Comparison of seafloor sound-speed profile measurement between the image source and reflection seismology techniques Samuel Pinson To cite this version: Samuel Pinson. Comparison of seafloor sound-speed profile measurement between the image source and reflection seismology techniques. 2015. <hal-01254106> HAL Id: hal-01254106 https://hal.archives-ouvertes.fr/hal-01254106 Submitted on 11 Jan 2016 HAL is a multi-disciplinary open access archive for the deposit and dissemination of scientific research documents, whether they are published or not. The documents may come from teaching and research institutions in France or abroad, or from public or private research centers. L’archive ouverte pluridisciplinaire HAL, est destinée au dépôt et à la diffusion de documents scientifiques de niveau recherche, publiés ou non, émanant des établissements d’enseignement et de recherche français ou étrangers, des laboratoires publics ou privés. Comparison of seaoor sound-speed prole measurement between the image source and reection seismology techniques S. Pinson a) Laboratório de Vibração e Acústica, Universidade Federal de Santa Catarina, Floriaónopolis, Brazil (Dated: July 13, 2015) In the context of sediment characterization, the image source method provides a fast and automated sound-speed prole measurement of the seaoor. In this letter, this method is compared to reection seismology methods. The comparison highlights similarities in the signal processing and a dierence in the basic equations of the wave reection travel time analysis. Understanding the links between the two methods helps sheds additional light on each method. PACS numbers: 43.30 Ma, 43.30 Pc, 43.60 Fg, 43.60 Rw (a) 1. Introduction A technique has recently been developed for rapidly estimating sub-seabed sound-speed proles using the concept of image sources. Hydrophones Source The image source method (ISM) has been used for measurements from a vertical 4,5 which yields a point estimate of sound receive array speed vs depth in the seabed. More recently it has 4,6 yielding the been applied to horizontal array data layer 0 (water) layer 1 layer 2 two-dimensional (depth vs range) sound-speed structure (b) of the seabed to 50 m in sub-bottom and 14 km in range with resolutions roughly 1 m in depth and 5 m in range. It turns out that the fundamental equations of the 40 image source method can be understood and compared with those from classical seismic reection methods. underlying connections between the two methods. The secondary purpose is to briey consider, in the light of the connections, relative strengths and possibilities of extension for the ISM. The letter is organized as follows. of both methods are presented. First, the principles This is followed by a short discussion to explore some basic dierences and similarities between them. 2. Basic ideas of the methods 35 Offset (m) This is the purpose of this letter, rst to explain the 30 25 20 0.025 0.03 0.035 0.04 0.045 Time (s) 0.05 0.055 Figure 1: (a): Sketch of the experiment. (b): Simulated seismogram of the seaoor reections. lated by a numerical evaluation of the Sommerfeld integral (see appendix of Ref. ? ) using the following geome- A typical measurement conguration for seaoor char- try: the source and 10 hydrophones are 20 m above the acterization by reection seismology is a source and a seaoor, the hydrophones are linearly spaced between 20 linear array of hydrophones (Fig. 1a). The source emits and 38 m from the source. The environment parameters a low frequency, short, powerful pulse such that the are presented in the Table I. A Mexican hat centered at wave goes deep into the seaoor. Then the wave is re- 1500 Hz has been used for the emitted pulse shape and ected from geological interfaces and recorded by the hy- 0.2% amplitude Gaussian noise related to the maximum drophone array. amplitude reection is added to the simulated signals. For illustration purposes, a set of data has been simu- The low noise is added to avoid division by zero in the semblance functions described in the next sections. The simulated reected echoes are displayed in Fig. 1b. Multiple paths between the seaoor and the sea surface are a) Electronic address: [email protected] not considered here. Image source & reection seismology 1 If one assumes that Layer n◦ Thickness (m) Sound speed (m/s) Density (kg/m3 ) 0 (water) 20 1500 1000 1 5 1600 1500 2 6 1700 2000 3 ∞ 1800 2500 Table I: Layered media parameters. c(l) rms (l) (l) (l) cnmo ≈ crms with: v u Pl (i) 2 (i) u i=0 (c ) τ⊥ t , = Pl (i) i=1 τ⊥ (2) c(i) is (i) the sound speed and τ⊥ is the travel time at normal incidence in the layer i, then one can apply the crms layer i where is the root mean square sound speed, 2 Dix formula to obtain layer sound speeds : c(l) v u (l) 2 (l−1) u (crms )2 t(l) − (c(l−1) rms ) t⊥ ⊥ . =t (l) (l−1) t⊥ − t⊥ (3) 2.1. Reection seismology There are dierent ways to determine the normal move Obtaining the sound speed in reection seismology is out sound speeds. One of them consists in calculating a rst step for imaging the earth's interior by migrat- a velocity spectrum (velocity rather than sound speed is ing the recorded signals at the correct reector's depths. used in the seismic community) For