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On diffusive scaling in acousto-optic imaging

Francis J. Chung Department of Mathematics, University of Kentucky, Lexington, KY 40506, USA fj.chung@uky.edu Ru-Yu Lai School of Mathematics, University of Minnesota, Minneapolis, MN 55455, USA rylai@umn.edu  and  Qin Li Department of Mathematics and Wisconsin Institute for Discoveries, University of Wisconsin-Madison, Madison, WI 53705, USA qinli@math.wisc.edu
Abstract.

Acousto-optic imaging (AOI) is a hybrid imaging process. By perturbing the to-be-reconstructed tissues with acoustic waves, one introduces the interaction between the acoustic and optical waves, leading to a more stable reconstruction of the optical properties. The mathematical model was described in [27], with the radiative transfer equation serving as the forward model for the optical transport. In this paper we investigate the stability of the reconstruction. In particular, we are interested in how the stability depends on the Knudsen number, 𝖪𝗇\mathsf{Kn}, a quantity that measures the intensity of the scattering effect of photon particles in a media. Our analysis shows that as 𝖪𝗇\mathsf{Kn} decreases to zero, photons scatter more frequently, and since information is lost, the reconstruction becomes harder. To counter this effect, devices need to be constructed so that laser beam is highly concentrated. We will give a quantitative error bound, and explicitly show that such concentration has an exponential dependence on 𝖪𝗇\mathsf{Kn}. Numerical evidence will be provided to verify the proof.

Chung is supported in part by Simons Collaboration Grant 582020. Lai is supported in part by the NSF grant DMS-1714490. Li is supported in part by DMS-1619778 and DMS-1750488. The collaboration started during the workshop “Mathematics in Optical Imaging” in IMA, 2019, and was continuously supported by KI-net, DMS-1107291 in the workshop “Forward and Inverse Problems in Kinetic Theory” in UW-Madison, 2019. The authors thank Professor John Schotland for helpful discussions.
Key words and phrases: Acousto-optic imaging, inverse problem, radiative transfer equation.

1. Introduction

High energy light is the classical way to probe optical properties of thick and highly scattering media. In contrast to most destructive experiments, here, high energy photons are injected into biological tissues, and the outgoing light intensities are measured at the surface of the samples by detectors. The map that maps the incoming light intensity to the outgoing light intensity carries optical information of the biological tissues, and is utilized to reconstruct optical parameters.

However, a long standing challenge of the reconstruction process centers around the stability issue. If the injected photons carry low energy, the resulting images are very blurred, and the reconstruction is typically unstable [10, 11, 19, 20, 31, 34]. This phenomenon is the so-called diffuse optical tomography, especially when the injected light is near-infrared. In this situation, the forward model is the classical elliptic type equation, and mathematically, recovering the optical parameter amounts to reconstructing the diffusion coefficient in the elliptic equation using the Dirichlet-to-Neumann map [42], and is proven mathematically to be logarithmically unstable [1]. Multiple strategies are adopted to “stabilize” the problem [36, 40], both by adjusting the experimental modalities upfront, or introducing image deblurring techniques as a post-processing [18, 29, 39, 41].

We follow the first approach in this paper. In particular, we investigate a modality called acousto-optic imaging (AOI), and study the stability of the media reconstruction when biological tissue is optically thick. AOI is one of the state-of-the-art hybrid imaging processes that fuse two or more imaging modalities to form a new imaging technique [8, 30]. In particular, AOI is based on the acousto-optic effect: optical properties of the medium are modified upon interaction with acoustic radiation. Presumably one can obtain more information upon a sequence of such modifications. The procedure combines the contrast advantage inheriting from optical properties and the resolution advantage of ultrasound  [15, 32, 44], and is expected to provide a more stable reconstruction.

In general, there are two types of AOI - direct imaging and tomographic imaging. In direct imaging, the sample is simultaneously affected by an ultrasound beam and illuminated with a laser source. The tagged photon, resulting from the interaction between the light and the ultrasound, is detected by external ultrasound transducers and then forms the image [28]. Tomographic imaging, the second type of AOI, makes use of a reconstruction algorithm to track down the optical properties of the medium through various inversion procedures. In the latter case, the inverse problems for incoherent AOI [2, 3, 4, 14, 15, 16] and for coherent AOI with diffuse light [25] were studied and the absorption and the diffusion coefficients of a scattering medium are stably reconstructed. On the other hand, for the problem within the framework of radiative transport theory, relevant results are also investigated in [9, 26, 27]; also see reviews [6, 7, 8, 35].

As a typical hybrid imaging problem, the inverse problem in acousto-optic imaging involves two steps: the first step amounts to reconstructing internal information from triggering the system using ultrasound. Ultrasound waves of different frequencies imposed on a physical system induces a wave-like perturbation to the media, leading to wave-like perturbation in the measurement. From measurements of this perturbation over a big spectrum of frequencies, a Fourier-type calculation provides internal information inside the physical domain. The second step then amounts to reconstructing optical parameters in the modeling equation using the internal data. The first step basically is an inverse Fourier series, and thus is regarded as a stable process, and since the internal data is obtained, it is largely believed that the reconstruction is also stable in the second step.

This is indeed the situation that we will be studying. As a forward model we use the radiative transfer equation (RTE) to characterize the dynamics of photon particles. This equation, besides containing optical parameters, also depends on the Knudsen number 𝖪𝗇\mathsf{Kn}: it is the ratio of mean free path and the typical domain length. In the thick and dense optical environment, the photon particles scatter frequently, and mathematically this amounts to setting this ratio to be small. One can also view this quantity to reflect the energy of the photon particles being used: indeed, for the same media, in the low energy regime, photon particles are scattered more often. One interesting phenomenon associated with low energy, high scattering situation is that, in this regime, mathematically one can asymptotically connects the RTE to a parabolic heat equation. It is a well-accepted fact that reconstruction of parameters are unstable for diffusion type equations, and thus it is a natural expectation that the inverse problem of the RTE is ill-posed accordingly in this regime.

The rest of this paper is organized as follows. In Section 2, we discuss the first step in AOI of determining the internal data, introduce preliminary results for the well-posedness of the transport equation, and present the main result in Theorem 2.4. Section 3 is concerned with the second step in AOI. We derive the reconstruction formula for the absorption coefficient from the reconstructed internal data and focus on the dependence of 𝖪𝗇\mathsf{Kn} in the associated convergence rate. The numerical evidence is presented in Section 4.

2. Problem setup and main results

In this section, we start by introducing some preliminary results and then describe the setup of the problem. Lastly, we present the main theorem.

To begin, consider a smooth bounded domain Ωn\Omega\subset\mathbb{R}^{n}. In this paper we use the RTE as the forward model for light propagation on Ω\Omega. We also assume the time scale is significantly larger, and the equation achieves the steady state:

(2.3) {θu=σs(x)𝖪𝗇(uu)𝖪𝗇σa(x)uin Ω×𝕊n1,u|Γ=f.\displaystyle\left\{\begin{array}[]{ll}\theta\cdot\nabla u=\frac{\sigma_{s}(x)}{\mathsf{Kn}}\left(\langle u\rangle-u\right)-\mathsf{Kn}\sigma_{a}(x)u&\hbox{in }\Omega\times\mathbb{S}^{n-1}\,,\\ u|_{\Gamma_{-}}=f\,.\\ \end{array}\right.

