23,24] boils down to the estimate of the integral

    \begin{equation} \mathbb I (x,y,k_1,k_2) : = \int e^{ik_1(|x - z_1| + |z_1 - y|) - ik_2(|x - z_2| + |z_2 - y|)} C(z_1,z_2) \,\mathrm{d}{z_1} \,\mathrm{d}{z_2}, \end{equation} (3.10)

    where C(z_1,z_2) = \int e^{i (z_1 - z_2) \cdot \xi} c(z_1,\xi) \,\mathrm{d}{\xi} and c \in S^{-m} . Readers may refer to [19,(30)-(31)], [20,(3.21) and (3.24)], [24,(4.2) and (2.1)] as well as [23,Theorems 3.1 and 3.3] as examples.

    One wonders the decaying rate of \mathbb I in terms of k_1 and k_2 , and after we got the decaying rate, we substitute this estimate into (3.8). If \mathbb I decays fast enough in terms of k_1 and/or k_2 , the corresponding integral in (3.8) will be finite and we can obtain some asymptotic ergodicity like (3.9). This is the principal idea in [18,19,20,23,24].

    Proposition 3.1. Assume \mathbb I is defined as in (3.10) and C(z_1,z_2) = \int e^{i (z_1 - z_2) \cdot \xi} c(z_1,\xi) \,\mathrm{d}{\xi} with c \in S^{-m} is a symbol. Then for \forall N \in \mathbb N there exists constants C_N > 0 such that

    |\mathbb I (x,y,k_1,k_2)| \leq C_N 〈k_1 - k_2〉^{-N} (k_1 + k_2)^{-m},

    holds uniformly for x , y .

    Proof. Denote \phi(z_1,z_2, x,y, k_1, k_2) : = k_1(|x - z_1| + |z_1 - y|) - k_2(|x - z_2| + |z_2 - y|) , then \mathbb I = \int e^{i\phi} C \,\mathrm{d}{z_1} \,\mathrm{d}{z_2} and \phi is the phase function. We have

    \begin{align} \phi(z_1,z_2, x,y, k_1, k_2) & = \frac {k_1 + k_2} 2 \big[ (|x - z_1| + |z_1 - y|) - (|x - z_2| + |z_2 - y|) \big] \\ & \quad + \frac {k_1 - k_2} 2 \big[ (|x - z_1| + |z_1 - y|) + (|x - z_2| + |z_2 - y|) \big]. \end{align} (3.11)

    We note that the xyz part of the second term in (3.11) is always positive and the first term equals to zero when z_1 = z_2 . Also, the function C will be singular when z_1 = z_2 . Therefore, the situation near the hyperplane S_0 : = \{ z_1 = z_2 \} is crucial for the behavior of \mathbb I regarding the decaying rate in terms of k_1 , k_2 . Therefore, we are willing to do a change of variables inside the integral (3.10) such that the hyperplane S_0 can be featured by a single variable, i.e. S_0 = \{v = 0\} for some variable v . To be specific, we choose the change of variables \tau_1(z_1, z_2) = (v,w) where

    \begin{equation*} \tau_1 \colon \quad v = z_1 - z_2, \quad w = z_1 + z_2. \end{equation*}

    The pull-back of C under \tau_1^{-1} is

    \begin{equation} C_1(v,w) : = (\tau_1^{-1})^* C(v,w) = C(\tau_1^{-1}(v,w)) = \int e^{i v \cdot \xi} c((v + w)/2,\xi) \,\mathrm{d}{\xi}. \end{equation} (3.12)

    Second, in order to make the phase function \phi more easy to handle, we are also willing to do another change of variables such that \phi can be represented in the form of inner products, i.e. \phi = s \cdot t for some s and t depending on x , y , z_1 , z_2 , k_1 and k_2 . One of the choices is \tau_2(z_1, z_2) = (s,t) , s = (s_1,\cdots, s_n) \in {\mathbb{R}^n} and t = (t_1,\cdots, t_n) \in {\mathbb{R}^n} where

    \begin{equation} \tau_2 \colon \quad \left\{ \begin{aligned} s_1 & = (|x - z_1| + |z_1 - y|) - (|x - z_2| + |z_2 - y|), \\ t_1 & = (|x - z_1| + |z_1 - y|) + (|x - z_2| + |z_2 - y|). \end{aligned} \right. \end{equation} (3.13)

