IMPROVEMENTS IN DIGITAL TIME-DELAY ACOUSTIC IMAGING

Abstract: This invention relates to improvements in or relating to digital time-delay acoustic imaging. According to the invention there is provided an acoustic imaging method for marine survey and other purposes comprising the steps of: insonifying a target area by periodic acoustic pulses; detecting reflections of said pulses by an array of at least two receiver transducers, which transducers generate respective output signals in response thereto, wherein further the signals are: sampled in time at a predetermined rate during an interval between said pulses; converted from analog to digital form; processed so as to generate a composite acoustic signal for each pixel in the insonified target area required to be imaged; and match-filtered with optimised filters in the frequency domain with an estimated source pulse signature.

Description: IMPROVEMENTS IN DIGITAL TIME-DELAY ACOUSTIC IMAGING INTRODUCTION This invention relates to improvements in or relating to digital time-delay acoustic imaging. The invention particularly, though not exclusively, relates to an acoustic method and apparatus intended for marine survey applications. The invention is also applicable to other applications of acoustic imaging. 2. PRIOR ART 2.1 GENERAL The general approach to digital acoustic imaging given in the literature is to store the set of samples received from a 2D or 3D array of transducers in a "space-time memory" . Processing of this dataset should enable an image of the whole insonified area or volume to be reconstructed [1] . Time-delay beamforming is the most widely used analog technique, being robust and either narrowband or wideband. It can also be extended from beamforming to imaging in polar coordinates by using a large number of beams simultaneously, separated in angle by a- few degrees. A digital version preserves these advantages, while adding some important new capabilities, particularly the ability to image in a Cartesian or other coordinate system, and the selection of the region of the scene to be imaged under computer control ("pan and zoom") . Conventional analog time-delay beamforming uses a fraction of the information received from an array of transducers to generate a line-scan of the scene in one particular direction. This direction is defined by a differential time delay, inserted between each pair of transducer echoes, before summation to form a composite signal with the required directivity. Time-delay imaging relies on fine compensation for phase-shifts between samples received at adjacent transducers. Hence a digital implementation requires either high sampling rates which is expensive both in digitizing hardware and computational load, or some method of interpolation between digital samples. Two papers by Pridham and Mucci in 1979 [2,3] established powerful techniques for interpolating or "upsampling" a sequence of digital samples, and proposed specific beamforming procedures using interpolated sampled signals from a transducer array. These interpolation techniques are based on local spectral estimation of FFT components by quadrature filtering. A paper by Ries [4] reviewed various interpolation techniques including Pridham and Muccis ' formulation. Ries gave an analytic solution for optimising the filter kernels, but did not discuss the possibility of avoiding explicit interpolation in the time domain. 2.2 THE INVENTOR AND OTHERS In 1992, a Patent was applied for in the names of Shippey and McHugh [5] . The acoustic imaging method claimed there uses essentially the same phase-shifting technique as Pridham and Mucci, employing a set of adjacent digital filters spanning the signal bandwidth (quadrature comb filter) for local spectral estimation. However explicit interpolation in the time domain is avoided with consequent simplification in the computation. This earlier Patent proposed a wideband version of the technique in which local spectral components of the composite echo are cross-multiplied by local spectral components of a frequency modulated source pulse to achieve pulse compression at little extra cost . However it gives no idea of how long the time window used in the comb filter for local spectral estimation should be, or the shape of the window function. It turns out that the shape of the window function is extremely important for the success of match-filtered imaging. This window function determines the bandwidth of each spectral component used in the comb filter. Unless the bandwidth of the source signal is spanned uniformly by the spectral components of the comb filter, time-delay correction by phase-shifting the spectral components becomes inaccurate. The shape of the window function also determines the shape of the match-filtered output, for example the width of the peak, and discrimination against background noise. It is not at all obvious that the same window function can satisfy these different requirements simultaneously. In the present Patent Application a method of designing the window function is given for any kernel length. It turns out that the required shape is not standard, so the availability of at least one design technique is very important. Furthermore, using this design technique, good performance can be obtained with fewer spectral components, and much shorter kernel lengths than would be expected. If the bandwidth of the source signature is not too wide, even a single spectral component can give adequate performance. For the narrowband case, with a single carrier frequency, the invention enables shorter kernel lengths to be employed. 2.3 SYNTHETIC APERTURE ACOUSTIC IMAGING Synthetic-aperture-radar (SAR) imaging, is mature technology, and the literature goes back many years [6,7] . There are also papers on synthetic-aperture imaging for non- destrucive testing applications, eg [8] . There are also early papers on synthetic-aperture imaging through water , ie Synthetic-Aperture Sonar (SAS) [3] , based on similar principles to SAR. However the technology is much more difficult for two reasons: a) pertubations in the movement of the acoustic platform through the water medium, compared with the very stable movement of an earth satellite in space. b) perturbations in the propagation of acoustic waves through the water medium due to currents and thermal effects, which are larger than the corresponding perturbations for propagation of electromagnetic waves in air. There have been recent studies on the effect of platform positioning errors on SAS imaging resolution, eg [10] . A method of compensating for these errors would make SAS more feasible, and a method of doing this will be given in this Application. 3. OBJECTS OF INVENTION An object of the invention is to obviate or mitigate disadvantages/problems in the prior art. Other objects of the invention include: to reduce the computation required for digital acoustic image reconstruction, and to improve the resolution of the reconstructed image. The invention has two aspects: 4. SUMMARY OF THE INVENTION ASPECT A: OPTIMISED MATCH-FILTERED IMAGING A first aspect of the invention offers a computationally efficient method of digital acoustic imaging, in which match-filtering is obtained at minimal additional computing cost by proper design of the window function used for local spectral estimation. If the source signal is frequency-modulated, a so-called "chirp" source, then match-filtering provides the pulse-compression required using such a source. ASPECT B: IMPROVEMENTS TO SYNTHETIC-APERTURE SONAR A second aspect of the invention extends the basic method of generating the composite signal for both narrowband and wideband echoes from real to synthetic apertures, and provides an automatic method for correcting for uncertainty in platform position, and the phase of the transmitted pulse. Although the invention is described in terms of digital hydroacoustic (sonar) imaging, either aspect could conceptually be applied to NDT (non-destructive industrial testing of materials) or medical ultrasonic imaging. The use of an optimised envelope design for Aspect A of the Invention applies to match-filtering of acoustic or radar echoes