1 Array Methods for Image Formation Outline 1.Fine scale heterogeneity in the mantle 2.CCP stacking versus scattered wave imaging 3.Scattered wave imaging systems 4.Born Scattering = Single scattering 5.Diffraction & Kirchhoff Depth Migration 6.Limitations 7.Examples 8.Tutorial: I use Matlab R2007b
2 Summary Data redundancy suppresses noise. Noise is whatever doesn’t fit the scattering model. The image is only as good as the 1.The velocity model 2.The completeness of the dataset 3.The assumptions the imaging system is based on. 1.We use a single-scattering assumption
3 SNORCLE Subduction forming the Proterozoic continental mantle lithosphere: Lateral advection of mass Cook et al., (1999) Bostock (1998)
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6 Geometry: Fine scales in the mantle Allegre and Turcotte, 1986Kellogg and Turcotte, 1994
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8 Coherent Subduction SUMA: Statistical Upper Mantle Assemblage Reservoirs are distributed
9 Structures from basalt extraction Oman ophiolite
10 Regional Seismology: PNE Data Highly heterogeneous models of the CL Nielsen et al, 2003, GJI
11 Two classes of scattered wave imaging systems 1.Incoherent imaging systems which are frequency and amplitude sensitive. Examples are 1.Photography 2.Military Sonar 3.Some deep crustal reflection seismology 2.Coherent imaging systems use phase coherence and are therefore sensitive to frequency, amplitude, and phase. Examples are 1.Medical ultrasound imaging 2.Military sonar 3.Exploration seismology 4.Receiver function imaging 5.Scattered wave imaging in teleseismic studies 3.Mixed systems 1.Sumatra earthquake source by Ishii et al See Blackledge, 1989, Quantitative Coherent Imaging: Theory and Applications
12 Direct imaging with seismic waves Images based on this model of 1 D scattering are referred to as common conversion point stacks or CCP images Converted Wave Imaging from a continuous, specular, interface From Niu and James, 2002, EPSL
13 CCP Stacking blurs the subsurface The lateral focus is weak
14 Fresnel Zones and other measures of wave sampling Fresnel zones Banana donuts Wavepaths Are all about the same thing They are means to estimate the sampling volume for waves of finite- frequency, i.e. not a ray, but a wave. Flatté et al., Sound Transmission Through a Fluctuating Ocean
15 Moho
16 Moho 410
17 Moho 1p2s 2p1s 1p2s Moho T 0 =3s 1. Lateral heterogeneity is blurred 2. Mispositioning in depth from average V(z) profile 3. Pulses broaden due to increase in V with z 4. Crustal multiples obscure upper mantle 5. Diffractions stacked out VE=1:1
18 Scattered wave imaging Based on diffraction theory: Every point in the subsurface causes scattering
19 Scattered wave imaging improves lateral resolution It also restores dips
20 USArray: Bigfoot x = 70 km, 7s < T < 30s
21 S. Ham, unpublished Slab Multiples Slab Multiples Mismatch
22 Resolution Considerations Earthquakes are the only inexpensive energy source able to investigate the mantle Coherent Scattered Wave Imaging provides about an order of magnitude better resolution than travel time tomography. For wavelength R scat ~ /2 versus R tomo ~ ( L) 1/2 For a normalized wavelength and path of 100 R scat ~ 0.5 versus R tomo ~ 10 The tomography model provides a smooth background for scattered wave imaging
23 The receiver function: –Approximately isolates the SV wave from the P wave –Reduces a vector system to a scalar system –Allows use of a scalar imaging equation with P and S calculated separately for single scattering: From Barbara’s lecture:
24 Three elements of an imaging algorithm 1.A scattering model 2.Wave (de)propagator Diffraction integrals (Wilson et al., 2005) Kirchhoff Integrals (Bostock, 2002; Levander et al., 2005) One-way and two-way finite-difference operators (Stanford SEP) Generalized Radon Transforms (Bostock et al., 2001) Fourier transforms in space and/or time with phase shifting (Stolt, 1977, Geophysics) 3.A focusing criteria known as an imaging condition
25 Depropagator: assume smooth coefficients i.e., c(x,y,z) varies smoothly. Let L be the wave equation Operator for the smooth medium The Green’s function is the inverse operator to the wave equation For a general source:
26 The Born Approximation Perturbing the velocity field perturbs the wavefield c= c+ c -> L contains c
27 Born Scattering Perturb the velocity field Assume a constant density scalar wave equation with a smoothly varying velocity field c(x)
28 Born Scattering: Solve for the perturbed field to first order The total field consists of two parts, the response to the smooth medium Plus the response to the perturbed medium U The approximate solution satisfies two inhomogenous wave equations. Note that energy is not conserved. It is the scattered field that we use for imaging, noise is anything that doesn’t fit the scattering model
29 The scattering function for P to S conversion from a heterogeneity Wu and Aki, 1985, Geophysics where Shear wave impedance Fourier Transform relations