    We comment that under (3.13), the phase function \phi will only depend on s_1 and t_1 , and the choice of s_j and t_j\; (j = 2,\cdots, n) is inessential as long as the change of variables \tau_2 is a diffeomorphism. Hence we omit the precise definitions of s_j and t_j (j > 1) and readers may refer to [18,19,20,23,24] for more details. Another thing to note is the map \tau_1 \circ \tau_2^{-1} preserves S_0 , i.e. \tau_1 \circ \tau_2^{-1}(0,t) = (0,w) . By Lemma 3.3, there exists a symbol c_2 \in S^{-m} such that the pull-back of C_1 under \tau_1 \circ \tau_2^{-1} is

    \begin{equation} C_2(s,t) : = (\tau_1 \circ \tau_2^{-1})^* C_1(s,t) = \int e^{i s \cdot \xi} c_2(t,\xi) \,\mathrm{d}{\xi}, \end{equation} (3.14)

    By using Lemma 3.3, we can express c_2 by c , \tau_1 and \tau_2 , which involves some detailed computations. Note that we only need the leading term of c_2 so the computations wouldn't be too complicated.

    The relationship (3.14) also gives

    C_2(s,t) = (\tau_1 \circ \tau_2^{-1})^* (\tau_1^{-1})^* C(s,t) = (\tau_2^{-1})^* C(s,t),

    and hence we can do the change of variables \tau_2 in (3.10) to obtain

    \begin{align} &\mathbb I (x,y,k_1,k_2) \\ & = \int e^{ik_1(|x - z_1| + |z_1 - y|) - ik_2(|x - z_2| + |z_2 - y|)} C(\tau_2^{-1} \circ \tau_2(z_1,z_2)) {\rm{d}} (\tau_2^{-1} \circ \tau_2(z_1,z_2)) \\ & = \int e^{i(k_1 + k_2) s_1 / 2 + i(k_1 - k_2) t_1 / 2} C(\tau_2^{-1} (s,t)) |\det \tau_2^{-1}(s,t)| {\rm{d}} (s,t) \\ & = \int e^{i(k_1 + k_2) s \cdot e_1 / 2 + i(k_1 - k_2) t \cdot e_1 / 2} C_2(s,t) |\det \tau_2^{-1}(s,t)| \,\mathrm{d}{s} \,\mathrm{d}{t}. \end{align} (3.15)

    Here we need the help of Lemma 3.2 to deal with the |\det \tau_2^{-1}(s,t)| term: there exists a symbol \tilde c_2 \in S_{-m} such that

    \begin{equation} C_2(s,t) |\det \tau_2^{-1}(s,t)| = \int e^{i s \cdot \xi} \tilde c_2(t,\xi) \,\mathrm{d}{\xi}. \end{equation} (3.16)

    The computation of the leading term of \tilde c_2 is straight forward,

    \tilde c_2(t,\xi) - c_2(t,\xi) |\det \tau_2^{-1}(0,t)| \in S^{-m-1}.

    Combining (3.15) and (3.16), we arrive at

    \begin{align*} \mathbb I (x,y,k_1,k_2) & = \int e^{i(k_1 + k_2) s \cdot e_1 / 2 + i(k_1 - k_2) t \cdot e_1 / 2} \int e^{i s \cdot \xi} \tilde c_2(t,\xi) \,\mathrm{d}{\xi} \,\mathrm{d}{s} \,\mathrm{d}{t} \\ & \simeq \int e^{i(k_1 - k_2) t \cdot e_1 / 2} \tilde c_2(t,-(k_1 + k_2)e_1 / 2) \,\mathrm{d}{t}. \end{align*}

    Now we can see \mathbb I is decaying at the rate of 〈k_1 - k_2〉^{-N} (k_1 + k_2)^{-m} for arbitrary N \in \mathbb N .