generated in any manner whatever provided that these echoes can be converted to sampled digital data. 4A. A SUMMARY OF ASPECT A OF INVENTION: EFFICIENT MATCH-FILTERED IMAGING (FIG 1) 4A.1 SYSTEM OUTLINE There is provided an acoustic image method for marine survey and other purposes wherein a target area is insonified by periodic acoustic pulses, for example "chirp" (swept-frequency) pulses. Reflections of said pulses are detected by a receiver array of at least two transducers which generate output signals in response thereto. These signals are: a) sampled in time at a predetermined rate during the interval between said transmitted pulses, b) digitized by some known form of analog-to-digital conversion equipment, c) processed so as to generate a composite acoustic signal for each pixel in the insonified target area which is required to be imaged. d) match-filtering in the frequency domain with the estimated source pulse signature. The invention further provides an apparatus for use in an acoustic imaging system as defined above. It may be convenient to store digitised samples from step (b) in digital computer memory prior to step (c) , but this is not a necessary feature of the invention. The more detailed description below will be simplified by assuming that Doppler shifting of the acoustic echo due to differential motion of the target area and the transducers is negligible. The modifications necessary to handle Doppler shifting for a real aperture will be given in Section 4B.4 and for a synthetic aperture in 4A.5. 4A.2 GENERATING THE COMPOSITE ECHO (STEP c) This step is executed as follows for a 2D or 3D image: for each pixel in the required image, i) a corresponding set of digitized samples is selected for each transducer, the echo time for the centre sample of the set being closest to the estimated time of flight of a transmitted pulse to the point in the insonified area corresponding to the pixel and back to the particular transducer in the array. ii) for each such sample set, local in-phase and quadrature frequency components are estimated by a quadrature comb filter, ie a set of one or more quadrature digital filters spanning the signal bandwidth with a common window function {WJ}, i=-}_L..5.L-1, where L is the length of the kernel in samples. This window function should preferably have been optimised in a preliminary step e, described in Sec. 4A.4 below. iii) each pair of local in-phase and quadrature components is phase-shifted to correct for any difference between the required time delay and the time delay for the ' selected centre sample. iv) the in-phase and quadrature frequency components of the composite signal are formed as the weighted sum of phase-shifted in-phase and quadrature components for each transducer. It may be preferable to carry out step c(ii) for all possible sample sets or subsets thereof before step c(i) . Step c is defined mathematically in Equations Al,Ala,A2,A2a,A3 of Appendix A. 4A.3 MATCH-FILTERING OF COMPOSITE ECHOES (STEP d) This match-filter step is executed by: (i) extracting one or more corresponding spectral components of the source signature,, using the same digital comb filter used for Step c(ii) ; ii) complex multiplication of the above spectral components of the source signature by the spectral components of the composite echo signal, to generate the complex matched filtered signal in accordance with (A4-9) , and (All) of Appendix A; iii) addition of the above in-phase and quadrature spectral components to generate the in-phase and quadrature components of the complex envelope; iv) determination of the magnitude of the complex envelope by squaring and adding the in-phase and quadrature components of the complex match-filtered signal in accordance with (A10) . If the source signature is stable from pulse to pulse, then Step d(i) can be carried out in advance, and need not be repeated for each pulse or "ping" . If only a single spectral component is used, then step d(ii) becomes redundant. Pulse compression is already achieved by optimisation of the window function used in step c(ii) . 4A.4 OPTIMISATION OF WINDOW FUNCTION (STEP e) 4A.4.1 Methodology A standard comb filter for local spectral estimation is the local FFT with a standard window function such as the Hanning Window. Using such a comb filter for pulse compression, the kernel length should be at least equal to the length of the transmitted pulse for good compression. The number of FFT components required to span the signal bandwidth increases with the number of samples contained in the pulse length. This aspect of the invention is the use of shorter kernel lengths than the pulse length, and a subset of at least one Fourier spectral component by using an optimised window function. This reduces the computing load in steps c(ii) and c(iii) above proportionately. It is not obvious that window functions can be found which simultaneously provide good time compensation in step c(iii) and good pulse compression in step (d) . It is also not obvious that an optimisation technique can be found which will give good window functions. However for given source signature, sampling interval, kernel length L, and choice of spectral subset, an optimised window function {w,-} is found by the iterative technique outlined below, which minimises the error function Err t defined below, and more formally in Appendix B: The Phase Error Err p is defined as the standard deviation of time-displaced and time-compensated pulse- compressed echoes of the source signal from each other using the algorithm of Appendix A, estimated for a range of sub- sample time displacements, and normalised appropriately. The Shape Error Err s is defined as the standard deviation of the complex envelope of the same output signal from an ideal response, which is the complex envelope of the match-filtered source signature, normalised appropriately. Let C be the compression ratio, defined as the peak signal to rms noise ratio after match-filtering, divided by the peak signal to rms noise ratio before match-filtering. Define C 0 as the compression ratio obtained using time- domain match-filtering. Then if C is the compression ratio obtained using frequency-domain match-filtering as in steps c,d above we can define an error function Err c proportional to log(C/C 0 ) . The Error Function which is minimised by mathematical optimisation of the envelope is a weighted function of Err p ,Err s ,Err c and possibly other errors, eg Err t = U p Err p + u s Err s + u c Err c .... where u p , u s , u c ... are weights chosen in accordance with the operational importance of the individual errors. One method of envelope optimisation is to use the following iterative procedure: i) iteration begins using a standard window function of length L such as the Hanning window; ii) at each iteration step, the change e^ in Err t is estimated for equal small changes in each envelope coefficient Wj; iii) a change in the whole set of envelope coefficients {W J } is made in proportion to the set {e,-}; iv) the iteration process can be stopped when the change in the envelope at each iteration becomes negligible. After optimisation, it is possible to assess the performance in terms of : * time-compensation, * sensitivity to noise, * peak width of compressed pulse, * secondary peak levels, etc. Hence it is straightforward to estimate the minimum acceptable kernel length, and in the wideband case the minimum number of spectral components for particular operational situation. 4A.4.1 Results of using the optimised window function Fig 2A, 2B gives the component pulse shapes and the optimised envelope (right-hand side) for the following situation: Source signature: chirp from 0.1 - 0.4 normalised by sampling frequency pulse envelope: Hanning pulse length: 65 samples. a) Hanning envelope, 65 samples, 21 spectral components. b) Optimised envelope, 49 samples, 5 spectral components. The compressed pulse amplitude is reduced in proportion to the Compression Loss. In this example, the Shape error is marginal and the Phase Error is negligible for the optimised window. In another test, with the following parameters: Source signature: chirp from 0.3-0.45 normalised frequency pulse length: 129 samples a) Optimised envelope, 129 samples, 1 spectral components, b) Optimised envelope, 129 samples, 3 spectral components, Fig 3A shows the compressed pulse using only one component and Fig 3B with three components. The compressed pulse using time-delay match filtering is shown on both graphs for comparison. Fig 3C shows the two optimised envolopes. Stray signal outside the main peak is noticable in Fig 3A but still acceptable for most purposes. This stray signal is eliminated in Fig 3B at the expence of Compression Loss. Phase errors are again negligible, giving almost perfect time-delay imaging. 