Prestack depth migration and illumination maps - OnePetro
Prestack depth migration and illumination maps - OnePetro
Prestack depth migration and illumination maps - OnePetro
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PreStack Depth Migration <strong>and</strong> <strong>illumination</strong> <strong>maps</strong><br />
Renaud Laurain*, <strong>and</strong> Vetle Vinje, NORSAR.<br />
Summary<br />
Designing a survey is often based on fold <strong>and</strong> offset distribution<br />
under the assumption of a flat subsurface geometry. In real<br />
situations, this is hardly the case. Recently, ray tracing has frequently<br />
been used to predict the <strong>illumination</strong> at selected<br />
reflectors corresponding to given seismic surveys. Illumination<br />
<strong>maps</strong> are used as an aid to choose the best possible survey<br />
when planning a seismic acquisition. In this 2-D synthetic<br />
study we compare hit density <strong>and</strong> <strong>illumination</strong> amplitude <strong>maps</strong><br />
from ray tracing with the result from prestack <strong>depth</strong> <strong>migration</strong><br />
(PSDM). We show that (i) holes (i.e. non-illuminated zones) in<br />
the ray-tracing based <strong>illumination</strong> <strong>maps</strong> correspond well with<br />
holes in the PSDM images <strong>and</strong> (ii) <strong>illumination</strong> amplitude<br />
<strong>maps</strong> only crudely approximate the amplitudes in the PSDM<br />
images.<br />
Introduction<br />
When designing a seismic acquisition, it has become common<br />
practice to model a hypothetical reflection data set using ray<br />
tracing in order to plan the survey geometry (i.e. source <strong>and</strong><br />
receiver positions) to obtain an optimum image of the subsurface<br />
(Bear et. al., 1999, Sassolas et. al., 1999, Pereyra et. al.,<br />
1999, Rosl<strong>and</strong> <strong>and</strong> Drivenes, 2000). For a given survey in a<br />
given model, ray tracing may be used to estimate the subsurface<br />
<strong>illumination</strong> at selected horizons in terms of e.g. hit density<br />
<strong>and</strong> amplitude distribution.<br />
On a model designed to combine the effects of both a syncline<br />
with a steep flank <strong>and</strong> a lens (e.g. a salt body), a full finite difference<br />
data set has been generated <strong>and</strong> migrated using a<br />
PSDM algorithm. Then, the correspondence between PSDM<br />
Root Mean Square amplitude (RMS amplitude) profiles along<br />
the target horizon <strong>and</strong> hit density <strong>and</strong> amplitude <strong>illumination</strong><br />
<strong>maps</strong> are studied.<br />
Model<br />
Figure 1 displays the model we used to generate a synthetic<br />
marine data set with classic 2-D finite-difference (FD) code.<br />
The upper layer represents water (velocity 1.5 km/s). The sediment<br />
layer, delimited by the sea bottom <strong>and</strong> the target horizon,<br />
is affected by a vertical gradient function (from 2.0 to 3.0<br />
km/s at the deepest point). The target geometry is chosen so<br />
that the steepest part of the syncline can not be illuminated<br />
properly except by using a recording time longer than 5.0 s. In<br />
the sediment layer, a salt lens with constant velocity of 4.0 km/<br />
s has been introduced to study the effects of shadow zones<br />
induced on the target horizon.<br />
Depth (km)<br />
Distance (km)<br />
0.0 2.0 4.0 6.0 8.0 10.0 12.0 14.0<br />
P-velocity (km/s)<br />
1.5 2.0 2.5 3.0 3.5 4.0<br />
Fig.1: Model used for generating synthetic data. Shots are<br />
plotted as red triangles at the surface. Target horizon is plotted<br />
in red.<br />
The data acquisition scheme is designed as a marine survey<br />
with a nominal fold of 10 in bin cells of 5 m size. Shots are<br />
located on the surface, every 50 m between 3.0 <strong>and</strong> 14.5 km.<br />
For each shot, 100 receivers with offsets from 10 m to 1000 m<br />
<strong>and</strong> a 10.0 m interval are used (figure 1). An example of constant-offset<br />
FD section is given in figure 2.<br />
sea bottom<br />
top salt<br />
bottom salt<br />
Target Horizon<br />
Fig.2: Constant-offset section for offset 10.0 m.<br />
target horizon<br />
SEG Int'l Exposition <strong>and</strong> Annual Meeting * San Antonio, Texas * September 9-14, 2001<br />