    We would like to comment that the estimation of \mathbb I is difficult due to the presence of the norm inside the phase function \phi . However, the designs of \tau_1 and \tau_2 in the arguments above are so peculiar that the estimate of \mathbb I is possible.

    In this section we consider the key steps in the works [22,25]. In [22,25], the authors use far-field data to achieve the recovery, and this makes the derivations different from what has been discussed in Section 3. A different methodology is required to obtain accurate estimate of the decaying rate. Lemmas 4.1–4.3 plays key roles in the derivation. Before stepping into the key steps in the derivation, we shall first investigate some useful lemmas.

    First, let us recall the notion of the fractional Laplacian [30] of order s \in (0,1) in \mathbb{R}^n ( n\geq 3 ),

    \begin{equation} (-\Delta)^{s/2} \varphi(x) : = (2\pi)^{-n} \iint e^{i(x-y) \cdot \xi} |\xi|^s \varphi(y) \,\mathrm{d}{y} \,\mathrm{d}{\xi}, \end{equation} (4.1)

    where the integration is defined as an oscillatory integral. When \varphi \in \mathscr{S}( {\mathbb{R}^n}) , (4.1) can be understood as a usual Lebesgue integral if one integrates w.r.t. y first and then integrates w.r.t. \xi . By duality arguments, the fractional Laplacian can be generalized to act on wider range of functions and distributions (cf. [32]). It can be verified that the fractional Laplacian is self-adjoint.

    In the following two lemmas, we present the results in a more general form where the space dimension n can be arbitrary but greater than 2, though only the case n = 3 shall be used subsequently.

    Lemma 4.1. For any s \in (0,1) , we have

    \begin{equation*} (-\Delta_\xi)^{s/2} (e^{ix \cdot \xi}) = |x|^s e^{ix \cdot \xi} \end{equation*}

    in the distributional sense.

    Proof. Check [22,Lemma 3.1].

    Lemma 4.2. For any m < 0 and s \in (0,1) , we have

    \big( (-\Delta_\xi)^{s/2} c \big) (x,\xi) \in S^{m-s} \quad \mathit{\text{for any}} \quad c(x,\xi) \in S^m.

    Proof. Check [22,Corollary 3.1].

    In the sequel, we denote \mathop{{\rm{diam}}}(\Omega) : = \sup\limits_{x, x' \in \Omega} \{ |x - x'|\} .

    Lemma 4.3. Assume \Omega is a bounded domain in {\mathbb{R}^n} . For \forall \alpha, \beta \in \mathbb{R} such that \alpha < n and \beta < n , and for \forall p \in {\mathbb{R}^n} \backslash \{0\} , there exists a constant C_{\alpha,\beta} independent of p and \Omega such that

    \begin{equation*} \int_\Omega |t|^{-\alpha} |t - p|^{-\beta} \,\mathrm{d}{t} \leq C_{\alpha,\beta} \times \begin{cases} |p|^{n - \alpha - \beta} + ( \mathop{{\rm{diam}}} (\Omega))^{n - \alpha - \beta}, & \alpha + \beta \neq n, \\ \ln \frac 1 {|p|} + \ln ( \mathop{{\rm{diam}}}(\Omega)) +C_{\alpha, \beta}, & \alpha + \beta = n. \end{cases} \end{equation*}

    Proof. Check [25,Lemma 3.5].

    In this subsection we restrict ourselves to \mathbb{R}^3 . One of the key difficulty in [22] is to obtain an asymptotics about a integral

    \begin{equation} \mathbb J : = \int e^{ik\varphi(y,s,z,t)} \big( \int e^{i(z-y) \cdot \xi} c_q(z,\xi) \,\mathrm{d}{\xi} \big) \big( \int e^{i(t-s) \cdot \eta} c_f(t,\xi) \,\mathrm{d}{\eta} \big) \,\mathrm{d}{{(s, y, t, z)}}, \end{equation} (4.2)