4A.4.3 Discussion The computational advantages of using optimised filters increase with pulse length, enabling this method of digital imaging to be used with preferred pulse lengths in situations where the computational load would otherwise be prohibitive. Successful optimisation can be carried out even for kernel lengths which are only 1/4 of the pulse length at the expense of peak signal-to-noise discrimination, or using a single frequency component at the expense of secondary peaks in the compressed pulse. Both penalties may be acceptable in particular operational situations. The method of time-delay imaging combined with pulse compression is any case computationally efficient, avoiding explicit interpolation in the time domain, and providing match-filtering at little extra cost. In combination with envelope optimisation, the technique becomes very attractive indeed. 4A.5 SIGNIFICANT DOPPLER SHIFT DUE TO MOTION 4A.5.1 Introduction This is the situation where there is a significant closing velocity of the transducer array with respect to all or part of the target region. Closing velocity due to motion of the transducer array can be estimated from standard instrumentation, for example standard navigation instrumentation in the case of a transducer array mounted on the hull of a vessel. Closing velocity due to motion of a discrete target can be detected by spectral analysis of the echo itself. The closing velocity has two effects: * it modifies the times of flight used in step c(i) above * it modifies the spectral components of the echo from the region in space corresponding to each pixel in the image by the Doppler Shift for echoes from that direction. 4A.5.2 Correction to time delay The two-way delay time for a particular pixel and a particular tranducer can be expressed as the sum of two components: * the delay time to some reference point on the array; * the differential delay time to the particular transducer. Provided that the array is not rotating rapidly in space, the differential delay times are negligibly affected by Doppler shift, and only the delay time to the reference point is affected. This delay time is nominally twice the spatial separation of the reference point on the array from the pixel centre in space, divided by the speed of sound in the medium. Doppler shift is corrected for by subtracting the closing velocity from this speed. 4A.5.3 Spectral estimation For real aperture imaging, the set of spectral filters used must be modified to span the echo bandwidth as modified by Doppler shift. This modification could mean shifting centre frequency (frequencies) , adding one or more spectral components, etc. It may also be necessary to allow for Doppler shift in the copy of the source pulse used for match-filtering. This can be done by compressing or extending the pulse in the time^-domain before applying the comb filter in step d(i) . If the expected Doppler shift is dependant on the pixel being imaged, then several sets of source pulse spectral components are required for step d(i) , spanning the range of Doppler shifts which can be expected. If the source pulse is stable from pulse to pulse, these direction-dependant frequency components can be stored from pulse to pulse, and need only be recomputed if the speed of motion changes significantly. 4A.6 OPTIMISED PULSE COMPRESSION FOR COMPOSITE SIGNALS DERIVED OTHER THEN IN STEP c Step d can be applied when a composite sonar or radar echo signal is provided by other means as follows: (i) the composite echo signal is sampled and digitized as in steps a and b above if not already in digital form, (ii) spectral components of this composite signal are then extracted as in step c(i) . The phase-shifting in step c(ii) is omitted as the composite signal has been formed already. (iii) match-filtering is carried out using an optimum window as described in 4A.4 above, but with Err p excluded from Err t , since there is no phase-error to minimise. 4B SUMMARY OF ASPECT B OF INVENTION: EXTENSION TO SYNTHETIC-APERTURE IMAGING 4B.1 INTRODUCTION The new method of synthetic-aperture acoustic imaging relies on the possibility of computing time-delays from pixels located in a coordinate system fixed in space to both the source and receiver transducers of a moving acoustic platform. This acoustic platform could be: i) a vehicle moving through a water medium for hydroacoustic applications; ii) a hand or machine-held ultrasonic transducer configuration for medical ultrasonic or non-destructive testing; The method of generating the required time delays depends on application. Section 4B.2 presents possible methods for use in hydroacoustic applications. If synthetic-aperture imaging is used, the minimum number of receiver transducers in Sec. 4A.1 is reduced to one. 4B.2 ESTIMATION OF TIME DELAYS FOR IMAGING IN A STABILIZED COORDINATE SYSTEM 4B.2.1 Positioning system There is provided a positioning system such as GPS which directly or indirectly enables the position of some reference point on the acoustic platform, conveniently chosen to be the effective origin of the source pulse, to be located in the required spatial coordinate system. There may also be provided an additional positioning system, such as a conventional echo-sounder, which gives the height of the acoustic platform above the seabed surface immediately below it. 4B.2.2 Attitude measuring system There is provided an attitude measuring system, eg gyroscope and compass, which directly or indirectly enables each transducer of the receiver array to be located in space with respect to the said reference point. 4B.2.3 Basic Computation Let the required image frame of reference be a 3D volume fixed in space, or a 2D slice of the water volume, aligned with the required ground coordinate system. Then the time delays from each 3D pixel (voxel) to each transducer can be found as follows: i) by a standard mathematical procedure, the location of each required pixel in space is converted to a location in a coordinate system fixed to the acoustic platform, with the reference point as origin, using the position and attitude information available from 4B.2.1, 4B.2.2. ii) The distance from each required pixel to the origin is then given by Pythagoras equation. This can be converted to time by dividing by the estimated speed of sound in the medium. iii) The differential distance to each receiver transducer, and hence the differential acoustic travel time for a wave originating from the pixel is also given by standard geometry. In the computation c(iii) of 4A.2, these differential delays are required with great accuracy in order to image the composite signal correctly for each pixel. The time delay to the reference point, which is considerably larger, is required with lower accuracy. Hence the above procedure has important advantages. A useful approximate computation of time-delays is given in Appendix B. 4B.2.4 Time-delays to Seabed Let the required image be a 2D area of the seabed defined in the required spatial coordinate system. Then the above procedure must be modified in order to locate the seabed surface in the vertical direction. This can be done in different ways- depending on the operational situation, for example: i) the seabed is assumed to be locally flat and horizontal. Then all pixels of the seabed surface can be assumed to lie in a plane, in which the vertical distance below the platform is known from 5.2.1 ii) the acoustic aperture containing the set of receiver transducers has extension in the vertical or Z direction; for example it may consist of two linear rows of transducers, one above the other separated by the mid-value of the acoustic wavelength. Then for each (X,Y) pixel on the seabed, it is possible to estimate time delays for a range of Z values, and select the Z value giving the greatest amplitude for the pixel . 