30 Regional Seismology: PNE Data Highly heterogeneous models of the CL Nielsen et al, 2003, GJI Background model is very smooth U senses the smooth field U senses the rough field
31 Signal Detection: Elastic P to S Scattering from a discrete heterogeneity Wu and Aki, 1985, Geophysics Specular P to S Conversion Aki and Richards, 1980 Levander et al., 2006, Tectonophysics
32 Definition of an image, from Scales (1995), Seismic Imaging Recall from the RF lecture the definition of a receiver function
33 A specific depropagator: Diffraction Integrals Start with two scalar wave equations, one homogeneous: and the other the equation for the Green ’ s function: the response to a singularity in space and time:
34 Fourier Transform with respect to time giving two Helmholtz equations where k = /c
35 Apply Green ’ s Theorem, a form of representation theorem:
36 Given measurements or estimates of two fields U and G, and their normal derivatives on a closed surface S defined by r 0, we can predict the value of the field U anywhere within the volume, r s. The integral has been widely used in diffraction theory and forms the basis of a class of seismic migration operators. Use the definition of the 3D delta function to sift U(r s, )
37 We need a Green ’ s function The free space asymptotic Green ’ s function for variable velocity can be written as The constant velocity free space Green’s function is given by
38 Here (r,r s ) is the solution to the eikonal equation: And A(r,r s ) is the solution to the transport equation: The solution is referred to as a high-frequency or asymptotic solution. Both equations are solved numerically
39 We want a Green ’ s function that vanishes on S o, or one whose derivative vanishes on S o Recenter the coordinate system so that z=0 lies in S A Green ’ s function which vanishes at z=0 is given by: Where r ’ s is the image around x of r s. At z=0 This is also approximately true if S o has topography with wavelength long compared to the incident field. This is called Kirchhoff’s approximation.
40 The diffraction integral becomes Assume that the phase fluctuations are greater than the amplitude fluctuations we can throw away the first term. This is a far field approximation: This is the Rayleigh-Sommerfeld diffraction integral (Sommerfeld, 1932, Optics) If we use it to backward propagate the wavefield, rather than forward propagate it, it is an imaging integral.
41 Imaging Condition The imaging condition is given by the time it took the source to arrive at the scatterer plus the time it took the scattered waves to arrive at the receiver. If we have an accurate description of c( r) then the waves are focused at the scattering point. (attributed to Jon Claerbout) The image is as good as the velocity model. For an incident P-wave and a scattered S-wave, and an observation at r o, then the image would focus at point r, when
42 Because the phase is zero at the imaging point, the inverse Fourier transform becomes a frequency sum Recall that U is a receiver function and the desired image is Define
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44 S (x,z) P (x,z)
45 Sensitivities Spatial aliasing and Aperture –First Fresnel zone has to be well sampled in a Fourier sense –Generally 2L > z target We need lots of receivers Ex: =3.6, f=0.5, 45 deg x = 5 km L~1000 km 400 stations
46 Data redundancy –Redundancy builds Signal/(Random Noise) as N 0.5, where N is the number of data contributing at a given image point: N=N event *N receiver –Events from different incidence angles, i.e. source distances, suppresses reverberations –Events from different incidence angles reconstruct a larger angular spectrum of the target
47 Other considerations 1.A good starting velocity model is required –Use the travel-time tomography model 2.Data preconditioning –DC removal –Frequency filter –Remove the direct wave and other signals that don’t fit the scattering model –Wavenumber filters (ouch!)
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49 Vp~ 7.75 km/s 1% Partial Melt
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51 Jemez Lineament: Mazatzal-Yavapai Boundary Jemez Lineament: Mazatzal-Yavapai Zone of melt production
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54 Structures from basalt extraction Oman ophiolite
55 RISTRA Receiver Functions DeepProbe
56 Example: Kaapvaal Craton x ~ 35 km A L ~ 20 o 9 Eqs
57 Levander et al., 2005, AGU Monograph
58 RF from Niu et al., 2004, EPSL
59 Bostock et al., 2001, 2002 Generalized Radon Transform
60 Alaska Subduction Zone dV p /V o (Pp d p)dV s /V o (P d s, Pp d s, Ps d s) dV/V 0 (%) Rondenay et al., 2008
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66 CMB Imaging using ScS precursors and the Generalized Radon Transform Wang et al., 2006 Ma et al., 2008
67 D’’ Wang et al., 2006; Ma et al, 2008
68 Summary Data redundancy suppresses noise. Noise is whatever doesn’t fit the scattering model. The image is only as good as the 1.The velocity model 2.The completeness of the dataset 3.The assumptions the imaging system is based on. 4.We use a single-scattering assumption