The solution u(x,θ)u(x,\theta) characterizes the density of photon particles at a physical point xΩx\in\Omega moving in direction θ𝕊n1\theta\in\mathbb{S}^{n-1} for n2n\geq 2. The left-hand side of (2.3) is a transport term describing particles at the position xx moving in the θ\theta direction. The terms on the right represent the interaction of the photon particles with the medium, where σa\sigma_{a} is the absorption coefficient, σs\sigma_{s} is the scattering coefficient. The scattering operator is uu\langle u\rangle-u with

u:=1|𝕊n1|𝕊n1u(x,θ)dθ=:u(x,θ)dθ\langle u\rangle:=\frac{1}{|\mathbb{S}^{n-1}|}\int_{\mathbb{S}^{n-1}}u(x,\theta)~{}d\theta=:\fint u(x,\theta)~{}d\theta

standing for the angular average of uu. Physically it means the particles with different velocities at xx are redistributed in an isotropic way at rate σs(x)\sigma_{s}(x). It is also common to insert an anisotropic term k(x,θ,θ)k(x,\theta,\theta^{\prime}) in the integral defined above, but it does not bring extra mathematical difficulty and thus will be neglected here. The parameter 𝖪𝗇\mathsf{Kn} in the equation is called the Knudsen number, and as described above, represents the ratio of mean free path to the typical domain length.

For conciseness of notation, we denote the total absorption coefficient

σ=σs+𝖪𝗇2σa,\sigma=\sigma_{s}+\mathsf{Kn}^{2}\sigma_{a}\,,

and rewrite the right-hand side of (2.3) as a linear operator

(2.4) u:=σs𝖪𝗇uσ𝖪𝗇u.\mathcal{L}u:=\frac{\sigma_{s}}{\mathsf{Kn}}\langle u\rangle-{\frac{\sigma}{\mathsf{Kn}}}u\,.

The boundary condition of (2.3) is imposed on Γ\Gamma_{-}: a a set of coordinates at the physical boundary Ω\partial\Omega with inward velocities. More specifically:

(2.5) Γ±:={(x,θ)Ω×3:±n(x)θ>0},\displaystyle\Gamma_{\pm}:=\{(x,\theta)\in\partial\Omega\times\mathbb{R}^{3}:\pm\ n(x)\cdot\theta>0\}\,,

where n(x)n(x) is the unit outer normal to Ω\partial\Omega at the point xΩx\in\partial\Omega. Similarly, Γ+\Gamma_{+} collects all outgoing coordinates at the boundary.

The well-posedness problem of (2.3) has been extensively studied. We refer the readers to, for instance, [22, 23, 24] for detailed discussion on the existence of solutions to (2.3) under different constraints. For our purpose, we will be using the following boundedness result, with 𝖪𝗇\mathsf{Kn} included and adjusted to fit our setting.

Theorem 2.1 (Theorem 2.1 in [9]).

Suppose σs\sigma_{s} and σa\sigma_{a} are bounded and uniformly positive functions in Ω\Omega and the source term SL(Ω×𝕊n1)S\in L^{\infty}(\Omega\times\mathbb{S}^{n-1}). For any 𝖪𝗇>0\mathsf{Kn}>0 and any boundary value fL(Γ)f\in L^{\infty}(\Gamma_{-}), there exists a strong unique solution uL(Ω×𝕊n1)u\in L^{\infty}(\Omega\times\mathbb{S}^{n-1}) to the boundary value problem

(2.8) {θu=σs𝖪𝗇(uu)𝖪𝗇σau+Sin Ω×𝕊n1,u=fon Γ.\displaystyle\left\{\begin{array}[]{ll}\theta\cdot\nabla u={\frac{\sigma_{s}}{\mathsf{Kn}}}(\langle u\rangle-u)-\mathsf{Kn}\sigma_{a}u+S&\hbox{in }\Omega\times\mathbb{S}^{n-1}\,,\\ u=f&\hbox{on }\Gamma_{-}\,.\\ \end{array}\right.

Furthermore we have the estimate:

(2.9) uL(Ω×𝕊n1)C𝖪𝗇(SL(Ω×𝕊n1)+1𝖪𝗇fL(Γ)),\|u\|_{L^{\infty}(\Omega\times\mathbb{S}^{n-1})}\leq\frac{C}{\mathsf{Kn}}\left(\|S\|_{L^{\infty}(\Omega\times\mathbb{S}^{n-1})}+\frac{1}{\mathsf{Kn}}\|f\|_{L^{\infty}(\Gamma_{-})}\right),

holds for some positive constant CC depending only on σa\sigma_{a} and σs\sigma_{s}.

In the low energy regime, 𝖪𝗇\mathsf{Kn} is small, and one can perform the asymptotic expansion in 𝖪𝗇\mathsf{Kn}. In the leading order the scattering term σs𝖪𝗇(uu)\frac{\sigma_{s}}{\mathsf{Kn}}(\langle u\rangle-u) becomes dominant, and it drives uuu\sim\langle u\rangle, meaning uu is a constant in θ\theta at every location xx, see [19]. This degeneracy of information, as will be explained in details in Section 3, is one of the main reason for the rise of instability.

With the well-posedness result in Theorem 2.1, the trace can be taken and we define the albedo operator 𝒜\mathcal{A}:

(2.10) 𝒜:L(Γ)L(Γ+):u|Γ+=𝒜f.\displaystyle\mathcal{A}:L^{\infty}(\Gamma_{-})\rightarrow L^{\infty}(\Gamma_{+}):\quad u|_{\Gamma_{+}}=\mathcal{A}f\,.

It maps the incoming light intensity to the outgoing light intensity.

2.1. Problem setup

Acousto-optic imaging is an imaging modality that introduces an acoustic wave to the medium, and thus induces a wave-like perturbation to the coefficients σa\sigma_{a} and σs\sigma_{s}, that gives rise to new coefficients σa,ε\sigma_{a,\varepsilon} and σs,ε\sigma_{s,\varepsilon}. Following the setup presented in [27], the modulated coefficients take the form

(2.11) σa,ε:=(1+εcos(qx))σa,σs,ε:=(1+εcos(qx))σs,\displaystyle\sigma_{a,\varepsilon}:=(1+\varepsilon\cos(q\cdot x))\sigma_{a}\,,\quad\sigma_{s,\varepsilon}:=(1+\varepsilon\cos(q\cdot x))\sigma_{s}\,,

where 0<ε10<\varepsilon\ll 1 is the strength of introduced acoustic effect. The cos(qx)\cos{(q\cdot x)} perturbation comes from the assumption that the introduced acoustic wave is basically sinusoidal, and the wave vector qq can be experimentally adjusted.

