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**Solid Earth**
An interactive open-access journal of the European Geosciences Union

Journal topic

- About
- Editorial board
- Articles
- Special issues
- Highlight articles
- Manuscript tracking
- Subscribe to alerts
- Peer review
- For authors
- For reviewers
- EGU publications
- Imprint
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- About
- Editorial board
- Articles
- Special issues
- Highlight articles
- Manuscript tracking
- Subscribe to alerts
- Peer review
- For authors
- For reviewers
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- Abstract
- Introduction
- Theory and applications of a classical wave field representation
- Theory and applications of a modified single-sided wave field representation
- Conclusions
- Code availability
- Author contributions
- Competing interests
- Special issue statement
- Acknowledgements
- Review statement
- References
- Supplement

SE | Volume 10, issue 2

Solid Earth, 10, 517–536, 2019

https://doi.org/10.5194/se-10-517-2019

© Author(s) 2019. This work is distributed under

the Creative Commons Attribution 4.0 License.

https://doi.org/10.5194/se-10-517-2019

© Author(s) 2019. This work is distributed under

the Creative Commons Attribution 4.0 License.

Special issue: Advances in seismic imaging across the scales

**Review article**
11 Apr 2019

**Review article** | 11 Apr 2019

Green's theorem in seismic imaging across the scales

- Department of Geoscience and Engineering, Delft University of Technology, Stevinweg 1, 2628 CN Delft, the Netherlands

- Department of Geoscience and Engineering, Delft University of Technology, Stevinweg 1, 2628 CN Delft, the Netherlands

**Correspondence**: Kees Wapenaar (c.p.a.wapenaar@tudelft.nl)

**Correspondence**: Kees Wapenaar (c.p.a.wapenaar@tudelft.nl)

Abstract

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The earthquake seismology and seismic exploration communities have developed a variety of seismic imaging methods for passive- and active-source data. Despite the seemingly different approaches and underlying principles, many of those methods are based in some way or another on Green's theorem. The aim of this paper is to discuss a variety of imaging methods in a systematic way, using a specific form of Green's theorem (the homogeneous Green's function representation) as a common starting point. The imaging methods we cover are time-reversal acoustics, seismic interferometry, back propagation, source–receiver redatuming and imaging by double focusing. We review classical approaches and discuss recent developments that fully account for multiple scattering, using the Marchenko method. We briefly indicate new applications for monitoring and forecasting of responses to induced seismic sources, which are discussed in detail in a companion paper.

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How to cite.

Wapenaar, K., Brackenhoff, J., and Thorbecke, J.: Green's theorem in seismic imaging across the scales, Solid Earth, 10, 517–536, https://doi.org/10.5194/se-10-517-2019, 2019.

1 Introduction

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Through the years, the earthquake seismology and seismic exploration communities have developed a variety of seismic imaging methods for passive- and active-source data, based on a wide range of principles such as time-reversal acoustics, Green's function retrieval by noise correlation (a form of seismic interferometry), back propagation (also known as holography) and source–receiver redatuming. Many of these methods are rooted in some way or another in Green's theorem (Green, 1828; Morse and Feshbach, 1953; Challis and Sheard, 2003). The current paper is a modest attempt to discuss a variety of imaging methods and their underlying principles in a systematic way, using Green's theorem as the common starting point. We are certainly not the first to recognize links between different imaging methods. For example, Esmersoy and Oristaglio (1988) discussed the link between back propagation and reverse-time migration, Derode et al. (2003) derived Green's function retrieval from the principle of time-reversal acoustics by physical reasoning and Schuster et al. (2004) linked seismic interferometry to back propagation, to name but a few.

We start by reviewing a specific form of Green's theorem, namely the classical representation of the homogeneous Green's function, originally developed for optical holography (Porter, 1970; Porter and Devaney, 1982). The homogeneous Green's function is the superposition of the causal Green's function and its time reversal. We use its surface-integral representation to derive time-reversal acoustics, seismic interferometry, back propagation, source–receiver redatuming and imaging by double focusing in a systematic way, confirming that these methods are all very similar. We briefly discuss the potential and the limitations of these methods. Because the classical homogeneous Green's function representation is based on a closed surface integral, an implicit assumption of all of these methods is that the medium of interest can be accessed from all sides. Due to the fact that acquisition is limited to the Earth's surface in most seismic applications, a major part of the closed surface integral is necessarily neglected. This implies that errors are introduced and, in particular, that multiple reflections between layer interfaces are not correctly handled. To address this issue, we also discuss a recently developed single-sided representation of the homogeneous Green's function. We use this to derive, in the same systematic way, modified seismic imaging methods that account for multiple reflections between layer interfaces. In a companion paper (Brackenhoff et al., 2019) we extensively discuss applications for monitoring induced seismicity.

Although the solid Earth supports elastodynamic (vectorial) waves, to facilitate the comparison of the different methods discussed in this paper we have chosen to consider scalar waves only. Scalar waves, which obey the acoustic wave equation, serve as an approximation for compressional body waves propagating through the solid Earth, or for the fundamental mode of surface waves propagating along the Earth's surface, depending on the application. In several places we give references to extensions of the methods that account for the full elastodynamic wave field.

2 Theory and applications of a classical wave field representation

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We consider an inhomogeneous lossless acoustic
medium, with mass density *ρ*(** x**)
and compressibility

$$\begin{array}{}\text{(1)}& {\partial}_{i}\left({\mathit{\rho}}^{-\mathrm{1}}{\partial}_{i}G\right)-\mathit{\kappa}{\partial}_{t}^{\mathrm{2}}G=-\mathit{\delta}(\mathit{x}-{\mathit{x}}_{\mathrm{A}}){\partial}_{t}\mathit{\delta}\left(t\right),\end{array}$$

where ∂_{t} stands for the temporal differential operator
$\partial /\partial t$ and ∂_{i} represents the spatial differential operator
$\partial /\partial {x}_{i}$. Latin subscripts (except *t*) take on the values 1,
2 and 3, and Einstein's summation convention applies to repeated subscripts.
We impose the condition $G(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)=\mathrm{0}$ for *t*<0, so that $G(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$ for *t*>0 is the causal solution of Eq. (1),
representing a wave field originating from the source at *x*_{A}. Note
that the Green's function obeys source–receiver reciprocity, i.e.,
$G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},t)=G({\mathit{x}}_{\mathrm{A}},{\mathit{x}}_{\mathrm{B}},t)$, assuming both are causal and
obey the same boundary conditions (Rayleigh, 1878; Landau and Lifshitz, 1959; Morse and Ingard, 1968). This property will be frequently used without always mentioning
it explicitly.

The time-reversal of the Green's function, $G(\mathit{x},{\mathit{x}}_{\mathrm{A}},-t)$, is the acausal solution of Eq. (1), which, for *t*<0,
represents a wave field converging to a sink at *x*_{A}.
The homogeneous Green's function ${G}_{\mathrm{h}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$ is defined as the superposition of the Green's function and its time reversal, according to

$$\begin{array}{}\text{(2)}& {G}_{\mathrm{h}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)=G(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)+G(\mathit{x},{\mathit{x}}_{\mathrm{A}},-t).\end{array}$$

It is called “homogeneous” because it obeys a homogeneous wave equation,
i.e., a wave equation without a singularity on the right-hand side. Hence
${\partial}_{i}\left({\mathit{\rho}}^{-\mathrm{1}}{\partial}_{i}{G}_{\mathrm{h}}\right)-\mathit{\kappa}{\partial}_{t}^{\mathrm{2}}{G}_{\mathrm{h}}=\mathrm{0}$,
in which the medium parameters *ρ*(** x**) and

$$\begin{array}{}\text{(3)}& u\left(\mathit{\omega}\right)=\underset{-\mathrm{\infty}}{\overset{\mathrm{\infty}}{\int}}u\left(t\right)\mathrm{exp}\left(i\mathit{\omega}t\right)\mathrm{d}t.\end{array}$$

Here *ω* denotes angular frequency and *i* the imaginary unit.
For notational convenience, we use the same symbol for quantities in the time domain and in the frequency domain. The wave equation for the Green's function
in the frequency domain reads

$$\begin{array}{}\text{(4)}& {\partial}_{i}\left({\mathit{\rho}}^{-\mathrm{1}}{\partial}_{i}G\right)+\mathit{\kappa}{\mathit{\omega}}^{\mathrm{2}}G=i\mathit{\omega}\mathit{\delta}(\mathit{x}-{\mathit{x}}_{\mathrm{A}}).\end{array}$$