0.0<br />
1.0<br />
2.0<br />
3.0<br />
4.0<br />
5.0
PreStack Depth Migration<br />
The finite difference data is migrated on two local targets<br />
using a un-weighted PreStack Depth Migration algorithm. For<br />
each point of the defined target, the <strong>migration</strong> process performs<br />
a sum of amplitudes along diffraction-traveltime curves.<br />
The stacking is done with wide aperture <strong>and</strong> unit weights<br />
along the diffraction-traveltime curves. The traveltime <strong>maps</strong><br />
required for this process are generated with a first arrival<br />
Eikonal solver in a background velocity model where the target<br />
interface has been removed (figure 3). The first target area<br />
(denoted as target 1) covers the syncline. The second target<br />
area (denoted as target 2) has been chosen beneath the salt lens<br />
in order to study the induced focusing/defocusing effects.<br />
Migrated sections using the source-receiver pairs as input<br />
(every shot, all offsets, traveltimes up to 8.5 s) are displayed in<br />
figures 4 <strong>and</strong> 5.<br />
Depth Depth (km) (km)<br />
0.0<br />
0.0<br />
2.0<br />
2.0<br />
4.0<br />
4.0<br />
6.0<br />
6.0<br />
8.0<br />
8.0<br />
10.0<br />
10.0<br />
( )<br />
12.0 Distance 14.0 (km)<br />
12.0 14.0 0.0<br />
0.0<br />
1.0<br />
Target 1<br />
1.0<br />
2.0<br />
2.0<br />
3.0<br />
3.0<br />
4.0<br />
Target 2<br />
4.0<br />
5.0<br />
5.0<br />
P-velocity (km/s)<br />
1.5 2.0 2.5 3.0 3.5 4.0<br />
Fig.3: Velocity model used for performing the <strong>depth</strong> <strong>migration</strong>.<br />
Target areas are limited by the red boxes. Red squares represent<br />
the shots used as input data.<br />
Fig.4: Migrated section of target 1. Target horizon is superimposed<br />
in black.<br />
Fig.5: Migrated section of target 2. Target horizon is superimposed<br />
in black. The red line superimposed on the horizontal<br />
axis represents the salt lens extension.<br />
PreStack Depth Migration <strong>and</strong> <strong>illumination</strong> <strong>maps</strong><br />
Illumination <strong>maps</strong><br />
In order to generate <strong>illumination</strong> <strong>maps</strong> of the target horizon, a<br />
full data set is modeled by wavefront construction (Vinje et.<br />
al., 1996). Reflection points on the target horizon <strong>and</strong> amplitudes<br />
of the corresponding rays from each shot to each<br />
receiver in the survey are computed. To be comparable to the<br />
finite difference data set, ray tracing is done with cylindrical<br />
sources. The wavefront construction is performed in a 2.5-D<br />
model extrapolated from the 2-D model (see figure 6) using<br />
the same survey as used for the finite difference data.<br />
Receiver<br />
Fig.6: 2.5-D model used to generate <strong>illumination</strong> <strong>maps</strong>. Shots<br />
are shown in black. Reflection points along the target horizon<br />
are plotted in red.<br />
To perform the calculation of the <strong>illumination</strong> <strong>maps</strong>, the surface<br />
of the reflector is divided in bin cells of given constant<br />
area. In each cell, the following quantities are computed:<br />
•hit density (i.e. number of reflection points per unit area)<br />
•<strong>illumination</strong> amplitude<br />
∑<br />
A<br />
i<br />
A = -------------------------------i<br />
Bin Cell Area<br />
where A<br />
i<br />
is the complex amplitude coefficient in the<br />
receiver for ray number i reflecting in the bin cell.<br />
Amplitude <strong>illumination</strong> <strong>and</strong> <strong>migration</strong><br />
Shot<br />
Even using a fairly small aperture (1 km), the survey illuminates<br />
the whole target horizon as may be seen by the reflection<br />
points on the target horizon in figure 6. The steepest part of the<br />
syncline presents a low illuminated zone (x=3.4 km). This is<br />
obvious on both hit density <strong>and</strong> amplitude <strong>illumination</strong> curves<br />
(see figure 7). RMS amplitude along the migrated horizon (figure<br />
8) is smoother than the <strong>illumination</strong> amplitude curve, even<br />
if the general variations show some similarities.<br />
SEG Int'l Exposition <strong>and</strong> Annual Meeting * San Antonio, Texas * September 9-14, 2001