reection from interface l of the layered media, the 10 . The velocity spectrum is calculated by summing the recorded signals along hy- layered media is approximated by an equivalent homoge- perbolas (colored curves on Fig. 1b) dened by Eq. (1): (l) neous medium in which the sound speed is cnmo . The subscript nmo s X 2 2 1 N H x − x n s , V S(t⊥ , cnmo ) = sn t2⊥ + N c nmo n=1 is used in the seismic community and stands 10 . To determine c(l) , the nmo for Normal MoveOut (NMO) three sides of the right triangle are considered: the o- (4) (xs − xn ), twice (l) (l) the depth of the interface t⊥ × cnmo , and the hypotenuse (l) (l) (l) tn × cnmo (Fig. 2). t⊥ is the null oset travel time (i.e. (l) at normal incidence) of the interface l reection and tn is the travel time of the interface l reection at the oset set between the source and the receiver (xs − xn ). (l) time tn of the reection from interface l trum avoids that problem: P 1 N N n=1 sH n V Ssemb (t⊥ , cnmo ) = PN H 1 n=1 sn N z (l) θnmo (l) θnmo (l) source c (0 ) o m interface xn −xs cnmo (5) signals are identical along travel time hyperbolas and l close to 0 when dierent. t (l) × t (l) × image t2⊥ The semblance is a similarity measurement and is 1 when (l) cn (l) (l) ! 2 2 + . ! r 2 2 x −x t2⊥ + cnnmos r x θ0 t⊥ × cnmo stands for Hilbert trans- low amplitude reections. The semblance velocity spec- is written: = (xn , 0) rc = (xc , 0) H plitude reected pulses thus making it dicult to detect sensor rn = (xs , 0) signal recorded at the hy- form). The velocity spectrum is not sensitive to low am- Using the Pythagorean theorem, the travel source rs sH n (t) is the analytic drophone n (the superscript where local maxima of It is then possible to select V Ssemb (t⊥ , cnmo ) to calculate a sound- speed prole using Eq. (3). image source located in a 2.2. Image source method water sound-speed medium Figure 2: Ray diagram for the reection on the interface l in a (l) cnmo equivalent sound-speed medium. In gray is the ray diagram for the image source l located in a water sound-speed c(0) medium. The idea of the ISM is to consider wave reections from geological interfaces as waves coming from image sources located symmetrically to the real source relative to the interfaces. The image sources are located in a water sound speed c(0) medium by migrating the recorded signals in the space domain: t(l) n ≈ s (l) t⊥ 2 + xn − xs (l) cnmo 2 , (1) 2 N 1 X Im (r) = sH n (tn (r)) , N (6) n=1 Image source & reection seismology 2 where tn (r) = krn − rk /c(0) and r = (x, z) is the spatial 3. Link between the methods coordinate. Im (r) This function is displayed in Fig. 3a where the 3 One can notice the strong similarity between Eq. (4) z ≈ and Eq. (6), the velocity spectrum and the image source images relative to the 3 interfaces are apparent at −40, -50 and -62 m. But because their amplitudes are a function of impedance contrast, this means that low map respectively. Both consist of summing the signals along hyperbolic travel times which are driven by dier- cnmo ent parameters: a semblance function of the migrated signals is used for and, an automatic detection: The similarity is such that it is possible to change the semblance function in Fig. 3d results and z change of variables from (7) r = (x, z) s in small Applying a threshold on this function, the image source search area is conned to a neighborhood. cnmo = Im (r). c(0) |xc − xs | , tc sin θ0 s One can t⊥ = tc cos θnmo = tc 1− notice in Fig. 3d that image sources related to multiple reections between interfaces also appear. Even weak noise on the simulated signals generally hides those low amplitudes from real echoes ? . Also environment, the for signals multiple recorded reection be- (cnmo , t⊥ ) using (10) and: The image source locations are found by taking the local maxima of to Eq. (9) and simple trigonometry (Fig. 2): regions where the focused signals are coherent which simplies image detection. for the velocity spectrum for the image source map. image source map into a velocity spectrum through a 2 P 1 N (t ( r )) N n=1 sH n n Isemb (r) = 1 PN . 2 H n=1 |sn (tn (r))| N The x and t⊥ impedance contrast layers will be dicult to detect. So tc = krc − rk /c0 cnmo sin θ0 c0 2 (11) |xc −x| |zc −z| . The result of this variable change is shown on Fig. 3b for where the Im and θ0 = tan−1 map and on Fig. 3e for the Isemb map. Fig. 3c tween interfaces are assumed to be hidden by reections and 3f are a zoom on the NMO sound speeds of Fig. 3b from deeper interfaces through the Born approximation . and 3e. 6 After image source localization, the receive array is collapsed to a point sensor at the array center 1 N (0) P c rc = (xc , zc ) = n rn . With the assumption of a water sound speed equivalent medium, the image sources are not on the vertical source axis as they should be (gray drawing in Fig. 2). From the location of image sources, one can (l) between the image source deduce the travel times tc (l) l and the array center rc and the angle of arrival θ0 (the subscript stands for the angle of incidence in water i.e. layer 0 and the upper index stands for the interface number on which the wave is reected). With these parameters it is then possible to deduce layer