The homogeneous Green's function in the frequency domain is defined as

$$\begin{array}{ll}{\displaystyle}{G}_{\mathrm{h}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})& {\displaystyle}=G(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})+{G}^{*}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\\ \text{(5)}& {\displaystyle}& {\displaystyle}=\mathrm{2}\mathrm{\Re}\mathit{\left\{}G\right(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega}\left)\mathit{\right\}},\end{array}$$

where the superscript asterisk denotes complex conjugation, and ℜ means that the real part is taken. The classical representation of the homogeneous Green's function reads (Porter, 1970; Oristaglio, 1989; Supplement, Sect. S1.3)

$$\begin{array}{ll}{\displaystyle}{G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})& {\displaystyle}=\underset{\mathbb{S}}{\oint}{\displaystyle \frac{\mathrm{1}}{i\mathit{\omega}\mathit{\rho}\left(\mathit{x}\right)}}\left(\mathit{\right\{}{\partial}_{i}G(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})\mathit{\left\}}{G}^{*}\right(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\\ \text{(6)}& {\displaystyle}& {\displaystyle}-G(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){\partial}_{i}{G}^{*}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})){n}_{i}\mathrm{d}\mathit{x},\end{array}$$

see Fig. 1. Here 𝕊 is an arbitrarily shaped closed surface with an outward pointing normal vector $\mathit{n}=({n}_{\mathrm{1}},{n}_{\mathrm{2}},{n}_{\mathrm{3}})$,
which does not necessarily coincide with the boundary of the medium.
It is assumed that *x*_{A} and *x*_{B} are situated inside
𝕊. Note that the aforementioned authors use a slightly different
definition of the Green's function (the factor *i**ω* in the source term
in Eq. (4) is absent in their case). Nevertheless, we will
refer to Eq. (6) as the classical homogeneous Green's
function representation. When 𝕊 is sufficiently smooth and the
medium outside 𝕊 is homogeneous (with mass density *ρ*_{0},
compressibility *κ*_{0} and propagation velocity
${c}_{\mathrm{0}}=({\mathit{\kappa}}_{\mathrm{0}}{\mathit{\rho}}_{\mathrm{0}}{)}^{-\mathrm{1}/\mathrm{2}}$), the two terms under the integral in Eq. (6) are nearly identical (but opposite in sign); hence, this
representation may be approximated by

$$\begin{array}{}\text{(7)}& {G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})=-\mathrm{2}\underset{\mathbb{S}}{\oint}{\displaystyle \frac{\mathrm{1}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}G(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){\partial}_{i}{G}^{*}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega}){n}_{i}\mathrm{d}\mathit{x}.\end{array}$$

The main approximation is that evanescent waves are neglected (Zheng et al., 2011; Wapenaar et al., 2011).

In the following sections we discuss different imaging methods. Each time we first introduce the specific method in an intuitive way, after which we present a more quantitative derivation based on Eq. (7).

Time-reversal acoustics has been pioneered by Fink and co-workers
(Fink, 1992, 2006; Derode et al., 1995; Draeger and Fink, 1999). It makes use of
the fact that the acoustic wave equation for a lossless medium is invariant
under time reversal (for discussions regarding elastodynamic time-reversal
methods we refer the reader to Scalerandi et al., 2009; Anderson et al., 2009;
Wang and McMechan, 2015). Hence, given a particular solution of the wave equation,
its time-reversal obeys the same wave equation. Figure 2 illustrates
the principle (following Derode et al., 1995, and Fink, 2006). In
Fig. 2a, an impulsive source at *x*_{A} emits a wave field which,
after propagation through a highly scattering medium, is recorded by
receivers at ** x** on the surface 𝕊

The time-reversal principle can be made more quantitative using Green's theorem (Fink, 2006). First, using the equation of motion, we express the normal component of the particle velocity at 𝕊 in the frequency domain as

$$\begin{array}{}\text{(8)}& {v}_{\mathrm{n}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})={\displaystyle \frac{\mathrm{1}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}{\partial}_{i}G(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega}){n}_{i}s\left(\mathit{\omega}\right),\end{array}$$

where *s*(*ω*) is the spectrum of the source at *x*_{A}.
Using this in the homogeneous Green's function representation of Eq. (7) we obtain

$$\begin{array}{}\text{(9)}& {G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega}){s}^{*}\left(\mathit{\omega}\right)=\mathrm{2}\underset{\mathbb{S}}{\oint}G({\mathit{x}}_{\mathrm{B}},\mathit{x},\mathit{\omega}){v}_{\mathrm{n}}^{*}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}\mathit{x},\end{array}$$

or, in the time domain (using Eq. 2),

$$\begin{array}{ll}{\displaystyle}\mathit{\left\{}G\right({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},t)& {\displaystyle}+G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},-t)\mathit{\}}*s(-t)\\ \text{(10)}& {\displaystyle}& {\displaystyle}=\mathrm{2}\underset{\mathbb{S}}{\oint}\underset{\text{\u201cpropagator\u201d}}{\underbrace{G({\mathit{x}}_{\mathrm{B}},\mathit{x},t)}}*\underset{\text{\u201csecondary\hspace{0.17em}sources\u201d}}{\underbrace{{v}_{\mathrm{n}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},-t)}}\mathrm{d}\mathit{x},\end{array}$$

where the inline asterisk (*) denotes temporal convolution. This is the
fundamental expression for time-reversal acoustics. The integrand on the
right-hand side formulates the propagation of the time-reversed field
${v}_{\mathrm{n}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},-t)$ through the inhomogeneous medium by the Green's
function $G({\mathit{x}}_{\mathrm{B}},\mathit{x},t)$ from the sources at ** x** on the
boundary 𝕊 to any receiver position

$$\begin{array}{}\text{(11)}& \left[\mathit{\right\{}G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},t)+G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},-t)\mathit{\}}*s(t){]}_{t=\mathrm{0}}=-{\displaystyle \frac{\overline{\mathit{\rho}}}{\mathrm{2}\mathit{\pi}r}}\dot{s}(d/\overline{c})\end{array}$$

(Douma and Snieder, 2015; Wapenaar and Thorbecke, 2017),
where $\overline{c}$ and $\overline{\mathit{\rho}}$ are the propagation velocity and mass density in the neighborhood of
*x*_{A}, *d* is the distance of *x*_{B} to *x*_{A},
and $\dot{s}\left(t\right)$ denotes the derivative of the source function *s*(*t*).

It should be noted that the integration in Eq. (10) takes place over sources on a closed surface 𝕊.
However, in the example in Fig. 2 the time-reversed field is emitted into the medium from a finite open surface 𝕊_{0}.
Despite this discrepancy, a good focus is obtained around *x*_{A}.
Nevertheless, Fig. 2c also shows a noisy field at *t*=0, particularly in the scattering region. According to Eq. (10),
this noisy field would vanish if the time-reversed field was emitted from a closed surface into the
medium.

Figure 2 is representative of ultrasonic applications of time-reversal acoustics, because in those applications it is feasible to physically emit the time-reversed field into the real medium (Fink, 1992, 2006; Cassereau and Fink, 1992; Derode et al., 1995; Draeger and Fink, 1999; Tanter and Fink, 2014). Time-reversal acoustics also finds applications in geophysics at various scales, but in those applications the time-reversed field is emitted numerically into a model of the Earth. This is used for source characterization (McMechan, 1982; Gajewski and Tessmer, 2005; Larmat et al., 2010) and for structural imaging by reverse-time migration (McMechan, 1983; Whitmore, 1983; Baysal et al., 1983; Etgen et al., 2009; Zhang and Sun, 2009; Clapp et al., 2010). In these model-driven applications it is much more difficult to account for multiple scattering, which is therefore usually ignored. Moreover, the scattering mechanism is often very different, particularly in applications dedicated to imaging the Earth's crust. We discuss a second time-reversal example to illustrate this.

Whereas in Fig. 2 we considered short-period multiple scattering
at randomly distributed point-like scatterers in a homogeneous background
medium, in Fig. 3 we consider long-period multiple scattering at
extended interfaces between layers with distinct medium parameters (which is
representative for multiple scattering in the Earth's crust). Figure 3a
shows the response ${v}_{\mathrm{n}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$ to a source
at *x*_{A} inside a layered medium, observed at the surface
𝕊_{0}. The time-reversal of this response is emitted from
𝕊_{0} into the same layered medium. The field at *t*=0 is shown in
Fig. 3b. We again observe a clear focus at *x*_{A}, but this
time the multiple scattering does not contribute to the resolution of the
focus (because there are no point scatterers that effectively widen the
aperture angle). On the contrary, the multiply scattered waves give rise to
strong, distinct artefacts in other regions in the medium. Again, these
artefacts would disappear entirely if the time-reversed field was
emitted from a closed surface, but this is of course unrealistic for
geophysical applications. In Sect. 3.2 we discuss a modified
approach to single-sided time-reversal acoustics which does not suffer from
artefacts such as those in Fig. 3b.