We denote uεu_{\varepsilon} to be the solution to the RTE with the modulated coefficients, namely:

(2.12) {θuε=σs,ε𝖪𝗇(uεuε)𝖪𝗇σa,εuε,uε|Γ=f.\displaystyle\begin{cases}\theta\cdot\nabla u_{\varepsilon}=\frac{\sigma_{s,\varepsilon}}{\mathsf{Kn}}(\langle u_{\varepsilon}\rangle-u_{\varepsilon})-\mathsf{Kn}\sigma_{a,\varepsilon}u_{\varepsilon}\,,\\ u_{\varepsilon}|_{\Gamma_{-}}=f\,.\\ \end{cases}

For small ε\varepsilon, the well-posedness result for (2.12) still holds true according to Theorem 2.1. Hence, for each qq, we can define the corresponding albedo operator:

𝒜ε,q:fuε|Γ+,\mathcal{A}_{\varepsilon,q}:f\mapsto u_{\varepsilon}|_{\Gamma_{+}}\,,

where uεu_{\varepsilon} is the solution to (2.12). Likewise, we also define the perturbed scattering operator ε\mathcal{L}_{\varepsilon}:

εu:=σs,ε𝖪𝗇uσε𝖪𝗇u,\mathcal{L}_{\varepsilon}u:=\frac{\sigma_{s,\varepsilon}}{\mathsf{Kn}}\langle u\rangle-\frac{\sigma_{\varepsilon}}{\mathsf{Kn}}u\,,

where the modulated total absorption coefficient is

σε:=σs,ε+𝖪𝗇2σa,ε.\sigma_{\varepsilon}:=\sigma_{s,\varepsilon}+\mathsf{Kn}^{2}\sigma_{a,\varepsilon}\,.

To extract internal information, we first introduce the adjoint RTE:

(2.13) {θv=v,v|Γ+=g.\displaystyle\begin{cases}-\theta\cdot\nabla v=\mathcal{L}v\,,\\ v|_{\Gamma_{+}}=g\,.\\ \end{cases}

It is straightforward to show that if vv solves the adjoint RTE, then

v~(x,θ)=v(x,θ)\tilde{v}(x,\theta)=v(x,-\theta)

solves the regular RTE. Therefore the well-posedness result applies and we can also define the adjoint albedo operator

𝒜~:L(Γ+)L(Γ):v|Γ=𝒜~g.\tilde{\mathcal{A}}:L^{\infty}(\Gamma_{+})\rightarrow L^{\infty}(\Gamma_{-}):v|_{\Gamma_{-}}=\tilde{\mathcal{A}}g\,.

Furthermore:

𝒜(g~)~=𝒜~(g),\widetilde{\mathcal{A}(\tilde{g})}=\tilde{\mathcal{A}}(g)\,,

so 𝒜~\tilde{\mathcal{A}} is determined by 𝒜\mathcal{A}. Here for a given function φ\varphi, the expression φ~\tilde{\varphi} indicates the reflection of φ\varphi in the θ\theta variable, namely, φ~(x,θ):=φ(x,θ)\tilde{\varphi}(x,\theta):=\varphi(x,-\theta).

Now we can use the adjoint RTE to obtain an internal functional. Using  (2.12) and  (2.13) we find

Ω×𝕊n1θn(x)(uεv)𝑑x𝑑θ\displaystyle\int_{\partial\Omega\times\mathbb{S}^{n-1}}\theta\cdot n(x)(u_{\varepsilon}v)~{}dxd\theta =Ω𝕊n1(vεuεuεv)𝑑x𝑑θ\displaystyle=\int_{\Omega}\int_{\mathbb{S}^{n-1}}(v\mathcal{L}_{\varepsilon}u_{\varepsilon}-u_{\varepsilon}\mathcal{L}v)~{}dxd\theta\,
=Ω𝕊n1v(ε)uε𝑑x𝑑θ,\displaystyle=\int_{\Omega}\int_{\mathbb{S}^{n-1}}v(\mathcal{L}_{\varepsilon}-\mathcal{L})u_{\varepsilon}~{}dxd\theta\,,
(2.14) =Ω𝕊n1εcos(qx)(uε)v𝑑x𝑑θ,\displaystyle=\int_{\Omega}\int_{\mathbb{S}^{n-1}}\varepsilon\cos(q\cdot x)(\mathcal{L}u_{\varepsilon})v~{}dxd\theta\,,

where we used the self-adjoint property of \mathcal{L} and ε\mathcal{L}_{\varepsilon} as well as ε=εcos(qx)\mathcal{L}_{\varepsilon}-\mathcal{L}=\varepsilon\cos(q\cdot x)\mathcal{L}. We can label the left-hand side of this BTBT (for boundary term) and rewrite it in terms of boundary values of vv and uεu_{\varepsilon}:

BT:=Γθnf𝒜~(g)𝑑S+Γ+θn𝒜ε,q(f)g𝑑S.BT:=\int_{\Gamma_{-}}\theta\cdot nf\tilde{\mathcal{A}}(g)~{}dS+\int_{\Gamma_{+}}\theta\cdot n\mathcal{A}_{\varepsilon,q}(f)g~{}dS\,.

Since the boundary values are known, this implies that BTBT is known.

Finally, in (2.1), we can write uε=u+(uεu)\mathcal{L}u_{\varepsilon}=\mathcal{L}u+\mathcal{L}(u_{\varepsilon}-u), so if uεuu_{\varepsilon}-u is small when ε0\varepsilon\to 0, (2.1) becomes

(2.15) ε|𝕊n1|Ωcos(qx)H(x)𝑑x+𝒪(ε2)=BT,\displaystyle\varepsilon|\mathbb{S}^{n-1}|\int_{\Omega}\cos(q\cdot x)H(x)~{}dx+\mathcal{O}(\varepsilon^{2})=BT\,,

where one defines the internal data HH as

(2.16) H(x):=𝕊n1vu𝑑θ.H(x):=\fint_{\mathbb{S}^{n-1}}v\mathcal{L}u~{}d\theta\,.

This means that in the leading order, with the measurement at the boundary, we can recover the quantity

εΩcos(qx)H(x)𝑑x.\varepsilon\int_{\Omega}\cos(q\cdot x)H(x)~{}dx\,.

As the reconstruction can be done for all qnq\in\mathbb{R}^{n}, we obtain the entire spectrum of the Fourier transform of HH, which is further used to recover HH. 111We assume that σa,σs\sigma_{a},\sigma_{s} are compactly supported in Ω\Omega.

To justify (2.15), we use the smallness of uuεu-u_{\varepsilon} described in the following Lemma:

Lemma 2.2.

For small ε\varepsilon, we have

uεuL(Ω×𝕊n1)𝒪(ε)uεL(Ω×𝕊n1).\|u_{\varepsilon}-u\|_{L^{\infty}(\Omega\times\mathbb{S}^{n-1})}\leq{\mathcal{O}(\varepsilon)}\|u_{\varepsilon}\|_{L^{\infty}(\Omega\times\mathbb{S}^{n-1})}\,.
Proof.