Illumination Amplitude amplitude density<br />
Fig.7: Hit density <strong>and</strong> amplitude <strong>illumination</strong> for the syncline<br />
(target 1). Sampling interval is 25.0 m.<br />
Fig.8: RMS amplitude along the migrated horizon for the syncline<br />
(target 1).<br />
Illumination Amplitude amplitude density<br />
Hit density<br />
x 10<br />
4<br />
4<br />
3<br />
2<br />
1<br />
15<br />
10<br />
0.00<br />
Hit density<br />
5<br />
3<br />
2<br />
1<br />
15<br />
10<br />
2.5 3 3.5<br />
Horizontal coordinate<br />
4 4.5<br />
2.5 3 3.5<br />
Horizontal coordinate<br />
4 4.5<br />
x 10<br />
4<br />
4<br />
5<br />
9.5 10 10.5 11 11.5 12 12.5 13 13.5 14 14.5<br />
Horizontal coordinate<br />
9.5 10 10.5 11 11.5 12 12.5 13 13.5 14 14.5<br />
Horizontal coordinate<br />
Fig.9: Hit density <strong>and</strong> amplitude <strong>illumination</strong> for the area<br />
under the salt lens (target 2). Sampling interval is 25.0 m. The<br />
red line on the horizontal axis represents the salt lens extension.<br />
Low-amplitude zone<br />
focusing<br />
Low-amplitude<br />
Fig.10: RMS amplitude along the migrated horizon under the<br />
salt lens (target 2). The red line superimposed on the horizontal<br />
axis represents the salt lens extension.<br />
PreStack Depth Migration <strong>and</strong> <strong>illumination</strong> <strong>maps</strong><br />
Under the salt lens (red line on figures 9 <strong>and</strong> 10), the hit density<br />
returns to normal (compared to the hit density before<br />
x=10.0 km) whereas the amplitude <strong>illumination</strong> remains lower<br />
due to the energy losses occurring when the wavefield is transmitted<br />
through the salt. This effect is also noticeable on the<br />
RMS amplitude extracted from the migrated section (figure<br />
10).<br />
Near the left edge of the salt lens (x=10.7 km in figure 9), there<br />
is a low-amplitude zone where very little energy is reflected<br />
even if the <strong>illumination</strong> density is high. This low-amplitude<br />
zone is also visible at x=10.7 km in the RMS section in figure<br />
10, but in this case the low-amplitude zone is larger. This is not<br />
an intrinsic limitation of the PSDM process, but rather a side<br />
effect introduced when using first arrival traveltime <strong>maps</strong>. The<br />
Eikonal solver computes first arrival traveltimes, which generally<br />
does not represent the most energetic part of the wavefield<br />
(Geoltrain <strong>and</strong> Brac, 1993). In this case, the first arrival is<br />
associated to a low energy event (figure 11) passing through<br />
the salt. The consequence is that the imaging will take place<br />
through the salt giving lower amplitudes in the PSDM image<br />
from about 9.5 to 11 km. This effect could be corrected by<br />
using only the traveltimes for the most energetic events<br />
instead, or all arrivals.<br />
Distance (km)<br />
8.0 9.0 10.0 11.0 12.0 13.0 14.0 15.0<br />
most energetic<br />
arrival<br />
Fig.11: Multi ray path example on the edge of the salt lens.<br />
Generally speaking, RMS amplitude profiles along both<br />
migrated horizons (figures 8 <strong>and</strong> 10) are smoother than the<br />
corresponding <strong>illumination</strong> <strong>and</strong> amplitude profiles. The PSDM<br />
process is performed on a finite difference data set on which<br />
Fresnel-zone effects introduce a smoothing (Bear et. al., 1999,<br />
Thore <strong>and</strong> Juliard, 1999). Moreover, the PSDM algorithm performs<br />
another smoothing when stacking amplitudes along the<br />
diffraction-traveltime curves. Therefore, RMS amplitude variations<br />
are not as drastic as they appear on the <strong>illumination</strong><br />
<strong>maps</strong>. Nevertheless, several general aspects remain coherent.<br />
Illumination holes <strong>and</strong> <strong>migration</strong><br />
first arrival<br />
Analyzing normal incidence ray tracing data, it is evident that,<br />
in this special case, the steep flank of the syncline is only illuminated<br />
by rays with a traveltime above 5.0 s. On a zero-offset<br />
section extracted from the finite difference data, a PSDM has<br />
SEG Int'l Exposition <strong>and</strong> Annual Meeting * San Antonio, Texas * September 9-14, 2001<br />
0.0<br />
0.5<br />