    in terms of k , where \varphi(y,s,z,t) : = -\hat x \cdot (y-z) - |y-s| + |z-t| , c_q \in S^{-m_q} and c_f \in S^{-m_f} with m_q , m_f satisfying the requirement in Theorem 1.6, \,\mathrm{d}{{(s, y, t, z)}} is a short notation for \,\mathrm{d}{s} \,\mathrm{d}{y} \,\mathrm{d}{t} \,\mathrm{d}{z} , and y,z \in D_q and s,t \in D_f two convex domains D_q and D_f satisfying (1.5). Recall the definition of the unit normal vector \boldsymbol{n} after (1.5). We introduce two differential operators with C^\infty -smooth coefficients as follows,

    \begin{equation*} L_1 : = \frac {(y-s) \cdot \nabla_s} {ik|y-s|}, \quad L_2 = L_{2,\hat x} : = \frac {\nabla_y \varphi \cdot \nabla_y} {ik|\nabla_y \varphi|}, \end{equation*}

    where {\nabla_y \varphi = \frac {s-y} {|s-y|} - \hat x} . The operator L_{2,\hat x} depends on \hat x because \nabla_y \varphi does. Due to the fact that y \in D_q while s \in D_f , the operator L_1 is well-defined. It can be verified there is a positive lower bound of |\nabla_y \varphi| for all \hat x\in \{\hat x \in \mathbb{S}^2 \colon \hat x \cdot \boldsymbol{n} \geq 0\} . It can also be verified that

    L_1 (e^{ik\varphi(y,s,z,t)}) = L_2 (e^{ik\varphi(y,s,z,t)}) = e^{ik\varphi(y,s,z,t)}.

    In what follows, we shall use { \mathcal{C}(\cdot)} and its variants, such as { \mathcal{\vec C}(\cdot)} , { \mathcal{C}_{a,b}(\cdot)} etc., to represent some generic smooth scalar/vector functions, within C_c^\infty( \mathbb{R}^3) or C_c^\infty( \mathbb{R}^{3 \times 4}) , whose particular definition may change line by line. By using integration by parts, one can compute

    \begin{align} \mathbb J = & \int \big( L_1^2 L_2^2 \big) (e^{ik\varphi(y,s,z,t)}) \cdot \big( \int e^{i(z-y) \cdot \xi} c_q(z,\xi) \,\mathrm{d}{\xi} \big) \cdot \big( \int e^{i(t-s) \cdot \eta} c_f(t,\eta) \,\mathrm{d}{\eta} \big) \,\mathrm{d}{{(s, y, t, z)}} \\ \simeq & \ k^{-4} \int_{\mathcal D} e^{ik\varphi(y,s,z,t)} \big[ \mathcal J_1\, (\mathcal K_1\, \mathcal{C} + \vec{\mathcal K}_2 \cdot \vec{ \mathcal{C}} + \sum\limits_{a,b = 1,2,3} \mathcal K_{3;a,b}\, \mathcal{C}_{a,b}) \\ & \ + \sum\limits_{c = 1,2,3} \mathcal J_{2;c}\, (\mathcal K_1\, \mathcal{C}_c + \vec{\mathcal K}_2 \cdot \vec{ \mathcal{C}}_c + \sum\limits_{a,b = 1,2,3} \mathcal K_{3;a,b}\, \mathcal{C}_{a,b,c}) \\ & \ + \sum\limits_{a',b' = 1,2,3} \mathcal J_{3;a',b'} (\mathcal K_1\, \mathcal{C}_{a',b'} + \vec{\mathcal K}_2 \cdot \vec{ \mathcal{C}}_{a',b'} + \sum\limits_{a,b = 1,2,3} \mathcal K_{3;a,b}\, \mathcal{C}_{a,b,a',b'}) \big] \,\mathrm{d}{{(s, y, t, z)}}, \end{align} (4.3)

    where the integral domain \mathcal D \subset \mathbb{R}^{3 \times 4} is bounded and