Since uu solves the RTE θu=u\theta\cdot\nabla u=\mathcal{L}u and uεu_{\varepsilon} solves the modulated RTE θuε=εuε\theta\cdot\nabla u_{\varepsilon}=\mathcal{L}_{\varepsilon}u_{\varepsilon} with the same incoming boundary conditions, we can write

θ(uεu)\displaystyle\theta\cdot\nabla(u_{\varepsilon}-u) =εuεu\displaystyle=\mathcal{L}_{\varepsilon}u_{\varepsilon}-\mathcal{L}u
=(uεu)+(ε)uε\displaystyle=\mathcal{L}(u_{\varepsilon}-u)+(\mathcal{L}_{\varepsilon}-\mathcal{L})u_{\varepsilon}
=(uεu)+εcos(qx)uε\displaystyle=\mathcal{L}(u_{\varepsilon}-u)+\varepsilon\cos(q\cdot x)\mathcal{L}u_{\varepsilon}

and uεu=0u_{\varepsilon}-u=0 on Γ\Gamma_{-}. It follows from Theorem 2.1 that

uεuL(Ω×𝕊n1)𝒪(ε)uεL(Ω×𝕊n1),\|u_{\varepsilon}-u\|_{L^{\infty}(\Omega\times\mathbb{S}^{n-1})}\leq{\mathcal{O}(\varepsilon)}\|\mathcal{L}u_{\varepsilon}\|_{L^{\infty}(\Omega\times\mathbb{S}^{n-1})}\,,

and thus from the definition of \mathcal{L} we derive

uεuL(Ω×𝕊n1)𝒪(ε)uεL(Ω×𝕊n1).\|u_{\varepsilon}-u\|_{L^{\infty}(\Omega\times\mathbb{S}^{n-1})}\leq{\mathcal{O}(\varepsilon)}\|u_{\varepsilon}\|_{L^{\infty}(\Omega\times\mathbb{S}^{n-1})}\,.

Remark 2.1.

We comment that the proof above may lead to a large constant in the 𝒪\mathcal{O} notation for small 𝖪𝗇\mathsf{Kn}, but this constant will not affect the later proof. Furthermore, the bounds shown above is not sharp in the diffusion limit. In the diffusion limit of 𝖪𝗇0\mathsf{Kn}\to 0, uu and uεu_{\varepsilon} approximately satisfy two elliptic equations. By comparing these two elliptic equations, we can obtain the smallness of uuεu-u_{\varepsilon} in ε\varepsilon, and such smallness will be independent of 𝖪𝗇\mathsf{Kn}.

This immediately leads to the following proposition:

Proposition 2.3.

Suppose that f,gL(Γ)f,\ g\in L^{\infty}(\Gamma_{-}). Let uu be the solution to the RTE with boundary data u|Γ=fu|_{\Gamma_{-}}=f, and vv be the solution to the adjoint RTE with boundary data v|Γ+=gv|_{\Gamma_{+}}=g. Then 𝒜~(g)\tilde{\mathcal{A}}(g) and 𝒜ε,q(f)\mathcal{A}_{\varepsilon,q}(f) uniquely determine the internal functional HL(Ω)H\in L^{\infty}(\Omega) up to 𝒪(ε)\mathcal{O}(\varepsilon) accuracy:

(2.17) H(x)=σs(x)𝖪𝗇uvσ(x)𝖪𝗇uv.\displaystyle H(x)=\frac{\sigma_{s}(x)}{\mathsf{Kn}}\langle u\rangle\langle v\rangle-\frac{\sigma(x)}{\mathsf{Kn}}\langle uv\rangle\,.

This directly comes from inserting the definition of \mathcal{L} (2.4) in that of HH in (2.16).

2.2. Main results

The main objective of this paper is to analyze the stability of the reconstruction process of AOI. In particular we are interested in the requirement imposed on the probing light when the diffusion effect is strong. More specifically, we consider the incoming light ff that is concentrated in angle:

f(x,θ):={cnh12(1n)if |θθ0|<h,0otherwise,f(x,\theta):=\left\{\begin{array}[]{ll}c_{n}h^{\frac{1}{2}(1-n)}&\hbox{if }|\theta-\theta_{0}|<h\,,\\ 0&\hbox{otherwise}\,,\\ \end{array}\right.

in Ω×𝕊n1\Omega\times\mathbb{S}^{n-1}, where hh stands for the concentration of the light beam, and cnc_{n} is chosen to be the constant depending only on nn such that

(2.18) 𝕊n1f2𝑑θ=1.\displaystyle\fint_{\mathbb{S}^{n-1}}f^{2}d\theta=1\,.

With concentrated light beam injected into the tissue, singularities are more likely to be preserved, keeping more information for the reconstruction. As 𝖪𝗇\mathsf{Kn} decreases, media becomes optically thicker, and the light beam needs to be more concentrated for a stable reconstruction. We will carefully trace such dependence of hh on 𝖪𝗇\mathsf{Kn}.

The main theorem we will prove is the following, and we leave the proof to Section 3.

Theorem 2.4.

Let HH be the internal functional defined in Proposition 2.3. Suppose that ff satisfies (3.4). If σCα(Ω)\sigma\in C^{\alpha}(\Omega), for some 0<α10<\alpha\leq 1, then for all xΩx\in\Omega one has

(2.19) σ(x)𝖪𝗇=f(xτ(x,θ0)θ0,θ0)𝒜(f)(x+τ+(x,θ0)θ0,θ0)H(x)+𝒪(hα)e3dsupσ𝖪𝗇,\frac{\sigma(x)}{\mathsf{Kn}}=-\frac{f(x-\tau_{-}(x,\theta_{0})\theta_{0},\theta_{0})}{\mathcal{A}(f)(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})}H(x)+\mathcal{O}(h^{\alpha})e^{\frac{3d\sup\sigma}{\mathsf{Kn}}}\,,

where τ±\tau_{\pm} represent the distance from xx to Ω\partial\Omega in the direction ±θ\pm\theta, and dd is the diameter of the domain Ω\Omega. The constant implied in the big 𝒪\mathcal{O} is independent of 𝖪𝗇\mathsf{Kn}. Moreover, if one chooses

(2.20) he3dsupσα𝖪𝗇,h\ll e^{\frac{-3d\sup\sigma}{\alpha\mathsf{Kn}}}\,,

then

(2.21) σ(x)𝖪𝗇=f(xτ(x,θ0)θ0,θ0)𝒜(f)(x+τ+(x,θ0)θ0,θ0)H(x)+𝒪(hα),\frac{\sigma(x)}{\mathsf{Kn}}=-\frac{f(x-\tau_{-}(x,\theta_{0})\theta_{0},\theta_{0})}{\mathcal{A}(f)(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})}H(x)+\mathcal{O}(h^{\alpha^{\prime}})\,,

for some 0<α<α0<\alpha^{\prime}<\alpha.

We make the following five remarks regarding the interpretation of Theorem 2.4.

First, on explicit reconstruction: we note, as in [27], that everything on the right side of (2.21), other than the error term, is explicit: can be directly calculated from boundary measurements. Thus (2.21) can be viewed as a reconstruction formula for σ\sigma in terms of boundary quantities.

Second, in the case 𝖪𝗇0\mathsf{Kn}\rightarrow 0, we have 𝖪𝗇2σa0\mathsf{Kn}^{2}\sigma_{a}\rightarrow 0 in the total absorption coefficient σ\sigma. Therefore it makes sense in this case to consider the reconstruction of one coefficient by (2.21), and not attempt to recover σa\sigma_{a} and σs\sigma_{s} separately as in [27].

Third, one preliminary assumption of σ\sigma: the theorem does require Hölder continuity. This is different from what is required in [27] where Hölder continuity is removed. The main difference is we are establishing a rate of convergence for the formula in terms of the angular concentration of the source, and thus some control on the modulus of continuity is needed (see the proof of Proposition 3.1 for details.) Heuristically, it should be reasonable to concede that a sufficiently rough coefficient cannot be well-resolved with any source that is not completely singular.