sound speeds and thicknesses using ray theory (l) time tc and the angle of arrival 1,46 . (l) θ0 From the travel 4. Discussion A comparison between Eq. (1) and Eq. (8) provides the basic dierence between classical reection seismology and the image source method. From the reection seismology point of view, the problem is written considering the right triangle dened by the source, the receiver and the image source in a medium. (l) cnmo equivalent sound-speed From the ISM point of view, the problem is written considering the source-receiver oset, the travel time and the angle of arrival on the receiver in a water sound speed c(0) medium. In reection seismology, one considers more realistic travel times by approximating , it is also possible to the wave front shape as being ellipsoidal. From a physics obtain the sound speed of the homogeneous media, equiv- point of view, reection seismology is better because ISM alent in travel time, to the layered media. Eq. (1) of the approximates the wave front as spherical. For this reason echo travel time is rewritten using the angle of arrival on the ISM has to use a limited aperture array to enable a the sensor: coherent echo summation in the image source localization t(l) c ≈ where (l) sin θnmo 1 (l) × sin θnmo |xc − xs | (l) (8) cnmo can be deduced from Snell-Descartes relation. process. , ections on interfaces, it becomes useful to understand (l) sin θ0 through the Then the equivalent medium sound-speed is given by: s c(l) nmo = As the ISM is an intuitive way of modeling the wave resome possibly unexpected phenomena associated with the velocity spectrum semblance function. Using the migration function (Eq. (6)) to nd the image sources, the resolution of the image location is driven by two dierent c(0) |xc − xs | (l) tc (l) sin θ0 experimental parameters: the array aperture that drives . (9) the angle resolution of the images and the pulse shape that drives the range resolution of the images to the array. Using the semblance function for the ISM, the angle Finally, using the Eq. (3) one can obtain the layer sound resolution remains the same but the range resolution is speeds. lost. Indeed, if the range resolution is driven by the pulse Image source & reection seismology 3 Figure 3: (a) and (d): Image source maps using respectively Im (Eq. (6)) and Isemb (Eq. (7)). The red point corresponds to the real source and the black points correspond to the hydrophones. (b) and (e): Im (Eq. (6)) and Isemb maps with coordinates changed from x and z to cnmo and t⊥ using Eq. (10) and Eq. (11) in order to obtain a velocity spectrum. (c) and (f): Zoom of (b) and (e). The colorbars on the right are related to the rows. The Im colormap is normalized by the maximum. Isemb is intrinsically between 0 and 1. shape for the migration function, the semblance shows a geologic interfaces are coherent value of 1 for the whole pulse duration (in the geologic interfaces and, neglected), case of a good signal to noise ratio). isotropic at and and parallel homogeneous This interpreta- layers. The reection seismology methods have far fewer tion in terms of angle and range resolution is lost for the assumptions, given many decades of progress since their semblance velocity spectrum (Eq. (5)). It results in the introduction. impossibility of an accurate automatic detection of the anisotropy NMO sound speeds using this semblance velocity spec- ters trum. 8,9 For example, extension to include the or inhomogeneities/statistical parame- 3,7 . It is possible, now with a clearer understanding Because of that, using the ISM, the semblance of the connections between the ISM and the classical function is only used to window small areas of the migra- methods, that ISM may be able to exploit some of these tion function (Eq. (6)) in which signals are summed co- advances. herently and in which accurate localization is performed using local maxima. The same process should be apply when using velocity spectrum. Using Eq. (1) to dene the travel times implies the use of an horizontal array for seismic techniques. 6. Acknowledgements By contrast in ISM, since the sound-speed equations are a function of the array center coordinate rc , the array conguration The author would like to gratefully acknowledge Charles Holland for his help and stimulating discussions is very exible as long as its aperture is not too large. about that work. Indeed, the rst results of the ISM was obtained using a This work is funded by Direction Générale de l'Armement vertical array of hydrophones moored on the seaoor . (DGA) through the Laboratoire Domaine Océaniques Originally the ISM did not employ the NMO approxi- (LDO) of the Institut Universitaire Européen de la Mer mation to give sound-speed proles. (IUEM). 5 Nevertheless, this formulation, borrowed from reection seismology, could be useful for eliminating the parallel layering restriction. 1 2 5. Conclusion 3 In its present form, the method requires the Born approximation (the multiple reections between the G.M. Bryan. The hydrophonepinger experiment. Acous. Soc. Am., 68:14031408, 1980. J. C.H. Dix. Seismic velocities from surface measurements. Geophysics, 20:6886, 1955. B. Iooss. 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