    \begin{alignat*} {2} & \mathcal J_1 : = \int e^{i(t-s) \cdot \eta}\, c_f(t,\eta) \,\mathrm{d}{\eta}, & \quad & \mathcal K_1 : = \int e^{i(z-y) \cdot \xi}\, c_q(z,\xi) \,\mathrm{d}{\xi}, \\ & \vec{\mathcal J}_2 : = \nabla_s \int e^{i(t-s) \cdot \eta}\, c_f(t,\eta) \,\mathrm{d}{\eta}, & \quad & \vec{\mathcal K}_2 : = \nabla_y \int e^{i(z-y) \cdot \xi}\, c_q(z,\xi) \,\mathrm{d}{\xi}, \\ & \mathcal J_{3;a,b} : = \partial_{s_a,s_b}^2 \int e^{i(t-s) \cdot \eta}\, c_f(t,\eta) \,\mathrm{d}{\eta}, & \quad & \mathcal K_{3;a,b} : = \partial_{y_a,y_b}^2 \int e^{i(z-y) \cdot \xi}\, c_q(z,\xi) \,\mathrm{d}{\xi}, \end{alignat*}

    and \mathcal J_{2;c} (resp. \mathcal K_{2;c} ) is the c -th component of the vector \vec{\mathcal J}_2 (resp. \vec{\mathcal K}_2 ).

    Here we only show how to estimate \mathcal J_1 and skip the details regarding \vec{\mathcal J}_2 , \mathcal K_1 , and \vec{\mathcal K}_2 ; readers may refer to the proof of [22,Lemma 3.3] for details. For the case where s \neq t , we have

    \begin{align} |\mathcal J_1| & = |\int e^{i(t-s) \cdot \eta}\, c_f(t,\eta) \,\mathrm{d}{\eta}| = |s-t|^{-2} \cdot |\int \Delta_\eta (e^{i(s-t) \cdot \eta})\, c_f(t,\eta) \,\mathrm{d}{\eta}| \\ & = |s-t|^{-2} \cdot |\int e^{i(t-s) \cdot \eta} (\Delta_\eta c_f) (t,\eta) \,\mathrm{d}{\eta}| \leq |s-t|^{-2} \int |(\Delta_\eta c_f) (t,\eta)| \,\mathrm{d}{\eta} \\ & \lesssim |s-t|^{-2} \int 〈\eta〉^{-m_f-2} \,\mathrm{d}{\eta} \lesssim |s-t|^{-2}. \end{align} (4.4)

    Similarly, we can have

    \begin{equation} |\mathcal J_1|,\, |\vec{\mathcal J}_2|,\, |\mathcal K_1|,\, |\vec{\mathcal K}_2| \lesssim |y-z|^{-2}. \end{equation} (4.5)

    But for J_{3;a,b} , if we mimic the derivation (4.4), then

    \begin{align} \mathcal J_{3;a,b} & \simeq \int e^{i(t-s) \cdot \eta} \cdot c_f(t,\eta) \eta_a \eta_b \,\mathrm{d}{\eta} \simeq |s-t|^{-2} \int \Delta_\eta (e^{i(t-s) \cdot \eta}) \cdot c_f(t,\eta) \eta_a \eta_b \,\mathrm{d}{\eta} \\ & = |s-t|^{-2} \int e^{i(t-s) \cdot \eta} \cdot \Delta_\eta (c_f(t,\eta) \eta_a \eta_b) \,\mathrm{d}{\eta}. \end{align} (4.6)

    Note that \Delta_\eta (c_f(t,\eta) \eta_a \eta_b) \in S^{-m_f} and thus is not absolutely integrable in \mathbb{R}^3 . If we further differentiate the term e^{i(t-s) \cdot \eta} in (4.6) by \frac {i(s-t) \cdot} {|s-t|^2} \nabla_\eta and then transfer the operator \nabla_\eta onto \Delta_\eta (c_f(t,\eta) \eta_a \eta_b) by using integration by parts, we would arrive at

    \begin{equation*} |\mathcal J_{3;a,b}| \lesssim |s-t|^{-3} \int |\nabla_\eta \Delta_\eta (c_f(t,\eta) \eta_a \eta_b)| \,\mathrm{d}{\eta} \leq |s-t|^{-3} \int 〈\eta〉^{-m_f-1} \,\mathrm{d}{\eta}. \end{equation*}