4B.3 SYNTHETIC APERTURE TECHNIQUE 4B.3.1 Introduction The methodology will first be described for a simplified situation (Fig. 3) in which just two narrowband source pulses are emitted, and two successive sets of echoes are received as the acoustic platform moves horizontally, parallel to the real array aperture. Then we obtain a synthetic receiver aperture which is the combined extent of the two real receiver apertures. Too large a movement between successive pings produces a gap in the synthetic aperture, giving the same side-lobe problems as a gap in a real receiver aperture, but this is a detail engineering design question. We consider the imaging of one particular pixel located in space, which is insonified from both positions of the acoustic platform. The further simplification is made that the transmitted source pulse from the second location is a precise copy of the source pulse transmitted from the first location. The further assumption is made that at the acoustic frequencies used, the echo time for a signal to and from the specified location in space is predictable to within a small fraction of the acoustic wavelength. The initial description of the method is simplified by considering a narrowband source pulse. Then the composite signal is required only for the carrier frequency. 4B.3.2 Methodology For each location of the array, the in-phase and quadrature components of the composite echo at each pixel are given by step c in Section 4A.2 above, with a single spectral component f c equal to the carrier frequency. Provided the estimated time delays are accurate, and the conditions of 4B.3.1 are fulfilled, then it is merely necessary to break the sequence of steps c(i)-c(iv) , d(i)- d(iv) of Sec. 4A.1 and 4A.2 at some point and combine the partially processed outputs from the two succesive pulses as the transmitter and/or receiver transducers move in space, before completing the sequence of operations. Four possibilities are illustrated in Fig 4: A) combining the spectral components of the composite signals after step c) ; B) combining the spectral components of the match- filtered signals after step d(ii) ; C) combining the in-phase and quadrature components of the complex envelope after step d(iii) ; D) combining the magnitude of the complex envelope after step d(iv) . To some extent the choice is a matter of computational convenience. Other factors affecting the choice are discussed in Sections 4B.3.6, 4B.4, 4B.5. The same principle can be extended directly to three or more successive positions of ■ the array, with a correspondingly longer synthetic aperture. For continuous synthetic-aperture imaging, the outputs for pixels in successive images should be placed in storage. After each new ping, the signals from the last n images are added to form a synthetic aperture image covering n pings, for some selected value of n. 4B.3.3 Correction for Phase Shift in the Source Pulse Assume that the arrangement of Fig 3A is used. The requirement of phase coherence of the source pulse can be relaxed as follows. It is supposed that there is an unknown phase shift of the carrier frequency of the source pulse between successive pings. Any phase shift in the source signature produces the same phase shift in the composite signal for all pixels reconstructed from that ping. Then θ can be found from the image data as follows. Let the set {P,-} be some selected subset of the common pixels in successive images from Position 1, Position 2 of the array, chosen to exlude far-range pixels where the signal-to-noise level is poor. Let the composite signals at {P j } from each position of the array be {a,-.exp o.,-}, {b,-.exp β,-} respectively. Then the magnitude of the complex difference summed over the two sets after phase shifting of the second set by θ, is given by: E = Σ (a,-.exp α,- - b,-.exp (β,--θ) ) i = Σ (a,- 2 + b,- 2 - 2a,-b,- cos (αj-β,-+θ) 1) i Differentiating E wrt θ and putting the sum equal to zero gives : tan θ = - Σ a sin(c -β j ) /Σ a,-^ cos(o. j -β,) 2) i i The value of θ which minimises the complex difference between the two sets should also maximise the constructive interference between the two images. After phase shifting the composite signals for all pixels in the second image by, the two sets of composite signals can be added as before. The same procedure extends to three or more successive images, taken two at a time. Although a modified algorithm which simultaneously determines the sequence of n-l unknown phase shifts for n images could be used instead. The number n is limited by the number of times the same pixel is insonified as the platform moves. If the actual source signature emitted at each ping can be measured or estimated in any manner, then the required phase-shifts can be measured directly and applied immediately to the data. 4B.3.4 Corrrection for Errors in Estimating the Position of the Array Reference Point Small unknown positioning errors (d x ,d y ,d z ) in locating the reference point of the array in space have a similar affect to phase errors in the source pulse. Then the region imaged for each pixel is almost unaffected by the error, but the errors in the computed time-delays destroy the constructive phase interference between images required for successful synthetic-aperture imaging. Even a large positioning error which is systematic from ping to ping does not affect the phase-coherence. Provided the random errors are of the same order as the acoustic wavelength, they can be corrected in a similar manner to 4B.3.3. Except in the near-field where the curvature of the acoustic wavefront must be considerd, the time-delay for each transducer is equally affected by each component d x ,d y ,d z of the displacement, hence producing a phase-shift in the composite signal. The calculation to determine the unknown displacement should therefore be carried out with a selected subset of the image pixels {P,-}, which also excludes near-range pixels. Each component of the unknown array displacement must be resolved along the vector to each pixel, and converted to a phase shift. This complicates the expressions in 1,2 but does not change the principle. As displacement components along each axis, d x ,d y ,d z resolve differently, all components required can be minimised simultaneously with each other. It is convenient to correct first for any phase change between successive source signals. When the unknown displacement has been estimated, the position of the platform reference point in space is corrected, and composite signals for all pixels can be calculated or recalculated. The synthetic aperture calculation is then carried out as described earlier. 4B.3.5 Wideband signals The method of section 4B.3.2 extends immediately to wideband signals with more than one spectral component processed. Note that proportionally more data has to be stored in the arrangements of Figs 3A,3B. 4B.3.6 Correction for phase shifts in wideband pulse The method of Sec. 4B.3.3 extends immediately to wideband pulses, since the phase change in each spectral component f m in Eq Ala,A2a,A3 of Appendix A can be found independantly of other spectral components. 4B.3.7 Wideband signals - correction for array displacement The method of Sec. 4B.3.4 can be extended to wideband signals in different ways, for example: i) only one spectral component is used to determine the axial components of the unknown displacement . ii) the difference minimisation for each axial component is carried out using a difference function, similar to (1) which is also summed over all spectral components. The above phase and position correction techniques rely on preserving phase information in the partially processed image data, as in Options A and B (Figs 3A,3B) . 