Fourth, on incoming data concentration: in the case 𝖪𝗇1\mathsf{Kn}\ll 1, (2.20) gives us a condition to guarantee that (2.19) can be used to reconstruct σ\sigma. In other words, in the case 𝖪𝗇1\mathsf{Kn}\ll 1, Theorem 2.4 gives a quantitative condition on the degree of angular concentration of the source required for tomography to work at all, with possible implications for the RTE-based optical tomography more generally.

Finally, on stability: this theorem also implies a quantitative stability estimate in terms of 𝖪𝗇\mathsf{Kn} for the acousto-optic reconstruction. In Section 3, we will show that f(xτ)𝒜f(x+τ+)ec𝖪𝗇\frac{f(x-\tau_{-})}{\mathcal{A}f(x+\tau_{+})}\sim e^{\frac{c}{\mathsf{Kn}}}; this means the perturbation in HH will be reflected exponentially in the reconstruction of σ\sigma. Applying (3.10), this means that in the regime where (2.21) applies, we have

1𝖪𝗇|σ1(x)σ2(x)|edsupσj𝖪𝗇|H1(x)H2(x)|+𝒪(hα).\frac{1}{\mathsf{Kn}}|\sigma_{1}(x)-\sigma_{2}(x)|\leq e^{\frac{d\sup\sigma_{j}}{\mathsf{Kn}}}|H_{1}(x)-H_{2}(x)|+\mathcal{O}(h^{\alpha})\,.

This shows that the stability of the reconstruction decays exponentially as 𝖪𝗇0\mathsf{Kn}\rightarrow 0, which should be expected from the reliance on singularities in the RTE (see also [31, 45, 33]).

3. Reconstruction of optical properties

We show Theorem 2.4 in this section. The proof relies on a proper decomposition of the transport solution according to the singularity. This technique, termed the singular decomposition, is the classical technique in the study of optics in inverse problems.

This was introduced in [5, 17, 21, 22, 23] and later was applied extensively to treat various settings related to parameter identification of the RTE [12, 13, 24, 35, 37, 38, 43]. For the purpose of this paper, we will decompose the solution to the RTE into two parts - the most singular (ballistic part) and the remainders, and then separate the singular contribution from the rest of H(x)H(x).

To start, we first write the solution uL(Ω×𝕊n1)u\in L^{\infty}(\Omega\times\mathbb{S}^{n-1}) of the equation (2.3) in the form of

u=u1+u2,u=u_{1}+u_{2}\,,

where u1u_{1} is the ballistic part that satisfies the X-ray equation and u2u_{2} takes care of the remaining terms, namely:

(3.1) {θu1=σ𝖪𝗇u1,u1|Γ=f,and {θu2=σs𝖪𝗇u2σ𝖪𝗇u2+σs𝖪𝗇u1,u2|Γ=0.\displaystyle\begin{cases}\theta\cdot\nabla u_{1}=-\frac{\sigma}{\mathsf{Kn}}u_{1}\,,\\ u_{1}|_{\Gamma_{-}}=f\,,\\ \end{cases}\quad\text{and}\hskip 28.45274pt\begin{cases}\theta\cdot\nabla u_{2}=\frac{\sigma_{s}}{\mathsf{Kn}}\langle u_{2}\rangle-\frac{\sigma}{\mathsf{Kn}}u_{2}+\frac{\sigma_{s}}{\mathsf{Kn}}\langle u_{1}\rangle\,,\\ u_{2}|_{\Gamma_{-}}=0\,.\\ \end{cases}

The existence of solutions to both equations follows from Theorem 2.1. Note that the entire boundary condition ff is applied on u1u_{1} leaving u2u_{2} with the trivial boundary condition.

A similar separation can also be performed to the adjoint RTE (2.13). We write v=v1+v2v=v_{1}+v_{2} with the components satisfying:

(3.2) {θv1=σ𝖪𝗇v1,v1|Γ+=g,and {θv2=σs𝖪𝗇v2σ𝖪𝗇v2+σs𝖪𝗇v1,v2|Γ+=0.\displaystyle\begin{cases}-\theta\cdot\nabla v_{1}=-\frac{\sigma}{\mathsf{Kn}}v_{1}\,,\\ v_{1}|_{\Gamma_{+}}=g\,,\\ \end{cases}\quad\text{and}\hskip 28.45274pt\begin{cases}-\theta\cdot\nabla v_{2}=\frac{\sigma_{s}}{\mathsf{Kn}}\langle v_{2}\rangle-\frac{\sigma}{\mathsf{Kn}}v_{2}+\frac{\sigma_{s}}{\mathsf{Kn}}\langle v_{1}\rangle\,,\\ v_{2}|_{\Gamma_{+}}=0\,.\end{cases}

With these decompositions, we now rewrite the internal function H(x)H(x) as:

H(x)\displaystyle H(x) =σs(x)𝖪𝗇(u1v1+u1v2+u2v1+u2v2)\displaystyle=\frac{\sigma_{s}(x)}{\mathsf{Kn}}(\langle u_{1}\rangle\langle v_{1}\rangle+\langle u_{1}\rangle\langle v_{2}\rangle+\langle u_{2}\rangle\langle v_{1}\rangle+\langle u_{2}\rangle\langle v_{2}\rangle)
(3.3) σ(x)𝖪𝗇(u1v1+u1v2+u2v1+u2v2),\displaystyle\hskip 28.45274pt-\frac{\sigma(x)}{\mathsf{Kn}}(\langle u_{1}v_{1}\rangle+\langle u_{1}v_{2}\rangle+\langle u_{2}v_{1}\rangle+\langle u_{2}v_{2}\rangle)\,,

simply by substituting u=u1+u2u=u_{1}+u_{2} and v=v1+v2v=v_{1}+v_{2} into the definition of HH (2.17).

As described previously, boundary conditions are light beams concentrated in the angle variable θ0𝕊n1\theta_{0}\in\mathbb{S}^{n-1}:

(3.4) g(x,θ)=f(x,θ):={cnh12(1n)if |θθ0|<h,0otherwise,g(x,\theta)=f(x,\theta):=\left\{\begin{array}[]{ll}c_{n}h^{\frac{1}{2}(1-n)}&\hbox{if }|\theta-\theta_{0}|<h\,,\\ 0&\hbox{otherwise}\,,\\ \end{array}\right.

in Ω×𝕊n1\Omega\times\mathbb{S}^{n-1}, where cnc_{n} is the normalization constant.

In the rest of the section we will show that with such concentrated incoming data (3.4) and sufficiently small hh, the term u1v1\langle u_{1}v_{1}\rangle essentially dominates the other terms in H(x)H(x). This can be seen from the estimates of the dominating and remaining terms presented in Proposition 3.1 and Proposition 3.2, respectively. Finally, from the explicit dependence of u1v1\langle u_{1}v_{1}\rangle on σ\sigma, we can derive the reconstruction of σ\sigma from the internal data.

Proposition 3.1.

Suppose σCα(Ω)\sigma\in C^{\alpha}(\Omega), and let uiu_{i} and viv_{i}, i=1,2i=1,2, satisfy (3.1) and (3.2) respectively with boundary condition defined in (3.4). Then for each xx in Ω\Omega, one has

u1v1(x)=e(x,θ0)σ𝖪𝗇𝑑s(1+𝖪𝗇1𝒪(hα)),\langle u_{1}v_{1}\rangle(x)=e^{-\int_{\ell(x,\theta_{0})}\frac{\sigma}{\mathsf{Kn}}ds}(1+\mathsf{Kn}^{-1}\mathcal{O}(h^{\alpha}))\,,

where (x,θ)\ell(x,\theta) denotes the section of the straight line through xx in the direction of θ\theta, intersected with Ω\Omega.