Under certain conditions, the cross-correlation of passive ambient-noise recordings at two receivers converges to the response that would be measured at one of the receivers if there were an impulsive source at the position of the other. This methodology, which creates a virtual source at the position of an actual receiver, is known as Green's function retrieval by noise correlation (a form of seismic interferometry). At the ultrasonic scale it has been pioneered by Weaver and co-workers (Weaver and Lobkis, 2001, 2002; Lobkis and Weaver, 2001), and the object of investigation at this scale is often a closed system (i.e., a finite specimen with reflecting boundaries on all sides). Early applications for open systems are discussed by Aki (1957), Claerbout (1968), Duvall et al. (1993), Rickett and Claerbout (1999), Schuster (2001), Wapenaar et al. (2002), Campillo and Paul (2003), Derode et al. (2003), Snieder (2004), Schuster et al. (2004), Roux et al. (2005), Sabra et al. (2005a), Larose et al. (2006) and Draganov et al. (2007). A detailed discussion of the many aspects of seismic interferometry is beyond the scope of this paper. Overviews of seismic interferometry, for passive as well as controlled-source data, are given by Schuster (2009), Wapenaar et al. (2010) and Nakata et al. (2019).

Figure 4 illustrates the principle for passive ambient-noise data.
In Fig. 4a, a distribution of uncorrelated noise sources *N*(** x**,

We use the homogeneous Green's function representation of Eq. (7) to explain this in a more quantitative way (Wapenaar et al., 2002; Weaver and Lobkis, 2004; van Manen et al., 2005; Korneev and Bakulin, 2006). Representations for elastodynamic interferometry are discussed by Wapenaar (2004), Halliday and Curtis (2008) and Kimman and Trampert (2010). Applying source–receiver reciprocity to the Green's functions under the integral in Eq. (7), we obtain

$$\begin{array}{}\text{(12)}& {G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})=-{\displaystyle \frac{\mathrm{2}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}\underset{\mathbb{S}}{\oint}G({\mathit{x}}_{\mathrm{B}},\mathit{x},\mathit{\omega}){\partial}_{i}{G}^{*}({\mathit{x}}_{\mathrm{A}},\mathit{x},\mathit{\omega}){n}_{i}\mathrm{d}\mathit{x}.\end{array}$$

The integrand can be interpreted as the Fourier transform of the
cross-correlation of responses to sources at ** x** on closed surface
𝕊, observed by receivers at

$$\begin{array}{}\text{(13)}& {\partial}_{i}G({\mathit{x}}_{\mathrm{A}},\mathit{x},\mathit{\omega}){n}_{i}\to {\displaystyle \frac{i\mathit{\omega}\left|\mathrm{cos}\right(\mathit{\alpha}\left(\mathit{x}\right)\left)\right|}{{c}_{\mathrm{0}}}}G({\mathit{x}}_{\mathrm{A}},\mathit{x},\mathit{\omega}).\end{array}$$

Here *α*(** x**) is the angle between the normal to 𝕊 at

$$\begin{array}{}\text{(14)}& {G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\approx {\displaystyle \frac{\mathrm{2}}{{\mathit{\rho}}_{\mathrm{0}}{c}_{\mathrm{0}}}}\underset{\mathbb{S}}{\oint}G({\mathit{x}}_{\mathrm{B}},\mathit{x},\mathit{\omega}){G}^{*}({\mathit{x}}_{\mathrm{A}},\mathit{x},\mathit{\omega})\mathrm{d}\mathit{x},\end{array}$$

or, in the time domain (using Eq. 2),

$$\begin{array}{ll}{\displaystyle}G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},t)& {\displaystyle}+G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},-t)\\ \text{(15)}& {\displaystyle}& {\displaystyle}\approx {\displaystyle \frac{\mathrm{2}}{{\mathit{\rho}}_{\mathrm{0}}{c}_{\mathrm{0}}}}\underset{\mathbb{S}}{\oint}G({\mathit{x}}_{\mathrm{B}},\mathit{x},t)*G({\mathit{x}}_{\mathrm{A}},\mathit{x},-t)\mathrm{d}\mathit{x}\end{array}$$

(the approximation sign refers to the far-field approximation, with the term
$\left|\mathrm{cos}\right(\mathit{\alpha}\left(\mathit{x}\right)\left)\right|$ ignored). This expression shows that the Green's
function and its time-reversal between *x*_{A} and *x*_{B} can be
approximately retrieved from the cross-correlation of responses to impulsive
monopole sources at ** x** on 𝕊, followed by an integration
along 𝕊. This expression, and variants of it, are used in
situations where responses to individual transient sources are available
(Kumar and Bostock, 2006; Schuster and Zhou, 2006; Bakulin and Calvert, 2006; Abe et al., 2007; Tonegawa et al., 2009; Ruigrok et al., 2010). Next, we modify this expression for
simultaneous noise sources. For a distribution of noise sources

$$\begin{array}{}\text{(16)}& {\displaystyle}& {\displaystyle}p({\mathit{x}}_{\mathrm{A}},t)=\underset{\mathbb{S}}{\oint}G({\mathit{x}}_{\mathrm{A}},\mathit{x},t)*N(\mathit{x},t)\mathrm{d}\mathit{x},\text{(17)}& {\displaystyle}& {\displaystyle}p({\mathit{x}}_{\mathrm{B}},t)=\underset{\mathbb{S}}{\oint}G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}^{\prime},t)*N({\mathit{x}}^{\prime},t)\mathrm{d}{\mathit{x}}^{\prime}.\end{array}$$

Assuming the noise sources are mutually uncorrelated, they obey

$$\begin{array}{}\text{(18)}& \langle N({\mathit{x}}^{\prime},t)*N(\mathit{x},-t)\rangle ={\mathit{\delta}}_{\mathbb{S}}(\mathit{x}-{\mathit{x}}^{\prime}){C}_{N}\left(t\right),\end{array}$$

where *C*_{N}(*t*) is the autocorrelation of the noise (which is assumed to be
the same for all sources), 〈⋅〉 stands for time averaging
and ${\mathit{\delta}}_{\mathbb{S}}(\mathit{x}-{\mathit{x}}^{\prime})$ is a 2-D delta function defined in
𝕊. Cross-correlation of the observed noise fields in *x*_{A}
and *x*_{B} gives

$$\begin{array}{ll}{\displaystyle}\langle p({\mathit{x}}_{\mathrm{B}},t)*p({\mathit{x}}_{\mathrm{A}},-t)\rangle & {\displaystyle}=\langle \underset{\mathbb{S}}{\oint}\underset{\mathbb{S}}{\oint}G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}^{\prime},t)*N({\mathit{x}}^{\prime},t)\\ \text{(19)}& {\displaystyle}& {\displaystyle}*G({\mathit{x}}_{\mathrm{A}},\mathit{x},-t)*N(\mathit{x},-t)\mathrm{d}{\mathit{x}}^{\prime}\mathrm{d}\mathit{x}\rangle .\end{array}$$

Using Eq. (18) this becomes

$$\begin{array}{ll}{\displaystyle}& {\displaystyle}\langle p({\mathit{x}}_{\mathrm{B}},t)*p({\mathit{x}}_{\mathrm{A}},-t)\rangle \\ \text{(20)}& {\displaystyle}& {\displaystyle}\phantom{\rule{0.25em}{0ex}}=\underset{\mathbb{S}}{\oint}G({\mathit{x}}_{\mathrm{B}},\mathit{x},t)*G({\mathit{x}}_{\mathrm{A}},\mathit{x},-t)*{C}_{N}\left(t\right)\mathrm{d}\mathit{x}.\end{array}$$

Note that the right-hand side resembles that of Eq. (15).
Hence, if we convolve both sides of Eq. (15) with *C*_{N}(*t*), we can replace its right-hand side
with the left-hand side of Eq. (20), according to

$$\begin{array}{ll}{\displaystyle}\mathit{\left\{}G\right({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},t)& {\displaystyle}+G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},-t)\mathit{\}}*{C}_{N}(t)\\ \text{(21)}& {\displaystyle}& {\displaystyle}\approx {\displaystyle \frac{\mathrm{2}}{{\mathit{\rho}}_{\mathrm{0}}{c}_{\mathrm{0}}}}\langle p({\mathit{x}}_{\mathrm{B}},t)*p({\mathit{x}}_{\mathrm{A}},-t)\rangle .\end{array}$$

Equation (21) (and its extension for elastodynamic waves)
is the fundamental expression of Green's function retrieval from ambient noise in an open system.
The right-hand side represents the cross-correlation of the ambient-noise responses at two receivers at *x*_{A} and *x*_{B}.
The left-hand side consists of a superposition of the virtual-source response
$G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},t)*{C}_{N}\left(t\right)$ and its time-reversal $G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},-t)*{C}_{N}\left(t\right)$.
Originally this methodology was based on intuitive arguments and was only used to retrieve the direct wave between the two receivers.
As Eq. (21) is derived from a representation which holds for an inhomogeneous medium, it
follows that the retrieved response is that of the inhomogeneous medium,
hence, in principle it includes scattering (this will be illustrated below
with a numerical example). The derivation that leads to Eq. (21) also reveals the approximations underlying the methodology of
Green's function retrieval.