    The term \int 〈\eta〉^{-m_f-1} \,\mathrm{d}{\eta} is absolutely integrable now, but the term |s-t|^{-3} is not integrable at the hyperplane s = t in \mathbb{R}^3 . To circumvent this dilemma, the fractional Laplacian can be applied as follows. By using Lemma 4.1 and 4.2, we can continue (4.6) as

    \begin{align} |\mathcal J_{3;a,b}| & \simeq |s-t|^{-2} \cdot \big| |s-t|^{-s} \int (-\Delta_\eta)^{s/2} (e^{i(t-s) \cdot \eta}) \cdot \Delta_\eta (c_f(t,\eta) \eta_j \eta_\ell) \,\mathrm{d}{\eta} \big| \\ & = |s-t|^{-2-s} \cdot |\int e^{i(t-s) \cdot \eta} \cdot (-\Delta_\eta)^{s/2} \big( \Delta_\eta (c_f(t,\eta) \eta_j \eta_\ell) \big) \,\mathrm{d}{\eta}| \\ & \lesssim |s-t|^{-2-s} \int 〈\eta〉^{-m_f+2-2-s} \,\mathrm{d}{\eta} = |s-t|^{-2-s} \int 〈\eta〉^{-m_f-s} \,\mathrm{d}{\eta}, \end{align} (4.7)

    where the number s is chosen to satisfy \max\{0, 3 - m_f\} < s < 1 , and the existence of such a number s is guaranteed by noting that m_f > 2 . Therefore, we have

    \left\{\begin{array}{l} -m_{f}-s < -3, \;\;\;\;\;\;\;\;\;\;\;\;(\rm 4.8a)\\ -2-s > -3.\;\;\;\;\;\;\;\;\;\;\;\;\;\;\;(\rm 4.8b) \end{array}\right.

    Thanks to the condition (4.8a), we can continue (4.7) as

    \begin{align} |\mathcal J_{3;a,b} | & \lesssim |s-t|^{-2-s} \int 〈\eta〉^{-m_f-s} \,\mathrm{d}{\eta} \lesssim |s-t|^{-2-s}. \end{align} (4.9)

    Using similar arguments, we can also conclude that K_{3;a,b}| \lesssim |y-z|^{-2-s} .

    Combining (4.3), (4.5) and (4.9), we arrive at

    \begin{align} |\mathbb J| & \lesssim k^{-4} \int_{\mathcal D} (|\mathcal J_1| + |\vec{\mathcal J}_2| + \sum\limits_{a',b' = 1,2,3} |\mathcal J_{3;a',b'}|) \cdot (|\mathcal K_1| + |\vec{\mathcal K}_2| + \sum\limits_{a,b = 1,2,3} |\mathcal K_{3;a,b}|) \,\mathrm{d}{{(s, y, t, z)}} \\ & \lesssim k^{-4} \int_{\widetilde{\mathcal D}} |s - t|^{-2-s} \,\mathrm{d}{s} \,\mathrm{d}{t} \cdot \int_{\widetilde{\mathcal D}} |y - z|^{-2-s} \,\mathrm{d}{y} \,\mathrm{d}{z} \end{align} (4.10)

    for some sufficiently large but bounded domain \widetilde{\mathcal D} \subset \mathbb{R}^{3 \times 2} satisfying \mathcal D \subset \widetilde{\mathcal D} \times \widetilde{\mathcal D} . Note that the integral (4.10) should be understood as a singular integral because of the presence of the singularities occurring when s = t and y = z . By (4.10) and (4.8b), we can finally conclude \(|\mathbb J| \lesssim k^{-4}, \) as k be large enough.

    In this subsection we restrict ourselves to \mathbb{R}^3 . We note that in (4.2), the domains D_q and D_f are assumed to be separated by two convex hulls. This condition is relaxed in [25] and the corresponding details in the proof is also modified. One of the key difficulty in [25] is to obtain an asymptotics about a integral

    \begin{equation} \mathbb K(x,y) : = \iint_{D_f \times D_f} K_f(s,t) \Phi(s-y; k_1) \overline \Phi(t-x; k_2) \,\mathrm{d}{{s}} \,\mathrm{d}{{t}}, \end{equation} (4.11)

    where K_f is the kernel of the covariance operator of the migr field f (cf. (2.4)), and \Phi is defined in the beginning of Section 2.1. From (4.11) we have

    \begin{align} \mathbb K(z,y) & \simeq \iint_{\widetilde{\mathcal D} \times \widetilde{\mathcal D}} e^{ik_1|s-y| -ik_2|t-z|} \big( |s-y|^{-1} |t-z|^{-1} \int e^{i(s-t) \cdot \xi} c(s,\xi) \,\mathrm{d}{{\xi}} \big) \,\mathrm{d}{{s}} \,\mathrm{d}{{t}}. \end{align} (4.12)