4B.4 DOPPLER SHIFTED SIGNALS AND DOPPLER DISCRIMINATION The Doppler shift for any particular pixel on the ground depends on the array location in space, and therefore changes from one pulse to the next. Hence if the change in Doppler shift is significant, it is necessary to carry out match-filtering for the particular pulse before combining the image data. This rules out Option A (Fig 3A) . Synthetic-aperture imaging may be designed to exploit frequency discrimination in echoes arriving from different locations on the ground. The methods of synthetic-aperture processing given above still apply, but the filter set used for spectral estimation in step c(i) should be designed for maximum resolution in the frequency domain. The optimisation technique given in Sec.4A.4 is no longer relevant, and standard window functions such as the Hanning Envelope can be used with the maximum number of spectral components rather than the minimum. 4B.5 PHASE-INCOHERENT ECHO If the transmission of sound in the medium at the selected frequency range is such that there is no phase- coherence between successive echoes, then Option D, Fig 3D, can be used to generate an image averaged over a number of pulses. There are then available image enhancement techniques which rely on inverting for the point-spread function. There is also disclosed herein: a method of acoustic imaging as hereinbefore described or otherwise in which the set of time delays to the receiver transducers is compensated for motion of the insonifier and receiver transducers in such a way as to stabilize the set of image pixels in space and generate an image directly in a ground coordinate system. In this case, additionally the repeated imaging of a subset of pixels of images derived from successive insonification pulses after lateral movement of the receiver array may be used to generate a synthetic-aperture image of such pixels. Also in this case, additionally the repeated imaging of a subset of pixels in images derived from successive insonification pulses after movement of the receiver array in any direction may be used to increase the signal-to-noise ratio at such pixels, and hence generate image improved for standard deblurring processing. 5. LIST OF DRAWINGS Fig 1 Simplified schematic diagram showing basic processing with negligible Doppler Shift; Fig 2a Comparison of compressed output pulses using Hanning window and a shorter filter with fewer spectral components using an optimised window; Fig 2b Optimised envelope; Fig 3a Comparison of compressed output pulse using single spectral component and optimised window function, with match-filtered pulse; Fig 3b Similar comparison using three spectral components; Fig 3c Optimised window functions for one and three spectral components; Fig 4 Options for combining image data in synthetic aperture computation; Fig 5 System block diagram; Fig 6a,b Block diagram of processing arrangements; Fig 7a,b Block diagrams for synthetic aperture processing. 6. DESCRIPTION OF PREFERRED EMBODIMENTS 6.1 SYSTEM OVERVIEW The overall system consists of four main modules: a) Source Pulse Generation b) Acoustic Projector and Receiver c) Data Acquisition d) Processing Position and attitude sensors for the Acoustic Projector and Receiver may be required to provide information to the Processing Module. Fig 5 is a block diagram illustrating the system. This consists of: * a Pulse Transmitter 1 capable of generating repeated sonic or ultrasonic pulses with the required waveform, * an Acoustic Projector and Receiver 2 capable of launching the required pulse in the required direction, and receiver echoes of this pulse from the required direction. Both projector and receiver consist of one or more transducers of conventional type. The same transducers may be used for both transmission and reception. Otherwise the module may be split mechanically into a Projector means 2a, and a Receiver means 2b. * a Data Acquisition means 3 is adapted to amplify, digitize, and sample the signals received at the set of Receiver transducers. * the Processing means 4 processes the samples generated by the Data Acquisition Means 3 to create the required image, and contains storage means as necessary for this computation. The Source Pulse Generator 1 may be of conventional type and will not be described further herein. 6.2 ACOUSTIC PROJECTOR AND RECEIVER This may take different forms depending on whether the application is ultrasonic imaging in air, or hydracoustic imaging at different frequencies. The set or sets of one or more acoustic transducers used for transmission and reception may be organized in a one- dimensional array or a two-dimensional array, or may be incorporated in the outer surface of a ship' s hull or underwater vessel. The number of receiver transducers is at least two, unless processing for synthetic-aperture imaging is carried out in means 4 , when the number can be reduced to one. The set of one or more transducers used for projection is required to insonify at least the region in space which is required to be imaged with each transmitted pulse. Power is conserved, and artefacts are reduced, if the projector array is designed to minimise the additional region insonified. The projector transducers may be arranged so as to project a narrow fan-beam in a plane so as to define an image area in the same plane. The set of one or more transducers used for reception may be designed to select image points in two or three dimensions depending on the arrangement of transducers. 6.2 DATA ACQUISITION The digitizer module contains means to access echoes received at each individual receiver transducer in means 2 above. It comprises: a) a front-end amplifier for each transducer, which includes a filter to limit the frequency range of the echoes to the required frequency range, which is almost always the frequency range of the source pulse. b) a sampling-digitizer unit consisting of one or more analog-to-digital conversion electronic circuits, which may also include further signal amplification as a function of echo time (time-varying-gain) . The transducer signals may be multiplexed before or after digitization, or even processed separately in a parallel implementation of the Processing means 4. 6.3 MATCH-FILTER PROCESSING Fig 1 gives a general block diagram for the basic image generation computation. The processing in individual blocks varies in detail depending on the specific application but the framework remains the same. This schematic diagram does not include the additional processing required for synthetic-aperture imaging. An additional processing step involving a search in the vertical direction is required for bathymetric measurement . The basic computation has already been given in Sections 4A.2, 4A.3 and is defined mathematically in Appendix A. The preferred embodiment is the use of a subset of Fourier components (Eq Ala,A2a, All) in conjunction with an optimised window function designed as described in Section 4A.4. The length of the window depends on the pulse length and the shape of the pulse envelope. A safe value is the length containing 90% of the pulse energy, but shorter lengths can be used for short-range imaging where electronic noise is not a limitation. The number of spectral components can be as few as 5 with a frequency modulated source chirping over a 4:1 frequency range, and as few as 3 for a frequency-modulated source chirping over a 1.5:1 frequency range. For a narrowband source with a single carrier frequency, only one spectral component equal to the carrier frequency is required. The computation can be implemented in a wide variety of ways, ranging from Fig 6a, in which all transducer samples are stored in one memory module, which is then accessed by a single processer unit, to Fig 6b, in which each transducer has its own associated memory and processer for local spectral estimation, which is independant of the pixel being imaged. Additional processers are used for the pixel- dependant processing, viz. time-delay computation, generation of the composite signal, and match-filtering. 