According to Eqs. (16) and (17), it is assumed that the
fields *p*(*x*_{A},*t*) and *p*(*x*_{B},*t*) are the responses to noise
sources on a closed surface 𝕊. However, in the example in Fig. 4, the noise field is emitted into the medium from a finite open
surface 𝕊_{0}. A consequence of this discrepancy is that the
retrieved response in Fig. 4b lacks the acausal term $G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},-t)*{C}_{N}\left(t\right)$.
Moreover, the causal term $G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},t)*{C}_{N}\left(t\right)$
is blurred by scattering noise, which does not vanish with
longer time-averaging. According to Eqs. (16), (17) and
(21), the retrieved response would contain the causal and acausal
terms and the scattering noise would vanish if the noise field was
emitted from a closed surface and the recorded fields at *x*_{A} and
*x*_{B} were correlated for a long enough time.

Figure 4 is representative of seismic surface-wave interferometry
(Campillo and Paul, 2003; Sabra et al., 2005b; Shapiro and Campillo, 2004; Bensen et al., 2007), in
which case Fig. 4a should be interpreted as a plan view, with the
noise signals representing microseisms, 𝕊_{0} representing a coast
line and the Green's functions representing the fundamental mode of surface
waves (with additional effort, higher-mode surface waves can be retrieved as
well – Halliday and Curtis, 2008; Kimman and Trampert, 2010; Kimman et al., 2012; van Dalen et al., 2014).
The retrieved surface-wave Green's functions are typically used for
tomographic imaging (Sabra et al., 2005a; Shapiro et al., 2005; Bensen et al., 2008; Lin et al., 2009). Seismic interferometry can also be used for reflection imaging
of the Earth's crust with body waves. Because the scattering mechanism is
very different, we discuss a second example to illustrate seismic
interferometry with body waves. Figure 5a shows the same layered
medium as Fig. 3a, but this time with noise sources at
𝕊_{0} in the subsurface and with the upper surface being a free
surface. For this situation the part of the closed-surface integral over the
free surface in Eq. (6) vanishes. Hence, the closed
surface integrals in Eqs. (16) and (17) can be replaced by
open surface integrals over the noise sources in the subsurface in Fig. 5a.
The responses to these noise sources, shown in the upper part of Fig. 5a,
are recorded by receivers below the free surface. For *p*(*x*_{A},*t*)
we take the central trace (indicated by the red box) and for *p*(*x*_{B},*t*)
(with variable *x*_{B}) all other traces. We apply Eq. (21)
to obtain the virtual-source response $G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},t)*{C}_{N}\left(t\right)$
and its time-reversal $G({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},-t)*{C}_{N}\left(t\right)$ for
a fixed virtual source at *x*_{A} and receivers at variable *x*_{B}.
The causal part is shown in Fig. 5b. In agreement with the theory,
this is the full reflection response of the layered medium, including
multiple reflections. Applications of reflection-response retrieval from
ambient noise range from the shallow subsurface to the global scale
(Chaput and Bostock, 2007; Draganov et al., 2009, 2013; Forghani and Snieder, 2010; Ryberg, 2011; Ruigrok et al., 2012; Tonegawa et al., 2013; Panea et al., 2014; Boué et al., 2014; Boullenger et al., 2015; Oren and Nowack, 2017; Almagro Vidal et al., 2018). As
body waves in ambient noise are usually weak in comparison with surface
waves, much effort is spent on recovering the body waves from behind the
surface waves. Reflection responses retrieved by body-wave interferometry are
typically used for reflection imaging.

For both methods discussed here (surface-wave interferometry and body-wave interferometry) we assumed that the noise sources are regularly distributed along a part of 𝕊 and that they all have the same autocorrelation function. In many practical situations the source distribution is irregular, and the autocorrelations are different for different sources. Several approaches have been developed to account for these issues, such as iterative correlation (Stehly et al., 2008), multidimensional deconvolution (Wapenaar and van der Neut, 2010; van der Neut et al., 2011), directional balancing (Curtis and Halliday, 2010a) and generalized interferometry, circumventing Green's function retrieval (Fichtner et al., 2017).

Given a wave field observed at the surface of a medium, the field inside the
medium can be obtained by back propagation (Schneider, 1978; Berkhout, 1982; Fischer and Langenberg, 1984; Wiggins, 1984; Langenberg et al., 1986). Because back
propagation implies retrieving a 3-D field inside a volume from a 2-D field at
a surface, it is also known as holography (Porter and Devaney, 1982; Lindsey and Braun, 2004). Figure 6 illustrates the principle. In Fig. 6a,
the field at the finite open surface 𝕊_{0} due to a
source at *x*_{A} inside a layered medium (the same medium as in Figs. 3
and 5) is back propagated to an arbitrary point *x*_{B}
inside the medium by the time-reversed direct arrival of the Green's
function, ${G}_{\mathrm{d}}(\mathit{x},{\mathit{x}}_{\mathrm{B}},-t)$. Figure 6b shows ${G}_{\mathrm{d}}(\mathit{x},{\mathit{x}}_{\mathrm{B}},-t)$
(for fixed *x*_{B}) and a snapshot of the back
propagated field at time instant *t*_{1}>0 for all *x*_{B}. Note that above
the source (which is located at *x*_{A}) the primary upgoing field coming
from the source is clearly retrieved. However, the field below the source is
not retrieved. Moreover, several artefacts are present because multiple
reflections between the layer interfaces are not accounted for.

Back propagation is conceptually different from time-reversal acoustics. In time-reversal acoustics the observed wave field is reversed in time and (physically or numerically) emitted into the medium, whereas in back propagation the original observed wave field is numerically back-propagated through the medium by a time-reversed Green's function. Despite this conceptual difference (time reversal of the wave field versus time reversal of the propagation operator), it is not surprising that these methods are very similar from a mathematical point of view.

A quantitative discussion of back propagation follows from Eq. (7). By interchanging
*x*_{A} and *x*_{B} and multiplying both
sides by the spectrum *s*(*ω*) of the source at *x*_{A}, we
obtain

$$\begin{array}{ll}{\displaystyle}& {\displaystyle}{G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})s\left(\mathit{\omega}\right)\\ \text{(22)}& {\displaystyle}& {\displaystyle}\phantom{\rule{0.25em}{0ex}}=-\mathrm{2}\underset{\mathbb{S}}{\oint}{\displaystyle \frac{\mathrm{1}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}\mathit{\left\{}{\partial}_{i}{G}^{*}\right(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}\left)\mathit{\right\}}G(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})s\left(\mathit{\omega}\right){n}_{i}\mathrm{d}\mathit{x}.\end{array}$$

Here $G(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})s\left(\mathit{\omega}\right)$ stands for the observed field
$p(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$ at the surface 𝕊, and
$-\frac{\mathrm{2}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}{\partial}_{i}{G}^{*}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){n}_{i}$ is the
back propagation operator, both in the frequency domain. Hence, in theory the
exact field ${G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})s\left(\mathit{\omega}\right)$ can be obtained
at any *x*_{B} inside the medium. Because in practical situations the
field $p(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$ is only observed at a finite part
𝕊_{0} of the surface, approximations arise in practice when the
closed surface 𝕊 is replaced by 𝕊_{0}. One of the
consequences is that multiple reflections are not handled correctly. A
detailed analysis (Wapenaar et al., 1989) shows that the primary arrival of the
upgoing wave field ${p}^{-}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})={G}^{-}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})s\left(\mathit{\omega}\right)$
is reasonably accurately retrieved with the following
approximation of Eq. (22):

$$\begin{array}{}\text{(23)}& {p}^{-}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\approx \underset{{\mathbb{S}}_{\mathrm{0}}}{\int}{F}_{\mathrm{d}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){p}^{-}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}\mathit{x}.\end{array}$$