    Define two differential operators

    L_1 : = \frac {(s-y) \cdot \nabla_s} {ik_1|s-y|} \quad \text{and} \quad L_2 : = \frac {(t-z) \cdot \nabla_t} {-ik_2|t-z|}.

    It can be verified that

    L_1 L_2 (e^{ik_1|s-y|-ik_2|t-z|}) = e^{ik_1|s-y|-ik_2|t-z|}.

    Hence, noting that the integrand is compactly supported in \widetilde{\mathcal D} \times \widetilde{\mathcal D} and by using integration by part, we can continue (4.12) as

    \begin{align} & \ |\mathbb K(z,y) | \\ \simeq & \ |\iint_{\widetilde{\mathcal D} \times \widetilde{\mathcal D}} L_1 L_2 (e^{ik_1|s-y| -ik_2|t-z|}) \big( |s-y|^{-1} |t-z|^{-1} \int e^{i(s-t) \cdot \xi} c_1(s,t,z,y,\xi) \,\mathrm{d}{{\xi}} \big) \,\mathrm{d}{{s}} \,\mathrm{d}{{t}}| \\ \lesssim & \ k_1^{-1} k_2^{-1} \iint_{\widetilde{\mathcal D} \times \widetilde{\mathcal D}} \big[ |s-y|^{-2} |t-z|^{-2} \mathcal J_0 + |s-y|^{-2} |t-z|^{-1} (\max\limits_a \mathcal J_{1;a}) \\ & + |s-y|^{-1} |t-z|^{-2} (\max\limits_{a}\mathcal J_{1;a}) + |s-y|^{-1} |t-z|^{-1} (\max\limits_{a,b} \mathcal J_{2;a,b}) \big] \,\mathrm{d}{s} \,\mathrm{d}{t}, \end{align} (4.13)

    where a,b are indices running from 1 to 3, and

    \begin{align*} \mathcal J_0 & : = |\int e^{i(s-t) \cdot \xi}\, c_1(s,t,z,y,\xi) \,\mathrm{d}{\xi}|, \\ \mathcal J_{1;a} & : = |\int e^{i(s-t) \cdot \xi}\, \xi_a c_1(s,t,z,y,\xi) \,\mathrm{d}{\xi}|, \\ \mathcal J_{2;a,b} & : = |\int e^{i(s-t) \cdot \xi}\, \xi_a \xi_b c_1(s,t,z,y,\xi) \,\mathrm{d}{\xi}|. \end{align*}

    Because of the condition m > 2 (cf. Theorem 1.5), we can find a number \tau \in (0,1) satisfying the inequalities 3 - m < \tau < 1 . Therefore, we have

    \left\{\begin{array}{l} -m-\tau < -3, \;\;\;\;\;\;\;\;\;\;\;\;\;\;\;(\rm 4.14a)\\ -2-\tau > -3.\;\;\;\;\;\;\;\;\;\;\;\;\;\;\;\;\;(\rm 4.14b) \end{array}\right.