Proof.

The ballistic terms of the solution uu to the RTE and the solution vv to the adjoint RTE are given explicitly by

(3.5) u1(x,θ)=e0τ(x,θ)1𝖪𝗇σ(xsθ)𝑑sf(xτ(x,θ)θ,θ),\displaystyle u_{1}(x,\theta)=e^{-\int_{0}^{\tau_{-}(x,\theta)}{\frac{1}{\mathsf{Kn}}}\sigma(x-s\theta)ds}f(x-\tau_{-}(x,\theta)\theta,\theta)\,,
(3.6) v1(x,θ)=e0τ+(x,θ)1𝖪𝗇σ(x+sθ)𝑑sg(x+τ+(x,θ)θ,θ),\displaystyle v_{1}(x,\theta)=e^{-\int_{0}^{\tau_{+}(x,\theta)}{\frac{1}{\mathsf{Kn}}}\sigma(x+s\theta)ds}g(x+\tau_{+}(x,\theta)\theta,\theta)\,,

where τ±(x,θ)\tau_{\pm}(x,\theta) is the distance from the point xx to the boundary in the direction ±θ\pm\theta.

Substituting these into u1v1(x)\langle u_{1}v_{1}\rangle(x) and using (3.4), we find that for any xΩx\in\Omega,

u1v1(x)=𝕊n1eτ(x,θ)τ+(x,θ)1𝖪𝗇σ(x+sθ)𝑑scn2h1nχθ0h(θ)𝑑θ,\langle u_{1}v_{1}\rangle(x)=\fint_{\mathbb{S}^{n-1}}e^{-\int_{-\tau_{-}(x,\theta)}^{\tau_{+}(x,\theta)}{\frac{1}{\mathsf{Kn}}}\sigma(x+s\theta)ds}c_{n}^{2}h^{1-n}\chi^{h}_{\theta_{0}}(\theta)d\theta\,,

where χθ0h(θ)\chi^{h}_{\theta_{0}}(\theta) is the characteristic function that is equal to 11 in |θθ0|<h|\theta-\theta_{0}|<h and equal to 0 otherwise. The integral in the exponent is precisely the integral over (x,θ)\ell(x,\theta), so we can rewrite this as

u1v1(x)=cn2h1n𝕊n1e1𝖪𝗇(x,θ)σ𝑑sχθ0h(θ)𝑑θ.\langle u_{1}v_{1}\rangle(x)=c_{n}^{2}h^{1-n}\fint_{\mathbb{S}^{n-1}}e^{-{\frac{1}{\mathsf{Kn}}}\int_{\ell(x,\theta)}\sigma ds}\chi^{h}_{\theta_{0}}(\theta)d\theta\,.

From (2.18) for small hh, we have

(3.7) u1v1(x)=e1𝖪𝗇(x,θ0)σ𝑑s+R,\langle u_{1}v_{1}\rangle(x)=e^{-\frac{1}{\mathsf{Kn}}\int_{\ell(x,\theta_{0})}\sigma ds}+R\,,

where RR is the error term

R\displaystyle R =𝕊n1(e1𝖪𝗇(x,θ)σ𝑑se1𝖪𝗇(x,θ0)σ𝑑s)cn2h1nχθ0h(θ)𝑑θ\displaystyle=\fint_{\mathbb{S}^{n-1}}(e^{-\frac{1}{\mathsf{Kn}}\int_{\ell(x,\theta)}\sigma ds}-e^{-\frac{1}{\mathsf{Kn}}\int_{\ell(x,\theta_{0})}\sigma ds})c_{n}^{2}h^{1-n}\chi^{h}_{\theta_{0}}(\theta)d\theta
=e1𝖪𝗇(x,θ0)σ𝑑s𝕊n1(e1𝖪𝗇((x,θ)σ𝑑s(x,θ0)σ𝑑s)1)cn2h1nχθ0h(θ)𝑑θ.\displaystyle=e^{-\frac{1}{\mathsf{Kn}}\int_{\ell(x,\theta_{0})}\sigma ds}\fint_{\mathbb{S}^{n-1}}(e^{-\frac{1}{\mathsf{Kn}}(\int_{\ell(x,\theta)}\sigma ds-\int_{\ell(x,\theta_{0})}\sigma ds)}-1)c_{n}^{2}h^{1-n}\chi^{h}_{\theta_{0}}(\theta)d\theta\,.

Since σCα(Ω)\sigma\in C^{\alpha}(\Omega), we have for sufficiently small hh

R=e1𝖪𝗇(x,θ0)σ𝑑s𝕊n1(e𝒪(hα)𝖪𝗇1)cn2h1nχθ0h(θ)𝑑θ.R=e^{-\frac{1}{\mathsf{Kn}}\int_{\ell(x,\theta_{0})}\sigma ds}\fint_{\mathbb{S}^{n-1}}(e^{-\frac{\mathcal{O}(h^{\alpha})}{\mathsf{Kn}}}-1)c_{n}^{2}h^{1-n}\chi^{h}_{\theta_{0}}(\theta)d\theta\,.

Note that the constant in the 𝒪\mathcal{O} notation merely depends on the regularity of σ\sigma. We can estimate |e𝒪(hα)𝖪𝗇1||e^{-\frac{\mathcal{O}(h^{\alpha})}{\mathsf{Kn}}}-1| by the Taylor remainder formula if 𝒪(hα)𝖪𝗇\frac{\mathcal{O}(h^{\alpha})}{\mathsf{Kn}} is small, or by 11 otherwise. In either case, we get

R=e1𝖪𝗇(x,θ0)σ𝑑s𝒪(hα)𝖪𝗇𝕊n1cn2h1nχθ0h(θ)𝑑θ.R=e^{-\frac{1}{\mathsf{Kn}}\int_{\ell(x,\theta_{0})}\sigma ds}\frac{\mathcal{O}(h^{\alpha})}{\mathsf{Kn}}\fint_{\mathbb{S}^{n-1}}c_{n}^{2}h^{1-n}\chi^{h}_{\theta_{0}}(\theta)d\theta\,.

Then (2.18) implies that

R=1𝖪𝗇e1𝖪𝗇(x,θ0)σ𝑑s𝒪(hα).R=\frac{1}{\mathsf{Kn}}e^{-\frac{1}{\mathsf{Kn}}\int_{\ell(x,\theta_{0})}\sigma ds}\mathcal{O}(h^{\alpha})\,.

Returning to (3.7), we conclude that

u1v1(x)=e1𝖪𝗇(x,θ0)σ𝑑s(1+𝖪𝗇1𝒪(hα))\langle u_{1}v_{1}\rangle(x)=e^{-\frac{1}{\mathsf{Kn}}\int_{\ell(x,\theta_{0})}\sigma ds}(1+\mathsf{Kn}^{-1}\mathcal{O}(h^{\alpha}))

as desired. ∎

The following proposition justifies the smallness of the remainder terms.

Proposition 3.2.