1.0<br />
1.5<br />
2.0<br />
2.5<br />
3.0
een run twice, once using the full time <strong>and</strong> once with the<br />
traces truncated at 5.0 s (figures 12 <strong>and</strong> 13). The correspondence<br />
between the area of no image in figure 12 b) <strong>and</strong> the<br />
shadow zone in the <strong>illumination</strong> amplitude in figure 14 b) is<br />
good.<br />
a) b)<br />
Fig.12: Migrated section of zero-offset data using the full<br />
traces up to 8.5 s (a) <strong>and</strong> truncating the traces at 5.0 s (b). Vertical<br />
dotted lines in b) delimit the non-illuminated zone<br />
according to the <strong>illumination</strong> amplitude map in figure 14.<br />
Fig.13: RMS amplitude measured along the migrated reflector<br />
using the full traces up to 8.5 s (solid line) <strong>and</strong> truncating the<br />
traces at 5.0 s (dashed line).<br />
Illumination Amplitude amplitude density<br />
b)<br />
Illumination Amplitude amplitude density<br />
a)<br />
15<br />
10<br />
5<br />
1.5<br />
1<br />
0.5<br />
0<br />
x 10 −4<br />
2.5 3 3.5 4 4.5<br />
x 10 −3<br />
Illumination Amplitude amplitude density full time full time<br />
Illumination Amplitude amplitude density cut cut at 5s at 5.0 s<br />
Non-illuminated zone<br />
2.5 3 3.5<br />
Horizontal coordinate<br />
4 4.5<br />
Fig.14: Amplitude density profile using the full traces up to<br />
8.5 s (a) <strong>and</strong> truncating the traces at 5.0 s (b).<br />
PreStack Depth Migration <strong>and</strong> <strong>illumination</strong> <strong>maps</strong><br />
Conclusions<br />
PSDM introduces a smearing of the recorded traces along isochrones<br />
tangential to the reflectors. This is not taken into<br />
account in the <strong>illumination</strong> <strong>maps</strong>, as they are made without<br />
any knowledge of the source pulse, using a simple process of<br />
adding amplitudes in bin cells.<br />
In spite of this, the synthetic example studied here shows that<br />
the variation of the <strong>illumination</strong> amplitude is comparable to<br />
the PSDM amplitude. Important effects like focusing/defocusing<br />
<strong>and</strong> the reduction of amplitude due to energy losses in the<br />
overburden is seen on the <strong>illumination</strong> amplitude profiles. This<br />
synthetic case also shows that there is a good correspondence<br />
between non-illuminated zones predicted by the <strong>illumination</strong><br />
<strong>maps</strong> <strong>and</strong> shadow zones on the PSDM seismic sections.<br />
Acknowledgments<br />
The authors would like to thanks Isabelle Lecomte (NORSAR)<br />
for implementing the PSDM algorithm.<br />
References<br />
•Bear, G., Lu, R., Lu, C., Watson, I. <strong>and</strong> Willen, D., 1999,<br />
The construction of subsurface <strong>illumination</strong> <strong>and</strong> amplitude<br />
<strong>maps</strong> via ray tracing: Annual Meeting Abstracts,<br />
Society Of Exploration Geophysicists, 1532-1535.<br />
•Geoltrain, S. <strong>and</strong> Brac, J., 1993, Can we image complex<br />
structures with first-arrival traveltime?: Geophysics, 58,<br />
no. 04, 564-575.<br />
•Pereyra, V., Carcione, L., Munoz, A., Ordaz, F., Yanez,<br />
E. <strong>and</strong> Yibirin, R., 1999, Model-based simulation for survey<br />
planning <strong>and</strong> optimization: Annual Meeting<br />
Abstracts, Society Of Exploration Geophysicists, 625-<br />
628.<br />
•Rosl<strong>and</strong>, B.O., Drivenes, G., Large Scale 3D Seismic<br />
Modelling in Exploration, Exp<strong>and</strong>ed Abstracts from the<br />
62nd Annual EAGE Conference, Glasgow, May 2000.<br />
•Sassolas, C., Lescoffit, G. <strong>and</strong> Nicodeme, P., 1999, The<br />
benefits of 3-D ray tracing in acquisition feasibility:<br />
Annual Meeting Abstracts, Society Of Exploration Geophysicists,<br />
629-632.<br />
•Thore, P. D. <strong>and</strong> Juliard, C., 1999, Fresnel zone effect on<br />
seismic velocity resolution: Geophysics, 64, no. 2, 593-<br />
603.<br />
•Vinje, V., Iversen, E., Åstebøl K., <strong>and</strong> Gjoystdal, H.,<br />
1996, Estimation of multivalued arrivals in 3D models<br />
using wavefront construction-Part I&II, Geophysical<br />
Prospecting, 44, 819-58.<br />
SEG Int'l Exposition <strong>and</strong> Annual Meeting * San Antonio, Texas * September 9-14, 2001