6.4 TIME-DELAY COMPUTATION It may be convenient to generate the image in a coordinate system which moves with the Acoustic Transmitter and Receiver. In this case the time-delays for all pixels in the required image and all Receiver Transducers can be wholly or partly precomputed and stored in a Look-Up-Table. In other situations, and particularly for Synthetic-Aperture Imaging, the time delays must be computed for an image generated in a coordinate system stabilized in space. In that case the time-delays for all pixels in the image and all Receiver Transducers must be recomputed whenever the Acoustic Transmitter and Receiver has moved between pulses. For most sonar applications, the Taylor Series approximation to the time-delay computation given in Appendix B is sufficiently accurate. The full geometrical computation may be required for medical ultrasonic and non- destructive testing applications when the range to the target area is similar to the dimensions of the acoustic aperture. It should be noted that additional sensors are required ■ to generate time-delays for a coordinate system stabilized in space, namely a positioning system, and an attitude measuring system. Additional sensors may also be used to estimate Doppler Shifting due to movement of the Transducer Array. 6.5 SYNTHETIC APERTURE PROCESSING The processing sequence is illustrated in Fig 7, where an additional step is added between generation of the composite signal for each pixel, and match filtering. This step is shown as carried out in a separate processing module, which is convenient although not necessary. The image data handed over to the Synthetic Aperture Module consists of the composite signal for each pixel, namely the complex value for each spectral component used (Option A in Sec. 4B.3.2) or the partially or wholly processed match-filtered signals (Options B,C,D) . The Synthetic Aperture Module stores such images generated from the last n pings (where n depends on a number of factors including the transmitter beamwidth) , and carries out any of the necessary computations given in Sec. 4B.3.3, 4B.3.4, 4B.3.6, 4B.3.7 to correct for phase-changes in the source signature, and errors in estimating the position of the acoustic platform reference point. The last n sets of pixel values signals are then combined to give a combined image for the synthetic aperture, and match-filtering is completed as defined in Sec 4B.3.2. 7. CHIRP (SWEPT-FREQUENCY) AND OTHER SOURCES In the case of a chirp (linear swept-frequency) source, and other sources with a balanced spectrum, it is possible to use direct quadrature match filtering in step (ii) of 4.A.2. The phase-shift used to compensate for a given small time-delay in step (iii) is computed for the centre frequency of the signal. The method of step 4A.4 can be applied to generate optimum swept-frequency kernels which are shorter than the pulse length. Optimisation can also be used to generate a kernel giving a wider peak in the range response in order to image a large insonified area at lower resolution. REFERENCES 1. "Processing directly sampled radar data": Waters W.M. et al, IEEE Int. Radar Conf. , Arlington (May 1985) pp.195-217 2. "Digital interpolation beamforming for low-pass and band¬ pass signals": Pridham R.G. and Mucci R.A. , Proc.IEEE, Vol 67, (June 1979) pp.904-919 3. "Shifted sideband beamformer" : Pridham R.G. and Mucci R.A. IEEE Trans, om ASSP, Vol 27. (Dec. 1979 ) pp.713-722 4. "Digital time-delay beamforming with interpolated signals": Ries S., Proc. European Conf. on Underwater Acoustics, Luxembourg, (Sept. 1992) Ed. M. Weydart, Elsevier Applied Science 1992, pp.594-689 5. "Method and apparatus for acoustic holographic imaging in marine and other acoustic remote sensing equipment": Shippey G.A. and McHugh R. Int Patent Application WO 92/00584, 9th Jan.1992. 6. "Digital Synthetic Aperture Radar Technology": Kirk J.C., IEEE Int. Radar Conf. (1975) 7. "Review of synthetic aperture radar", Proc. IEEE (May 1978) pp.563-583 8. "A real-time synthetic aperture digital acoustic imaging system": Bennet S., Peterson D.K., Corl D. and Kino G.S., Acoustic Imaging, Vol 10,pp.669-692, Plenum Press, New York 1981 9. "Extension of synthetic aperture radar techniques for undersea applications": Zacharia M.E., Chatillon J. and Bouhier M.E., IEEE J. Oceanic Eng. Vol.oe-4 No.2 (April 1979) pp.60-64. 10. "Navigation inaccuracies in synthetic aperture sonar; simulations and experimental set-up": Chatillon J. , Zacharia M.E. and Bouhier M.E., Undersea Defence Technology (UDT 92) , london UK, (June 1992) pp.553-557 APPENDIX A: FORMULATION OF THE PULSE-COMPRESSION ALGORITHM Al Forming the Composite Signal from Sampled Data Echoes are received at an array of K transducers, sampled at interval s, and stored in space-time memory. To form the composite signal, windows of length L samples are used to select sets from each tranducer sequence, centred on the nearest sample to the required delay time for that transducer. These sets are Fourier transformed and any residual fractional time delay is corrected by phase- shifting in the frequency domain. To simplify the notation, define the nearest sample to the required centre as x k 0 in the sequence {x k#n } received at the k' th transducer. Fourier components are given by: HL-l F k r = Σ x kj i w,-exp (2ττj . ri/L) (Al ) i = -iff. for r = - L . . HL- 1 , where {w,-} is some real-valued window function; Let the residual fractional time delay be τ k , where |τ k | ≤ ±5_s. Then each frequency component can be phase-shifted, using: k ,r = F k# r exp ( 2τrj . rτ k /L) (A2) In principle it is now possible to obtain the interpolated set of shifted samples by inverse Fourier transform of (A2) , although this step is not required. The accuracy of interpolation would then be seen to depend on the choice of window function, w,-. Fourier components of the composite signal are given by: K K F'p = Σ F' k/P = Σ F k#r exp(27rj .rτ k /L) , r=-._L.. L-1 .. (A3) k=l k=l A2. Match Filtering Match-filtering is carried out using spectral components of the source signature {S J }, determined with the same window function. These components are given by: ML-1 S r = Σ s,-Wjexp (27rj .ri/L) (A4) i = - L The compressed composite signal is then given by: C r = F' r S r , r = - L ML-1, (A5) ML-1 c, = 1/L Σ C r exp ( -2 rj . ri/L) (A6 ) r=-ML At the centre of the window i=0, and ML-1 c 0 = 1/L Σ C r (A7) r= -ML Write: F' r = G'.+JH' r , S r = P r +jQ r , C r = A r +jB r , c,-= a f +jb,- Then from (A5) C r = A r +jB r = (G' r P r -H' r Q r )+j (G'-Q-÷H'-P-) (A8) Since the compressed pulse is real, {c,-} can be replaced by {aj}. Also Ar mu st be symmetric and Br antisymmetric in r. Hence from (A7) : ML-1 a 0 = 1/L (A 0 + A j _ L + Σ 2A r ) (A9a) r=l The required signal at each pixel is the instantaneous power in the complex envelope of the compressed pulse {ci}. This envelope is obtained by replacing the Ar with the Cr in (A9) to get: ML- 1 c 0 = 1 /L ( C 0 + C j _ L + Σ 2C r ) (A9b) r=l with each Cr given by (A8) . The instantaneous power E 0 is then: E 0 = c 0 c 0 * (A10) As the centre of the time window traverses the echo, a 0 ,c 0 in (A9) give a signal related to the match-filtered response. For echoes which are delayed copies of the source, the FFT relationship (A5) only holds when the window is at least twice the pulse length and wholly contains it. As the compressed pulse leaves the window, the error gets worse. However {w,-} can be designed to give a good approximation to the ideal match-filter response as the window traverses the source pulse. Note that the expected inverse Fourier Transform is not required. A3. Reduced Filter Set The processing load can be reduced by using only a subset of M Forier spectral components f m chosen to span the signal bandwidth, and hence the echo bandwidth, as evenly as possible. fo = = r-JL = -r m /L m = 1..M The DC component f 0 can be set to zero provided the window length is reasonably long, since hydroacoustic echo samples should average to zero. The Nyquist spectral component is also not required. Then Equations (A1,A2) become: ML-1 F k , m = E x kιl -w 1 -exp(2πj.f πn -) (Ala) i = -ML F* k . m = F k,m exp(27rj.f m T k ) (A2a) for m = -M..M And (9) becomes: M M a 0 = 1/L ( Σ 2A,,, ) , c 0 = 1/L ( Σ 2C m ) (All) m=l m=l With this reduced set of spectral components, the choice of window function becomes more important both for accurate time-shifting, and for good