Under the same conditions as in Proposition 3.1, suppose 𝖪𝗇1\mathsf{Kn}\leq 1, there exists a constant CC independent of hh and 𝖪𝗇\mathsf{Kn} such that

ujvk(x)C𝖪𝗇4hn1\langle u_{j}\rangle\langle v_{k}\rangle(x)\leq C\mathsf{Kn}^{-4}h^{n-1}

for j,k=1,2j,k=1,2, and

ujvk(x)C𝖪𝗇4hn1\langle u_{j}v_{k}\rangle(x)\leq C\mathsf{Kn}^{-4}h^{n-1}

for j,k=1,2j,k=1,2 and j+k>2j+k>2 for each xx in Ω\Omega.

Proof.

First note that it follows directly from (3.5), (3.4), and σ>0\sigma>0, the angular average of u1u_{1} satisfies

(3.8) u1𝒪(hn12)for all xΩ.\langle u_{1}\rangle\leq\mathcal{O}(h^{\frac{n-1}{2}})\ \hbox{for all }x\in\Omega\,.

Moreover, Theorem 2.1 and (3.1) tell us that

u2L(Ω×Sn1)C𝖪𝗇2u1L(Ω).\|u_{2}\|_{L^{\infty}(\Omega\times S^{n-1})}\leq C\mathsf{Kn}^{-2}\left\|\langle u_{1}\rangle\right\|_{L^{\infty}(\Omega)}.

Combining with (3.8), we can deduce that

(3.9) u2L(Ω×Sn1)C𝖪𝗇2𝒪(hn12).\|u_{2}\|_{L^{\infty}(\Omega\times S^{n-1})}\leq C\mathsf{Kn}^{-2}\mathcal{O}(h^{\frac{n-1}{2}})\,.

The estimates (3.8) and (3.9) also hold for v1v_{1} and v2v_{2}, respectively. Together these estimates yield all of the bounds of Proposition 3.2. For instance, applying (3.8) to u1\langle u_{1}\rangle and (3.9) to v2L(Ω×Sn1)\|v_{2}\|_{L^{\infty}(\Omega\times S^{n-1})} we get

u1v2u1v2L(Ω×Sn1)𝖪𝗇2𝒪(hn1).\langle u_{1}v_{2}\rangle\leq\langle u_{1}\rangle\|v_{2}\|_{L^{\infty}(\Omega\times S^{n-1})}\leq\mathsf{Kn}^{-2}\mathcal{O}(h^{n-1})\,.

Similarly, we can derive

u2v2C𝖪𝗇4𝒪(hn1),\langle u_{2}v_{2}\rangle\leq C\mathsf{Kn}^{-4}\mathcal{O}(h^{n-1})\,,

where CC is a constant independent of 𝖪𝗇\mathsf{Kn} and hh. ∎

The main result is a natural consequence of the previous two propositions.

Proof of Theorem 2.4.

We first rewrite (3) as

H(x)+σ(x)𝖪𝗇u1v1\displaystyle H(x)+\frac{\sigma(x)}{\mathsf{Kn}}\langle u_{1}v_{1}\rangle
=σs(x)𝖪𝗇(u1v1+u1v2+u2v1+u2v2)\displaystyle=\frac{\sigma_{s}(x)}{\mathsf{Kn}}(\langle u_{1}\rangle\langle v_{1}\rangle+\langle u_{1}\rangle\langle v_{2}\rangle+\langle u_{2}\rangle\langle v_{1}\rangle+\langle u_{2}\rangle\langle v_{2}\rangle)
σ(x)𝖪𝗇(u1v2+u1v2+u2v2).\displaystyle\hskip 28.45274pt-\frac{\sigma(x)}{\mathsf{Kn}}(\langle u_{1}v_{2}\rangle+\langle u_{1}v_{2}\rangle+\langle u_{2}v_{2}\rangle)\,.

Applying Proposition 3.1 to the u1v1\langle u_{1}v_{1}\rangle term and Proposition 3.2 to everything else, for 𝖪𝗇1\mathsf{Kn}\ll 1, we get

H(x)+σ(x)𝖪𝗇(e1𝖪𝗇(x,θ0)σ𝑑s(1+𝖪𝗇1𝒪(hα)))=𝖪𝗇5𝒪(hn1).H(x)+\frac{\sigma(x)}{\mathsf{Kn}}\left(e^{-{\frac{1}{\mathsf{Kn}}}\int_{\ell(x,\theta_{0})}\sigma ds}(1+\mathsf{Kn}^{-1}\mathcal{O}(h^{\alpha}))\right)=\mathsf{Kn}^{-5}\mathcal{O}(h^{n-1})\,.

Multiplying through by e(x,θ0)σ𝖪𝗇𝑑se^{\int_{\ell(x,\theta_{0})}{\frac{\sigma}{\mathsf{Kn}}}ds}\,, one has

σ(x)𝖪𝗇+e(x,θ0)σ𝖪𝗇𝑑sH(x)=1𝖪𝗇2𝒪(hα)+1𝖪𝗇5𝒪(hn1)edsupσ𝖪𝗇.\frac{\sigma(x)}{\mathsf{Kn}}+e^{\int_{\ell(x,\theta_{0})}{\frac{\sigma}{\mathsf{Kn}}}ds}H(x)=\frac{1}{\mathsf{Kn}^{2}}\mathcal{O}(h^{\alpha})+\frac{1}{\mathsf{Kn}^{5}}\mathcal{O}(h^{n-1})e^{\frac{d\sup\sigma}{\mathsf{Kn}}}\,.

In the zero limit of 𝖪𝗇\mathsf{Kn}, the exponential term dominates, and the equation becomes

(3.10) σ(x)𝖪𝗇+e(x,θ0)σ𝖪𝗇𝑑sH(x)𝒪(hα)e2dsupσ𝖪𝗇.\frac{\sigma(x)}{\mathsf{Kn}}+e^{\int_{\ell(x,\theta_{0})}{\frac{\sigma}{\mathsf{Kn}}}ds}H(x)\leq\mathcal{O}(h^{\alpha})e^{\frac{2d\sup\sigma}{\mathsf{Kn}}}\,.

To estimate the exponential factor in front of H(x)H(x), we recall that from (3.5), u1u_{1} has explicit formula:

u1(x+τ+(x,θ0)θ0,θ0)=e1𝖪𝗇(x,θ0)σ𝑑sf(xτ(x,θ0)θ0,θ0),u_{1}(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})=e^{-{\frac{1}{\mathsf{Kn}}}\int_{\ell(x,\theta_{0})}\sigma ds}f(x-\tau_{-}(x,\theta_{0})\theta_{0},\theta_{0})\,,

and from (3.9) we also have:

|u2(x+τ+(x,θ0)θ0,θ0)|𝖪𝗇2𝒪(hn12).|u_{2}(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})|\leq\mathsf{Kn}^{-2}\mathcal{O}(h^{\frac{n-1}{2}})\,.