    By using Lemmas 4.1 and 4.2, these quantities \mathcal J_0 , \mathcal J_{1;a} and \mathcal J_{2;a,b} can be estimated as follows:

    \begin{align} \mathcal J_0 & = |s-t|^{-\tau} \cdot |\int (-\Delta_\xi)^{\tau/2} (e^{i(s-t) \cdot \xi}) c_1 (s,t,z,y,\xi) \,\mathrm{d}{\xi}| \\ & = |s-t|^{-\tau} \cdot |\int e^{i(s-t) \cdot \xi}\, (-\Delta_\xi)^{\tau/2} (c_1 (s,t,z,y,\xi)) \,\mathrm{d}{\xi}| \\ & \lesssim |s-t|^{-\tau} \cdot \int 〈\xi〉^{-m-\tau} \,\mathrm{d}{\xi} \lesssim |s-t|^{-\tau}. \end{align} (4.15)

    The last inequality in (4.15) makes use of the fact (4.14a). Similarly, by first using fractional Laplacian and then using first-order differential operator on e^{i(s-t) \cdot \xi} , we can have

    \begin{align} \mathcal J_{1;a} & \leq C |s-t|^{-1-\tau} \int 〈\xi〉^{-m+1-1-\tau} \,\mathrm{d}{\xi} \leq C |s-t|^{-1-\tau}, \end{align} (4.16)
    \begin{align} \mathcal J_{2;a,b} & \leq C |s - t|^{-2-\tau} |\int 〈\xi〉^{-m+2-2-\tau} \,\mathrm{d}{\xi}| \leq C |s - t|^{-2-\tau}, \end{align} (4.17)

    where the constant C is independent of the indices a , b . Combining (4.13), (4.15), (4.16) and (4.17), we can rewrite (4.13) as

    \begin{align} k_1 k_2 |\mathbb K(z,y)| & \lesssim \iint_{\widetilde{\mathcal D} \times \widetilde{\mathcal D}} \big[ |s-y|^{-2} |t-z|^{-2} |s - t|^{-\tau} + |s-y|^{-2} |t-z|^{-1} |s - t|^{-1-\tau} \\ & + |s-y|^{-1} |t-z|^{-2} |s - t|^{-1-\tau} + |s-y|^{-1} |t-z|^{-1} |s - t|^{-2-\tau} \big] \,\mathrm{d}{s} \,\mathrm{d}{t} \\ & = : \mathbb I_1 + \mathbb I_2 + \mathbb I_3 + \mathbb I_4. \end{align} (4.18)

    Denote \mathbf D : = \{x + x', x - x' \,;\, x, x' \in \widetilde{\mathcal D} \} . Then we apply Lemma 4.3 to estimate \mathbb I_1 as follows,

    \begin{align} \mathbb I_1 & = \iint_{\widetilde{\mathcal D} \times \widetilde{\mathcal D}} |s-y|^{-2} |t-z|^{-2} |s - t|^{-\tau} \,\mathrm{d}{s} \,\mathrm{d}{t} \\ & \leq \int_{\mathbf D} |s|^{-2} \big( \int_{\mathbf D} |t|^{-2} |t - (s+y-z)|^{-\tau} \,\mathrm{d}{t} \big) \,\mathrm{d}{s} \\ & \lesssim C_{\widetilde{\mathcal D}} + \int_{\mathbf D} |s|^{-2} |s - (z-y)|^{-(\tau-1)} \,\mathrm{d}{s} \\ & \simeq |z-y|^{2-\tau} + C_{\widetilde{\mathcal D}}. \end{align} (4.19)

    Note that in (4.19) we used Lemma 4.3 twice. Similarly,

    \begin{equation} \mathbb I_2,\, \mathbb I_3,\, \mathbb I_4 \lesssim |z-y|^{2-\tau} + C_{\widetilde{\mathcal D}}. \end{equation} (4.20)

    Recall that \tau \in (0,1) . By (4.18), (4.19) and (4.20) we arrive at

    \begin{equation*} |\mathbb K(z,y)| \leq C k_1^{-1} k_2^{-1} (|z-y|^{2-\tau} + C_{\widetilde{\mathcal D}}) \leq C k^{-2} (( \mathop{{\rm{diam}}} D_V)^{2-\tau} + C_{\widetilde{\mathcal D}}) \lesssim k^{-2}. \end{equation*}

    We have reviewed the recoveries of some statistics by using the near-field data as well as far-field data generated under a single realization of the randomness. In this paper we mainly focus on time-harmonic Schrödinger systems. One of the possible ways to extend the current works is to study the Helmholtz systems. It would be also interesting to conduct the work in the time domain. Moreover, the stability of the recovering procedure is also worth of investigation.



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