Here the back propagation operator ${F}_{\mathrm{d}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})$, also known as the focusing operator, is defined as

$$\begin{array}{}\text{(24)}& {F}_{\mathrm{d}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})={\displaystyle \frac{\mathrm{2}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}{\partial}_{\mathrm{3}}{G}_{\mathrm{d}}^{*}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}),\end{array}$$

where we used ${n}_{\mathrm{3}}=-\mathrm{1}$ at 𝕊_{0}, considering that the positive *x*_{3} axis is pointing downward.
Equations (23) and (24) represent the common approach to back propagation
for many applications in seismic imaging and inversion.
It works well for primary waves in media with low contrasts, but it breaks down when the contrasts are strong and
multiple reflections between the layer interfaces cannot be ignored.
In Sect. 3.3 we discuss a modified approach to back-propagation which enables the recovery of
the full wave field $p({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$,
including the multiple reflections, inside the medium (also below the source at *x*_{A})
and which also suppresses artefacts like those in Fig. 6b in a data-driven way.

In the previous section we discussed back propagation of
${p}^{-}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$, which is the response to a source at *x*_{A} inside the
medium, observed at ** x** at the surface. Here we extend this process for
the situation in which both the sources and receivers are located at the
surface. To this end, we first adapt Eqs. (23) and
(24). We replace 𝕊

$$\begin{array}{}\text{(25)}& {p}^{-,+}({\mathit{x}}_{\mathrm{A}},\mathit{x},\mathit{\omega})\approx \underset{{\mathbb{S}}_{\mathrm{0}}^{\prime}}{\int}{F}_{\mathrm{d}}^{+}({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega}){p}^{-,+}({\mathit{x}}^{\prime},\mathit{x},\mathit{\omega})\mathrm{d}{\mathit{x}}^{\prime},\end{array}$$

with

$$\begin{array}{}\text{(26)}& {F}_{\mathrm{d}}^{+}({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})={\displaystyle \frac{\mathrm{2}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}{\partial}_{\mathrm{3}}^{\prime}{G}_{\mathrm{d}}^{*}({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega}).\end{array}$$

Here ${\partial}_{\mathrm{3}}^{\prime}$ stands for differentiation with respect to ${x}_{\mathrm{3}}^{\prime}$. In
Eq. (25), ${p}^{-,+}({\mathit{x}}^{\prime},\mathit{x},\mathit{\omega})={G}^{-,+}({\mathit{x}}^{\prime},\mathit{x},\mathit{\omega})s\left(\mathit{\omega}\right)$ represents the reflection data at the surface.
The first superscript (−) denotes that the field is upgoing at *x*^{′};
the second superscript (+) denotes that the source at ** x** emits
downgoing waves. Furthermore, ${p}^{-,+}({\mathit{x}}_{\mathrm{A}},\mathit{x},\mathit{\omega})={G}^{-,+}({\mathit{x}}_{\mathrm{A}},\mathit{x},\mathit{\omega})s\left(\mathit{\omega}\right)$ is the back propagated upgoing field at

$$\begin{array}{}\text{(27)}& {p}^{-,+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\approx \underset{{\mathbb{S}}_{\mathrm{0}}^{\prime}}{\int}{p}^{-,+}(\mathit{x},{\mathit{x}}^{\prime},\mathit{\omega}){F}_{\mathrm{d}}^{+}({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}{\mathit{x}}^{\prime}.\end{array}$$

The receiver for upgoing waves at *x*_{A} has turned into a source for downgoing waves at *x*_{A}, and so on.
Hence, Eq. (27) back propagates the sources from *x*^{′} on ${\mathbb{S}}_{\mathrm{0}}^{\prime}$ to *x*_{A}.
Substituting this into Eq. (23),
with *p*^{−} replaced by ${p}^{-,+}$ on both sides, gives

$$\begin{array}{ll}{\displaystyle}& {\displaystyle}{p}^{-,+}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\\ \text{(28)}& {\displaystyle}& {\displaystyle}\phantom{\rule{0.25em}{0ex}}\approx \underset{{\mathbb{S}}_{\mathrm{0}}}{\int}\underset{{\mathbb{S}}_{\mathrm{0}}^{\prime}}{\int}{F}_{\mathrm{d}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){p}^{-,+}(\mathit{x},{\mathit{x}}^{\prime},\mathit{\omega}){F}_{\mathrm{d}}^{+}({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}{\mathit{x}}^{\prime}\mathrm{d}\mathit{x}.\end{array}$$

Here ${p}^{-,+}(\mathit{x},{\mathit{x}}^{\prime},\mathit{\omega})$ represents the reflection response at
the surface (illustrated by the blue arrows in Fig. 7a).
Similarly, ${p}^{-,+}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$ denotes the reflection
response to a source for downgoing waves at *x*_{A}, observed by a
receiver for upgoing waves at *x*_{B} (illustrated by the yellow arrows
in Fig. 7a). According to Eq. (28), it is
obtained by back propagating sources from *x*^{′} to *x*_{A} with
operator ${F}_{\mathrm{d}}^{+}({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$
and receivers from ** x** to

The redatumed response ${p}^{-,+}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$ can be used for
reflectivity imaging by setting *x*_{B} equal to *x*_{A} and
selecting the *t*=0 component in the time domain, as follows:

$$\begin{array}{}\text{(29)}& r\left({\mathit{x}}_{\mathrm{A}}\right)\approx {p}^{-,+}({\mathit{x}}_{\mathrm{A}},{\mathit{x}}_{\mathrm{A}},t=\mathrm{0})={\displaystyle \frac{\mathrm{1}}{\mathrm{2}\mathit{\pi}}}\underset{-\mathrm{\infty}}{\overset{\mathrm{\infty}}{\int}}{p}^{-,+}({\mathit{x}}_{\mathrm{A}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}\mathit{\omega}.\end{array}$$

The combined process (Eqs. 28 and 29)
comprises imaging by double focusing (Berkhout, 1982; Wiggins, 1984; Bleistein, 1987; Berkhout and Wapenaar, 1993; Blondel et al., 2018), because it involves
the application of the focusing operator ${F}_{\mathrm{d}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$ twice.
By taking the focal point *x*_{A} variable, a reflectivity
image of the entire region of interest is obtained. Figure 7b shows
an image of the same layered medium as considered in
previous examples obtained in this way. Note that the interfaces are clearly imaged, but also that
significant artefacts are present because multiple reflections are not
correctly handled (indicated by the red arrows). In Sect. 3.4 and
3.5 we discuss more rigorous approaches to source–receiver
redatuming and imaging by double focusing, which account for multiple
reflections in a data-driven way.

3 Theory and applications of a modified single-sided wave field representation

Back to toptop
The applications of Green's theorem, discussed in Sect. 2, are all derived from the classical homogeneous Green's function representation. This representation is exact, but it involves an integral over a closed surface. In many practical situations the medium of interest is only accessible from one side, which implies that the integration can only be carried out over an open surface. This induces approximations, of which the incomplete treatment of multiple reflections is the most significant one. In the following we discuss a modification of the homogeneous Green's function representation which involves an integral over an open surface and yet accounts for all multiple reflections. We call this modified representation the single-sided homogeneous Green's function representation. Next, we discuss how it can be used to improve several of the applications discussed in Sect. 2.