Considering the definition of the albedo operator:

𝒜(f)(x+τ+(x,θ0)θ0,θ0)=u(x+τ+(x,θ0)θ0,θ0)=u1(x+τ+(x,θ0)θ0,θ0)+u2(x+τ+(x,θ0)θ0,θ0),\mathcal{A}(f)(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})=u(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})=u_{1}(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})+u_{2}(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})\,,

we finally have

𝒜(f)(x+τ+(x,θ0)θ0,θ0)f(xτ(x,θ0)θ0,θ0)\displaystyle\frac{\mathcal{A}(f)(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})}{f(x-\tau_{-}(x,\theta_{0})\theta_{0},\theta_{0})} =e1𝖪𝗇(x,θ0)σ𝑑s+𝒪(hn12)𝖪𝗇2f(xτ(x,θ0)θ0,θ0)\displaystyle=e^{-{\frac{1}{\mathsf{Kn}}}\int_{\ell(x,\theta_{0})}\sigma ds}+\frac{\mathcal{O}(h^{\frac{n-1}{2}})}{\mathsf{Kn}^{2}f(x-\tau_{-}(x,\theta_{0})\theta_{0},\theta_{0})}
(3.11) =e1𝖪𝗇(x,θ0)σ𝑑s+𝒪(hn1)𝖪𝗇2,\displaystyle=e^{-{\frac{1}{\mathsf{Kn}}}\int_{\ell(x,\theta_{0})}\sigma ds}+\frac{\mathcal{O}(h^{n-1})}{\mathsf{Kn}^{2}}\,,

where we also used the fact that f|Γf|_{\Gamma_{-}} defined in (3.4). By substituting this back to (3.10), it immediately suggests:

σ(x)𝖪𝗇+f(xτ(x,θ0)θ0,θ0)𝒜(f)(x+τ+(x,θ0)θ0,θ0)H(x)=𝒪(hα)e2dsupσ𝖪𝗇+𝒪(hn1)𝖪𝗇2H(x).\frac{\sigma(x)}{\mathsf{Kn}}+{\color[rgb]{0,0,0}\definecolor[named]{pgfstrokecolor}{rgb}{0,0,0}\pgfsys@color@gray@stroke{0}\pgfsys@color@gray@fill{0}\frac{f(x-\tau_{-}(x,\theta_{0})\theta_{0},\theta_{0})}{\mathcal{A}(f)(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})}}H(x)=\mathcal{O}(h^{\alpha})e^{\frac{2d\sup\sigma}{\mathsf{Kn}}}+\frac{\mathcal{O}(h^{n-1})}{\mathsf{Kn}^{2}}H(x)\,.

Since (3.10) also implies that H(x)H(x) is of order e2dsupσ𝖪𝗇e^{\frac{2d\sup\sigma}{\mathsf{Kn}}}, we conclude

σ(x)𝖪𝗇+f(xτ(x,θ0)θ0,θ0)𝒜(f)(x+τ+(x,θ0)θ0,θ0)H(x)=𝒪(hα)e3dsupσ𝖪𝗇,\frac{\sigma(x)}{\mathsf{Kn}}+{\color[rgb]{0,0,0}\definecolor[named]{pgfstrokecolor}{rgb}{0,0,0}\pgfsys@color@gray@stroke{0}\pgfsys@color@gray@fill{0}\frac{f(x-\tau_{-}(x,\theta_{0})\theta_{0},\theta_{0})}{\mathcal{A}(f)(x+\tau_{+}(x,\theta_{0})\theta_{0},\theta_{0})}}H(x)=\mathcal{O}(h^{\alpha})e^{\frac{3d\sup\sigma}{\mathsf{Kn}}}\,,

Thus, Theorem 2.4 now follows. ∎

4. Numeric Examples

In this section we provide numerical evidence that verifies the analysis above.

As a numerical setup, we let Ω=[0,1]2\Omega=[0,1]^{2}, and mesh grids are sampled to resolve small scales in 𝖪𝗇\mathsf{Kn}. Since we only concern ourselves with the behavior of the different terms in H(x)H(x) in terms of 𝖪𝗇\mathsf{Kn} and hh, we use the simple media σ=1\sigma=1 all over the domain. In particular, the incoming light is concentrated at (x=0,y=1/2)(x=0,y=1/2) with hh indicating the concentration in velocity domain. In Figure 1 we plot the velocity average of the ballistic part, u1\langle u_{1}\rangle, for different 𝖪𝗇\mathsf{Kn} with h=2π25h=\frac{2\pi}{25} and h=14π25h=\frac{14\pi}{25}, and it can be clearly seen that smaller hh narrows down the spreading of u1\langle u_{1}\rangle while smaller 𝖪𝗇\mathsf{Kn} gives stronger decay of u1\langle u_{1}\rangle in space. Moreover, we also plot u2\langle u_{2}\rangle in Figure 2. Similar to the case of u1\langle u_{1}\rangle, as hh increases the function is more spread out, while smaller 𝖪𝗇\mathsf{Kn} leads to the stronger decay.

We also plot u1v1\langle u_{1}v_{1}\rangle as a function of 𝖪𝗇\mathsf{Kn} and hh. As seen in Figure 3, the quantity decays exponentially fast with respect to small 𝖪𝗇\mathsf{Kn} and algebraically fast with respect to small hh, which confirms with the result in Proposition 3.1. In addition, the remainder term H(x)1𝖪𝗇u1v1H(x)-\frac{1}{\mathsf{Kn}}\langle u_{1}v_{1}\rangle is plotted in Figure 4.

Lastly, the quantitative dependence of error on 𝖪𝗇\mathsf{Kn} and hh is plotted in Figure 5 and the observation confirms with the prediction of our theorem. Specifically, this error is an exponential function of 1𝖪𝗇\frac{1}{\mathsf{Kn}} and grows algebraically with respect to hh, where the error is defined to be the relative error, namely:

Error(x)=𝖪𝗇H(x)u1v1u1v1\text{Error}(x)=\frac{\mathsf{Kn}H(x)-\langle u_{1}v_{1}\rangle}{\langle u_{1}v_{1}\rangle}

and the plot shows the L2L^{2} norm over the space xΩx\in\Omega.

Refer to caption
Figure 1. The plot show u1\langle u_{1}\rangle with different 𝖪𝗇\mathsf{Kn} and hh. From left to right, 𝖪𝗇\mathsf{Kn} decreases as 2k2^{-k} with k=0,1,2,3,4k=0,1,2,3,4. The two rows are for hh being 2π25\frac{2\pi}{25} and 14π25\frac{14\pi}{25} respectively.
Refer to caption
Figure 2. The plot show u2\langle u_{2}\rangle with different 𝖪𝗇\mathsf{Kn} and hh. From left to right, 𝖪𝗇\mathsf{Kn} decreases as 2k2^{-k} with k=0,1,2,3,4k=0,1,2,3,4. The two rows are for hh being 2π25\frac{2\pi}{25} and 14π25\frac{14\pi}{25} respectively.
Refer to caption
Figure 3. As hh increases, the intensity of u1v1\langle u_{1}v_{1}\rangle is more spread out, and as 𝖪𝗇\mathsf{Kn} decreases, the intensity quickly decays and is low in the interior of the domain.
Refer to caption
Figure 4. The plot shows H(x)u1v1H(x)-\langle u_{1}v_{1}\rangle as a function of hh and 𝖪𝗇\mathsf{Kn}.
Refer to caption
Refer to caption
Figure 5. These two plots show the error as a function of 𝖪𝗇\mathsf{Kn} and hh. For every fixed 𝖪𝗇\mathsf{Kn}, the error grows almost linearly with respect to hh, and for every fixed hh, the logarithmic error grows almost linearly with respect to 1𝖪𝗇\frac{1}{\mathsf{Kn}}.

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