match filtering, as the number of spectral components M is reduced. Appendix B: Taylor Series Approximation to Time Delay When imaging in a frame of reference which moves with the sonar platform, it is possible to precompute a "Time-Delay Look-Up Table" giving the time delay between each pixel point in space and each transducer. If the frame of reference is fixed in space, and moves with respect to the platform, this precomputation does not appear to be feasible. We therefore look for an approximate computation of each time delay which is sufficiently cheap to execute in real time. Assuming that the primary purpose of the sonar is sidescan survey, and bathymetric precision is secondary, the velocity of sound in the water column can be taken as constant, so that time delays are directly proportional to distances. It then simplifies the imaging computation if time delays are generated in units of the sampling period. Then the integer part of the time delay can be used directly to index through store to select the required in-phase and quadrature frequency components, while the fractional part can be used to phase shift these components, using the spectral frequency normalised by the sampling frequency. Conversion to the required units is easily built into the time-delay computation, and will be ignored in the following discussion. Suppose that a coordinate system is defined which is fixed to the sonar platform, in fact with origin is at the centre of the sonar array of interest. In this coodinate system, consider a transducer with coordinates (u,v,w) , and a pixel point in space with coordinates (U,V,W) . The distance r from the transducer at (u,v,w) to the pixel point at (U,V,W) is given by: r = /( (u-U) ~ + (v-V) ~ + (w-W) 2 ) (Bl) If we assume that u,v,w << R, where R = (U 2 +V 2 +W 2 ) . then r can be expanded in the Taylor series : /\r = R + \r, where l r = - (Uu + Vv + Ww) R1 + ( (V 2 +W 2 )u 2 +(W 2 +U 2 )v 2 +(U 2 +V 2 )w 2 + UV.uv+VW.vw+WU.wu)R-3 + ... ... (B2) R is simply the distance from the pixel point to the origin, or reference point on the array. The first term in B2 is the far-field approximation in which the differential delay to a given transducer is obtained by resolving the (u,v,w) coordinates along the radial line from the reference point to the pixel point in space. The second term is the quadratic approximation often used for dynamic focus computations. In the time delay computation, the set {Λ.r} of differential delays between the origin and particular transducers is required with much greater accuracy than R itself, since an error in R merely displaces the pixel slightly in space, whereas the accuracy of the diffential delays determine the sharpness of imaging focus. Also the r are much smaller. The Taylor series allows the two computations to be carried out with different precision. Incidently a range search over a small interval can be carried out by varying R and leaving the {/\r} constant. There is an important special case, mainly relevant to narrow-band arrays, where the receiver array is a 2D matrix of evenly spaced transducers, and all transducers lie in the plane w=0. Then for the transducer at (mD,0.nD) , where D is the spacing /\r(m,n) - - (Urn + Wn) d + ((V 2 W 2 )m 2 + (U 2 +V 2 )n 2 + UW.mn)d 2 /R .... (B3) Write f = Ud = UD/R, g = Vd = VD/R, h = Wd = WD/R, .... (B4) to get: \r(m,n) « - (fm + hn) + ((g 2 +h 2 )m 2 + (f 2 +g 2 )n 2 + fg.mn) /R When carrying out the imaging computation, the parameters: R, f,g,h, f/R,g/R (and in general h/R) ... (B5) need to be evaluted once for each pixel. A Cartesian-to- polar look-up table can be used to speed up various computations, including the one required here to generate R from U,V,W. The quadratic expression Λr(m,n) needs to be evaluated once for each transducer. For a given m, the differential time delay between adjacent transducers, Λr(m,n+1) - r(m,n) is linear in n. Similarly for given n, the differential time delay is linear in m. This allows the set of time delays for any line of adjacent transducers to be generated rapidly. Essentially the same approximation is valid if the surface containing the set of transducers is a shallow dish, or quadratic surface. The chirp situation requires a much smaller number of transducers, but no assumption can be made about their location; for example it could be an advantage to be able to position each transducer independantly on the vehicle. In that case the expression (B2) needs to be evaluated for the (u,v,w) of each transducer, using a similar set of parameters to (B5) .

Claims: CLAIMS 1. An acoustic imaging method for marine survey and other purposes comprising the steps of : insonifying a target area by periodic acoustic pulses; detecting reflections of said pulses by a set of at least two receiver transducers, which transducers • generate output signals in response thereto, wherein further the signals are: a) sampled in time at a predetermined rate during an interval between said pulses, b) converted from analog to digital form, c) processed by means of a set of one or more optimised digital quadrature filters so as to generate a composite signal for each pixel in the insonified target area requiring to be imaged, and d) match-filtered in the frequency domain with an estimated source pulse signature. 2. An acoustic imaging method for marine survey and other purposes wherein a target region is insonified by periodic acoustic pulses, reflections of said pulses are detected by at least two transducers which generate output signals in response thereto, and said ouput signals are processed so as to produce an image of all or part of the insonified region, said image comprising a two or three-dimensional array of pixels, each corresponding to a point in the insonified region, and the intensity of the pixel representing the strength of the pulse reflected from the neighbourhood of the said corresponding point, comprising the steps of: a) sampling the output signals from each of said transducers at a predetermined rate during the period between said transmitted pulses; b) digitizing ' said samples; c) for each pixel of the image,. i) selecting a corrsponding set of samples from each transducer, the selection of the sample set being determined by the predicted time of flight of a transmitted pulse to the point in the insonified region corresponding to the pixel and back to the particular transducer in the array; ii) estimating the in-phase and quadrature coefficients for one or more frequency components selected from the bandwidth of the transmitted pulse, and present in each sample set, by convolution of the sample set with a digital filter set consisting of one or more pairs of digital filters, in which each pair of digital filters is defined by a sine and cosine function at the required frequency multiplied by a common modulation function known as a window function; iii) correcting the in-phase and quadrature coefficients for each frequency component by phase shifting with the effect of precisely aligning the sample set with the required time of flight; iv) combining the phase-shifted coefficients for each frequency component for all transducers to generate the corresponding coefficients for a composite signal; v) determining or predetermining the spectral components of the source signal by filtering the recorded or estimated source pulse with the same digital function set used for the echo, centering the window function at or near the centre of the pulse; vi) obtaining the spectral components of the match- filtered composite signal from the cross-products of spectral components of the composite signal with such spectral components of the source signal; vii) adding the spectral components of the match- filtered signal to obtain the in-phase and quadrature components of the match-filtered signal; viii) deriving the intensity of the pixel from the in- phase and quadrature components of the match-filtered composite signal; d) predetermining the window function for the frequency components used in steps (ii) and (v) either by minimising an error function which may include the predicted alignment errors in step (iii) , the predicted deviation from ideal match-filtering in steps (vi) , (vii) and (viii) , or by other means, wherein steps (v) - (vii) are omitted if only a single frequency component is selected. 