The classical homogeneous Green's function representations (Eqs. 6 and 7) are entirely formulated in terms of Green's
functions and their time reversals. A Green's function is the causal response
to a source at a specific position in space, say at *x*_{A}. A
time-reversed Green's function can be seen as a focusing function which
focuses at *x*_{A}. However, this only holds when it converges to
*x*_{A} equally from all directions, which can be achieved by emitting it into
the medium from a closed surface. For practical situations we need another
type of focusing function, which, when emitted into the medium from a single
surface, focuses at *x*_{A}. We introduce the focusing function using
Fig. 8. This figure shows a truncated version of the
medium, which is identical to the actual medium between the upper surface
𝕊_{0} and the focal plane 𝕊_{A} (the plane which
contains the focal point *x*_{A}), but it is reflection free above
𝕊_{0} and below 𝕊_{A} (here “reflection free” means
that the medium parameters do not vary in the vertical direction). We call
the focusing function ${f}_{\mathrm{1}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$. In the reflection-free
half-space above 𝕊_{0} the focusing function consists of both a
downgoing and upgoing part, according to

$$\begin{array}{}\text{(30)}& {f}_{\mathrm{1}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)={f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)+{f}_{\mathrm{1}}^{-}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t),\end{array}$$

where the superscripts + and − indicate downgoing and upgoing,
respectively. The downgoing part ${f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$ is shaped such
that ${f}_{\mathrm{1}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$ focuses at *x*_{A} at *t*=0, and
continues as a diverging downgoing field into the reflection-free half-space
below 𝕊_{A}. The upgoing part of the focusing function in the
upper half-space, ${f}_{\mathrm{1}}^{-}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$, is defined as the reflection
response of the truncated medium to the downgoing focusing function
${f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$. The focusing property at the focal plane
𝕊_{A} can be formulated as

$$\begin{array}{}\text{(31)}& \mathit{\delta}({\mathit{x}}_{\mathrm{H},\mathrm{A}}^{\prime}-{\mathit{x}}_{\mathrm{H},\mathrm{A}})\mathit{\delta}\left(t\right)=\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}\mathcal{T}({\mathit{x}}_{\mathrm{A}}^{\prime},\mathit{x},t)*{f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)\mathrm{d}\mathit{x},\end{array}$$

where $\mathcal{T}({\mathit{x}}_{\mathrm{A}}^{\prime},\mathit{x},t)$ is the transmission response of the
truncated medium between 𝕊_{0} and 𝕊_{A}, and
*x*_{H,A} and ${\mathit{x}}_{\mathrm{H},\mathrm{A}}^{\prime}$ are the horizontal
coordinates of *x*_{A} and ${\mathit{x}}_{\mathrm{A}}^{\prime}$ (both at 𝕊_{A}), respectively
(the precise definition of $\mathcal{T}({\mathit{x}}_{\mathrm{A}}^{\prime},\mathit{x},t)$ is given in
Appendix A of Wapenaar et al., 2014a). In physical terms, Eq. (31)
formulates the emission of ${f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$ from
𝕊_{0} into the truncated medium, leading to a focus at *x*_{A}.
In mathematical terms, Eq. (31) defines
${f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$ as the inverse of the transmission response
$\mathcal{T}({\mathit{x}}_{\mathrm{A}}^{\prime},\mathit{x},t)$. Because the evanescent part of the
transmission response cannot be inverted in a stable way, in practice the
focusing function, and hence the focus at 𝕊_{A}, is band-limited.

The focusing function is illustrated using a numerical example in Fig. 9.
Figure 9a shows how the downgoing part of the focusing function,
${f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$, is emitted from ** x** at 𝕊

Given the focusing function for a focal point at *x*_{A} and the Green's
function for a source at *x*_{B}, the single-sided representation of the
homogeneous Green's function in the frequency domain reads
(Wapenaar et al., 2016a)

$$\begin{array}{ll}{\displaystyle}{G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})& {\displaystyle}=\mathrm{2}\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}{\displaystyle \frac{\mathrm{1}}{\mathit{\omega}\mathit{\rho}\left(\mathit{x}\right)}}\left(\mathit{\right\{}{\partial}_{i}{G}_{\mathrm{h}}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})\mathit{\left\}}\mathrm{\Im}\mathit{\right\{}{f}_{\mathrm{1}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathit{\}}\\ \text{(32)}& {\displaystyle}& {\displaystyle}-{G}_{\mathrm{h}}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})\mathrm{\Im}\mathit{\left\{}{\partial}_{i}{f}_{\mathrm{1}}\right(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega}\left)\mathit{\right\}}){n}_{i}\mathrm{d}\mathit{x},\end{array}$$

where ℑ denotes the imaginary part. The derivation can be found in the
Supplement, Sect. S2.2 (a similar single-sided representation
for vectorial wave fields is derived by Wapenaar et al., 2016b, and illustrated
using numerical examples by Reinicke and Wapenaar, 2019). In Eq. (32), 𝕊_{0} may be a curved surface. Moreover, the
actual medium, in which the Green's function is defined, may be inhomogeneous
above 𝕊_{0} (in addition to being inhomogeneous below
𝕊_{0}). Note the resemblance with the classical representation of
Eq. (6). Unlike the classical representation, which is exact,
Eq. (32) holds under the assumption that evanescent waves can
be neglected. When 𝕊_{0} is horizontal and the medium above
𝕊_{0} is homogeneous (for the Green's function as well as for the
focusing function), this representation may be approximated by

$$\begin{array}{ll}{\displaystyle}{G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})& {\displaystyle}=\mathrm{4}\mathrm{\Re}\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}{\displaystyle \frac{\mathrm{1}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}G(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){\partial}_{\mathrm{3}}\left({f}_{\mathrm{1}}^{+}\right(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\\ \text{(33)}& {\displaystyle}& {\displaystyle}-\mathit{\left\{}{f}_{\mathrm{1}}^{-}\right(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega}\left){\mathit{\}}}^{*}\right)\mathrm{d}\mathit{x}\end{array}$$

(Van der Neut et al., 2017). For the derivation, see the Supplement, Sect. S2.3. For the decomposed Green's function ${G}^{-,+}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$, introduced in Sect. 2.5, we have the following representation (by combining Eqs. S31 and S38 of the Supplement)

$$\begin{array}{ll}{\displaystyle}{G}^{-,+}& {\displaystyle}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\\ {\displaystyle}& {\displaystyle}=\mathrm{2}\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}{\displaystyle \frac{\mathrm{1}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}{G}^{-,+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){\partial}_{\mathrm{3}}{f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}\mathit{x}\\ \text{(34)}& {\displaystyle}& {\displaystyle}-\mathit{\chi}\left({\mathit{x}}_{\mathrm{B}}\right){f}_{\mathrm{1}}^{-}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega}),\end{array}$$

where *χ* is the characteristic function of the medium enclosed by 𝕊_{0} and 𝕊_{A}. It is defined as

$$\begin{array}{}\text{(35)}& \mathit{\chi}\left({\mathit{x}}_{\mathrm{B}}\right)=\left\{\begin{array}{ll}\mathrm{1},& \text{for}{\mathit{x}}_{\mathrm{B}}\text{between}{\mathbb{S}}_{\mathrm{0}}\text{and}{\mathbb{S}}_{\mathrm{A}},\\ {\displaystyle \frac{\mathrm{1}}{\mathrm{2}}},& \text{for}{\mathit{x}}_{\mathrm{B}}\text{on}\mathbb{S}={\mathbb{S}}_{\mathrm{0}}\cup {\mathbb{S}}_{\mathrm{A}},\\ \mathrm{0},& \text{for}{\mathit{x}}_{\mathrm{B}}\text{outside}\mathbb{S}.\end{array}\right.\end{array}$$

In many practical situations 𝕊_{0} is a free surface, which means
that the assumption of a homogeneous medium above 𝕊_{0} is not
fulfilled. A free surface gives rise to surface-related multiple reflections.
These can be removed by a process called surface-related multiple elimination
(Verschuur et al., 1992). Applying this process is equivalent to replacing
the free surface with a transparent surface and a homogeneous half-space above
this surface (Fokkema and van den Berg, 1993; van Borselen et al., 1996). Hence, when
𝕊_{0} is a free surface, Eqs. (33) and
(34) hold for the situation after surface-related multiple
elimination.

The representations of Eqs. (33) and (34) form the
starting point for modifying several of the applications discussed in Sect. 2.
These methods, which will be discussed in the subsequent
sections, have the fact in common that they make use of focusing functions. As stated
earlier, the focusing function ${f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$ for ** x** at
𝕊

We discuss a modification of time-reversal acoustics. Assuming the focusing
functions are available for ** x** at 𝕊

$$\begin{array}{ll}{\displaystyle}& {\displaystyle}{\widehat{v}}_{\mathrm{n}}^{*}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\\ \text{(36)}& {\displaystyle}& {\displaystyle}\phantom{\rule{0.25em}{0ex}}={\displaystyle \frac{\mathrm{1}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}{\partial}_{\mathrm{3}}\left({f}_{\mathrm{1}}^{+}\right(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})-\mathit{\{}{f}_{\mathrm{1}}^{-}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega}){\mathit{\}}}^{*}\left)s\right(\mathit{\omega}),\end{array}$$

where for *s*(*ω*) we take a real-valued spectrum.
Using this in Eq. (33) we obtain

$$\begin{array}{}\text{(37)}& {G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})s\left(\mathit{\omega}\right)=\mathrm{4}\mathrm{\Re}\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}G({\mathit{x}}_{\mathrm{B}},\mathit{x},\mathit{\omega}){\widehat{v}}_{\mathrm{n}}^{*}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}\mathit{x}.\end{array}$$

In the time domain this becomes

$$\begin{array}{ll}{\displaystyle}{G}_{\mathrm{h}}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},t)*s\left(t\right)& {\displaystyle}=\mathrm{2}\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}G({\mathit{x}}_{\mathrm{B}},\mathit{x},t)*{\widehat{v}}_{\mathrm{n}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},-t)\mathrm{d}\mathit{x}\\ \text{(38)}& {\displaystyle}& {\displaystyle}+\mathrm{2}\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}G({\mathit{x}}_{\mathrm{B}},\mathit{x},-t)*{\widehat{v}}_{\mathrm{n}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)\mathrm{d}\mathit{x}.\end{array}$$

The first integral is the same as that in Eq. (10) (except that
${\widehat{v}}_{\mathrm{n}}$ is defined differently), whereas the second integral is the
time reversal of the first one. For ultrasonic applications, assuming there
are receivers at one or more *x*_{B} locations, the field
${\widehat{v}}_{\mathrm{n}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},-t)$ can be emitted physically into the real medium and
its response can be measured at *x*_{B}. The homogeneous Green's function
is then obtained by superposing this response and its time reversal. For
geophysical applications, the first integral can, at least in theory, be
evaluated by numerically emitting the field ${\widehat{v}}_{\mathrm{n}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},-t)$ into a model of the Earth. The superposition of this integral and
its time-reversal gives the homogeneous Green's function. Following either
one of these procedures, the result obtained at *t*=0 is shown in Fig. 10b.
For comparison, Fig. 10a once more shows the classical
time-reversal result of Fig. 3b. Note the different character of
the fields *v*_{n} and ${\widehat{v}}_{\mathrm{n}}$ in the upper panels, which only have
one event in common i.e., the time-reversed direct arrival. The
snapshots at *t*=0 in the lower panels are also very different: the artefacts
in Fig. 10a are almost entirely absent in Fig. 10b. The
latter figure only shows a clear focus at *x*_{A}.

Obtaining an accurate focus as in Fig. 10b by numerically emitting
the field ${\widehat{v}}_{\mathrm{n}}(\mathit{x},{\mathit{x}}_{\mathrm{A}},-t)$ into the Earth requires a
very accurate model of the Earth, which should include accurate information
on the position, structure and contrast of the layer interfaces. This
requirement can be overcome by also retrieving the Green's function $G({\mathit{x}}_{\mathrm{B}},\mathit{x},t)$
in Eq. (38) using the Marchenko method and
evaluating the integrals for all *x*_{B}. This is not discussed any further
here. Alternative methods that do not require information about the layer
interfaces are discussed in Sect. 3.3 to 3.5 and are
illustrated using examples.

We modify the approach for back propagation.
By interchanging *x*_{A} and *x*_{B} in Eq. (33)
and multiplying both sides with a real-valued source spectrum *s*(*ω*), we obtain

$$\begin{array}{ll}{\displaystyle}p({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})& {\displaystyle}+{p}^{*}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\\ \text{(39)}& {\displaystyle}& {\displaystyle}=\mathrm{2}\mathrm{\Re}\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}F(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})p(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}\mathit{x},\end{array}$$

with $p(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})=G(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})s\left(\mathit{\omega}\right)$ and

$$\begin{array}{}\text{(40)}& F(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})={\displaystyle \frac{\mathrm{2}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}{\partial}_{\mathrm{3}}\left({f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})-\mathit{\left\{}{f}_{\mathrm{1}}^{-}\right(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){\mathit{\}}}^{*}\right).\end{array}$$

Note that the operator ${F}_{\mathrm{d}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})$ in Eq. (24)
is an approximation of the operator $F(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})$ in Eq. (40). It is obtained by omitting the term
$\mathit{\left\{}{f}_{\mathrm{1}}^{-}\right(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){\mathit{\}}}^{*}$ and replacing the term ${f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})$ by its initial estimate, i.e., the Fourier transform of
the direct arrival of the Green's function, ${G}_{\mathrm{d}}(\mathit{x},{\mathit{x}}_{\mathrm{B}},-t)$. Figure 11 illustrates, in the time domain, the principle
of modified back propagation. In Fig. 11a, the field $p(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$
is back propagated to an arbitrary point *x*_{B} inside
the medium by operator $F(\mathit{x},{\mathit{x}}_{\mathrm{B}},t)$. This operator can be
obtained from reflection data at the surface and the initial estimate ${G}_{\mathrm{d}}(\mathit{x},{\mathit{x}}_{\mathrm{B}},-t)$, using the Marchenko method. Figure 11b
shows $F(\mathit{x},{\mathit{x}}_{\mathrm{B}},t)$ (for fixed *x*_{B}) and a snapshot of the
back propagated field at a time instant *t*_{1}>0 for all *x*_{B}. Note
that the full field $p({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},t)$ is retrieved (downgoing and
upgoing components, primaries and multiples) and that hardly any artefacts
are visible. The dashed lines in the snapshot in Fig. 11b indicate
the interfaces to aid with the interpretation of the snapshot. Note, however, that
these interfaces need not be known to obtain this result: only a smooth
subsurface model is required to define the initial estimate ${G}_{\mathrm{d}}(\mathit{x},{\mathit{x}}_{\mathrm{B}},-t)$ of the focusing operator. All other events in the focusing
operator come directly from the reflection data at the surface.

This back propagation method has an interesting application in the monitoring of induced
seismicity. Assuming $p(\mathit{x},{\mathit{x}}_{\mathrm{A}},t)$ stands for the response to an
induced seismic source at *x*_{A},
this method creates, in a data-driven way, omnidirectional virtual receivers at any *x*_{B} to monitor the emitted field from the source to the surface.
This application is extensively discussed in the companion paper (Brackenhoff et al., 2019).

We modify the approach for source–receiver redatuming. First, in Eq. (39), we replace 𝕊_{0} with ${\mathbb{S}}_{\mathrm{0}}^{\prime}$ (just
above 𝕊_{0}), ** x** with ${\mathit{x}}^{\prime}\in {\mathbb{S}}_{\mathrm{0}}^{\prime}$,

$$\begin{array}{ll}{\displaystyle}p(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})& {\displaystyle}+{p}^{*}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\\ \text{(41)}& {\displaystyle}& {\displaystyle}=\mathrm{2}\mathrm{\Re}\underset{{\mathbb{S}}_{\mathrm{0}}^{\prime}}{\int}p(\mathit{x},{\mathit{x}}^{\prime},\mathit{\omega})F({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}{\mathit{x}}^{\prime};\end{array}$$

$F({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$ is defined as in Eq. (40), with
∂_{3} replaced by ${\partial}_{\mathrm{3}}^{\prime}$, similar to Eq. (26).
The field $p(\mathit{x},{\mathit{x}}^{\prime},\mathit{\omega})=G(\mathit{x},{\mathit{x}}^{\prime},\mathit{\omega})s\left(\mathit{\omega}\right)$ represents the data at the surface. Equation (41)
back propagates the sources from *x*^{′} on
${\mathbb{S}}_{\mathrm{0}}^{\prime}$ to *x*_{A}. Source–receiver redatuming is now defined
as the following two-step process. In step one, apply Eq. (41) to create an omnidirectional virtual source at any desired
position *x*_{A} in the subsurface. According to the left-hand side, the
response to this virtual source is observed by actual receivers at ** x**
at the surface. Isolate $p(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$ from the left-hand side
by applying a time window (a simple Heaviside function) in the time domain.
In step two, substitute the retrieved response $p(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$
into Eq. (39) to create virtual receivers at any position

If we applied imaging to the retrieved response $p({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})+{p}^{*}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$ in a similar fashion to
Eq. (29), we would obtain an image of the virtual sources
instead of the reflectivity. Similar to Sect. 2.5 we need a
process to obtain the decomposed response ${p}^{-,+}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$.
Our starting point is Eq. (34), in which we
interchange *x*_{A} and *x*_{B} and choose both of these points at
𝕊_{A}, such that ${f}_{\mathrm{1}}^{-}({\mathit{x}}_{\mathrm{A}},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})=\mathrm{0}$. Applying
source–receiver reciprocity on the left-hand side and multiplying both sides
by a source spectrum *s*(*ω*), we obtain

$$\begin{array}{}\text{(42)}& {p}^{-,+}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})=\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}{F}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){p}^{-,+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}\mathit{x},\end{array}$$

with ${p}^{-,+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})={G}^{-,+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})s\left(\mathit{\omega}\right)$ and

$$\begin{array}{}\text{(43)}& {F}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega})={\displaystyle \frac{\mathrm{2}}{i\mathit{\omega}{\mathit{\rho}}_{\mathrm{0}}}}{\partial}_{\mathrm{3}}{f}_{\mathrm{1}}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}).\end{array}$$

Next, in Eq. (34), replace 𝕊_{0} with ${\mathbb{S}}_{\mathrm{0}}^{\prime}$
(just above 𝕊_{0}), ** x** with ${\mathit{x}}^{\prime}\in {\mathbb{S}}_{\mathrm{0}}^{\prime}$ and

$$\begin{array}{ll}{\displaystyle}{p}^{-,+}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})& {\displaystyle}=\underset{{\mathbb{S}}_{\mathrm{0}}^{\prime}}{\int}{p}^{-,+}(\mathit{x},{\mathit{x}}^{\prime},\mathit{\omega}){F}^{+}({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}{\mathit{x}}^{\prime}\\ \text{(44)}& {\displaystyle}& {\displaystyle}-{f}_{\mathrm{1}}^{-}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})s\left(\mathit{\omega}\right);\end{array}$$

${F}^{+}({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$ is defined as in Eq. (43),
with ∂_{3} replaced by ${\partial}_{\mathrm{3}}^{\prime}$, similar to Eq. (26).
Substitution of Eq. (44) into Eq. (42) yields

$$\begin{array}{ll}{\displaystyle}& {\displaystyle}{p}^{-,+}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})+\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}{F}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){f}_{\mathrm{1}}^{-}(\mathit{x},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})s\left(\mathit{\omega}\right)\mathrm{d}\mathit{x}\\ \text{(45)}& {\displaystyle}& {\displaystyle}\phantom{\rule{0.25em}{0ex}}=\underset{{\mathbb{S}}_{\mathrm{0}}}{\int}\underset{{\mathbb{S}}_{\mathrm{0}}^{\prime}}{\int}{F}^{+}(\mathit{x},{\mathit{x}}_{\mathrm{B}},\mathit{\omega}){p}^{-,+}(\mathit{x},{\mathit{x}}^{\prime},\mathit{\omega}){F}^{+}({\mathit{x}}^{\prime},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})\mathrm{d}{\mathit{x}}^{\prime}\mathrm{d}\mathit{x}.\end{array}$$

This is the modified version of Eq. (28), with the operators
${F}_{\mathrm{d}}^{+}$, which account for primaries only, replaced by the operators
*F*^{+}, which account for both primaries and multiples. These operators can be
obtained using the Marchenko method from the reflection data ${p}^{-,+}(\mathit{x},{\mathit{x}}^{\prime},\mathit{\omega})$ and a smooth model of the medium to define the initial
estimate of ${f}_{\mathrm{1}}^{+}$. The second term on the left-hand side can be removed by
a time-window in the time domain, which leaves the redatumed reflection
response ${p}^{-,+}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$. The reflectivity imaging step
to retrieve *r*(*x*_{A})
is the same as that in Eq. (29) and is
not repeated here. Figure 13b shows an image obtained by applying Eqs. (45)
and (29) for all *x*_{A} in the region of interest,
for the same medium that was imaged using the classical double-focusing method (which for ease of comparison is repeated in Fig. 13a).
Note that the artefacts caused by the internal multiple reflections (indicated by the red arrows in Fig. 13a), have almost entirely been removed.
In practical situations the modified method may suffer from imperfections in the data, such as incomplete sampling, anelastic losses, out-of-plane
reflections and 3-D spreading effects. Several of these imperfections can be accounted for by making the method adaptive (van der Neut et al., 2014).
Promising results have been obtained using real data (Ravasi et al., 2016; Staring et al., 2018).

Other methods exist that deal with internal multiple reflections in imaging. Davydenko and Verschuur (2017) discuss a method called full wave field migration.
This is a recursive method, starting at the surface, which alternately resolves layer interfaces and predicts the multiples related to these interfaces.
In contrast, Eq. (45) is non-recursive. The field ${p}^{-,+}({\mathit{x}}_{\mathrm{B}},{\mathit{x}}_{\mathrm{A}},\mathit{\omega})$ at 𝕊_{A} is obtained without needing
information about the layer interfaces between 𝕊_{0} and 𝕊_{A}; a smooth model suffices.
Following the work of Weglein et al. (1997, 2011) on an inverse-scattering series approach to multiple elimination,
Ten Kroode (2002) proposes a method that attenuates the internal multiples directly in the
reflection data at the surface, without requiring model information.
This method resembles a multiple prediction and removal method proposed by Jakubowicz (1998).
These methods address all orders of internal multiples, but only with approximate amplitudes.
Variants of the Marchenko method have been developed that aim to eliminate the internal multiples from the reflection data at the surface
(Meles et al., 2015; van der Neut and Wapenaar, 2016; Zhang et al., 2019).
The last reference shows that all orders of multiples are, at least in theory, predicted with the correct amplitudes without needing model information.
Once the internal multiples have been successfully eliminated from the reflection data at the surface, standard redatuming and imaging (for example as described in
Sect. 2.5) can be used to form an accurate image of the subsurface, without artefacts caused by multiple reflections.

4 Conclusions

Back to toptop
The classical homogeneous Green's function representation, originally developed for optical image formation by holograms, expresses the Green's function plus its time-reversal between two arbitrary points in terms of an integral along a surface enclosing these points. It forms a unified basis for a variety of seismic imaging methods, such as time-reversal acoustics, seismic interferometry, back propagation, source–receiver redatuming and imaging by double focusing. We have derived each of these methods by applying some simple manipulations to the classical homogeneous Green's function representation, which implies that these methods are all very similar. As a consequence, they share the same advantages and limitations. Because the underlying representation is exact, it accounts for all orders of multiple scattering. This property is exploited by seismic interferometry in a layered medium below a free surface and, to some extent, by time-reversal acoustics in a medium with random scatterers. However, in most cases multiple scattering is not correctly handled because in practical situations data are not available on a closed surface. We also discussed a single-sided homogeneous Green's function representation, which requires access to the medium from one side only, say from the Earth's surface. This single-sided representation ignores evanescent waves, but it accounts for all orders of multiple scattering, similar as the classical closed-surface representation. We used the single-sided representation as the basis for deriving modifications of time-reversal acoustics, back propagation, source–receiver redatuming and imaging by double focusing. These methods account for multiple scattering and can be used to obtain accurate images of the source or the subsurface, without artefacts related to multiple scattering. Another interesting application is the monitoring and forecasting of responses to induced seismic sources, which is discussed in detail in a companion paper.

Code availability

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Code availability.

The modeling and imaging software that was used to generate the numerical examples in this paper can be downloaded from https://github.com/JanThorbecke/OpenSource (last access: 1 April 2019).

Supplement

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Supplement.

The supplement related to this article is available online at: https://doi.org/10.5194/se-10-517-2019-supplement.

Author contributions

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Author contributions.

JB and JT developed the software and generated the numerical examples. KW wrote the paper. All authors reviewed the manuscript.

Competing interests

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Competing interests.

The authors declare that they have no conflict of interest.

Special issue statement

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Special issue statement.

This article is part of the special issue “Advances in seismic imaging across the scales”. It is a result of the EGU General Assembly 2018, Vienna, Austria, 8–13 April 2018.

Acknowledgements

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Acknowledgements.

We thank the two reviewers, Andreas Fichtner and Robert Nowack, for their valuable feedback, which helped us to improve the paper. This work has received funding from the European Union's Horizon 2020 research and innovation programme: European Research Council (grant agreement no. 742703).

Review statement

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Review statement.

This paper was edited by Nicholas Rawlinson and reviewed by Andreas Fichtner and Robert Nowack.

References

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Special issue

Short summary

The earthquake seismology and seismic exploration communities have developed a variety of seismic imaging methods for passive- and active-source data. Despite the seemingly different approaches and underlying principles, many of these methods are based in some way or another on the same mathematical theorem. Starting with this theorem, we discuss a variety of classical and recent seismic imaging methods in a systematic way and explain their similarities and differences.

The earthquake seismology and seismic exploration communities have developed a variety of...

Solid Earth

An interactive open-access journal of the European Geosciences Union