3. A method as claimed in claim 1 wherein the times of flight are obtained for a two or three-dimensional array of pixels fixed in space by mean of a computation using the measured position and attitude of the receiver array in space. 4. A method as claimed in either of claims 2 or 3 wherein: a) the periodic pulses are substantially identical; b) the random error in the computation of array position in claim 3 does not exceed a small fraction of the acoustic wavelengths used; c) the signals derived in steps c(iv) , c(vi) , c(vii) or c(viii) are combined together before carrying out any remaining steps of step c in claim 2. d) step d of claim 2 is not necessary to this claim 5. A method as claimed in claim 4 except that: a) the periodic pulses are identical apart from phase- shifts in the spectral components of successive pulses; b) phase-shifts in the spectral components of successive pulses are estimated as described in Section 4B.3.3 and used to correct the signals derived from successive pulses before combining them as in steps (c) of claim 4. 6. A method as claimed in claim 5 except that : a) the random error in the computation of the array position in claim 3 may be of a similar magnitude to the acoustic wavelengths used; b) errors in the computed position of the array are estimated as described in Section 4B.3.4 and used to correct the signals derived from successive pulses before combining them as in steps (c) of claim 4. 7. An acoustic imaging method for marine survey and other purposes wherein a target region is insonified by periodic pulses, reflections of said pulses are detected by at least two transducers which generate output signals in response thereto, and said output signals are processed so as to produce an image of all or part of the insonified region, said image comprising a two ot three-dimensional array of pixels, each corresponding to a point in the insonified region, and the intensity of the pixel representing the strength of the signal reflected from the neighbourhood of said corresponding point, comprising the steps of: a) determining the composite time-delayed echo for the set of receiver transducers in one or more particular directions by standard time-delay beamforming techniques; b) sampling and digitizing such an echo; c) for each beam direction and each required range, i) selecting a corresponding set of digitized samples, the selection of the sample set being determined by the predicted time of flight of a transmitted pulse to the point in the insonified region corresponding to the pixel and back to the centre of the array; ii) estimating the in-phase and quadrature coefficients for one or more frequency components selected from the bandwidth of the transmitted pulse, and present in each sample set by convolution of the sample set with a digital filter in which each pair of digital filiters is defined by a sine and cosine function at the required frequency multipled by a common modulation function known as a window function; iii) determining or predetermining the spectral components of the source signal by filtering the recorded or estimated source pulse with the same digital filter set used for the echo, centering the window function at or near the centre of the pulse; iv) obtaining the in-phase and quadrature components of the match-filtered composite signal by adding the cross- products of spectral components of the composite signal with such corresponding spectral components of the source signal; v) deriving the intensity of the pixel from the in- phase and quadrature components of the match-filtered composite signal; vi) predetermining the window function used in steps (ii) and (iii) either by minimising an error function which may include deviation from ideal match-filtering and other deviations or errors, or by other means, wherein steps (iii) , (iv) can be omitted if only a single frequency component is selected. 8. A method as claimed in any previous claim wherein steps c(i) and c (v) are modified to allow for change in the time delay to the pixel in the echo due to movement of the set of receiver transducers with respect to the source of the echo, and Doppler Shift in the echo, by applying the same Doppler Shift to the source pulse used in match filtering, as follows: i) for each pixel to be imaged the closing velocity to the target pixel is estimated from the measured speed and direction of motion of the receiver array and the estimated speed and direction of motion of the target pixel; ii) the recorded or estimated source pulse is digitally modified to allow for Doppler Shift in the waveform due to the closing velocity; iii) the spectral components of such modified source pulses are determined or predetermined by filtering with the same digital filter set used for the echo, centering the window function at or near the centre of the modified pulse. 9. An acoustic imaging method for marine survey and other purposes comprising the steps of: insonifying a target area by periodic acoustic pulses; detecting reflections of such pulses by one or more receiver transducer(s) , which transducer(s) generate a respective output signal (s) in response thereto, wherein the signal (s) is/are: a) sampled in time at a predetermined rate during an interval between said pulses; b) converted from an analog to digital form; c) processed so as to generate a composite acoustic signal for each pixel in the insonified target area required to be imaged; wherein further the processed signal is modified to allow for Doppler shift in the echo due to movement of the set of receiver transducers with respect to the source of the echo, by applying the same Doppler Shift to the source pulse signature used for match-filtering, as follows: i) for each pixel to be imaged the closing velocity to the target pixel is estimated from the measured speed and direction of motion of the receiver array and the estimated speed and direction of motion of the target pixel; ii) the recorded or estimated source pulse is digitally modified to allow for Doppler Shift in the waveform due to the closing velocity; iii) the spectral components of such modified source pulses are determined or predetermined by filtering with the same digital filter set used for the echo, centering the window function at or near the centre of the modified pulse. 10. A method as claimed in any of claims 2 to 9, wherein a single quadrature filter is used in step (ii) of claim 2 which is just the source signature and its quadrature, possibly optimised for shorter kernel length or different compressed pulse shape. 11. A method as claimed in claim 10, wherein the single frequency used to compute the phase-shift in step (iii) of claim 2 is the centre frequency of the source signal, modified by Doppler shift of the echo if significant. 12. A method of acoustic imaging as claimed in any of the previous claims or otherwise in which the set of time delays to the receiver transducers is compensated for motion of the insonifier and receiver transducers in such a way as to stabilize the set of image pixels in space and generate an image directly in a ground coordinate system. 13. A method as claimed in claim 12 in which additionally the repeated imaging of a subset of pixels in images derived from successive insonification pulses after lateral movement of the receiver array is used to generate a synthetic- aperture image of such pixels. 14. A method as claimed in claim 12 in which additionally the repeated imaging of a subset of pixels in images derived from successive insonification pulses after movement of the receiver array in any direction is used to increase the signal-to-noise ratio of such pixels, and hence generate an image improved for standard deblurring processing. 15. An acoustic imaging apparatus for marine survey and other purposes comprising: means for insonifying a target area by periodic acoustic pulses; means for detecting reflections of said pulses comprising a set of at least two receiver transducers, which transducers generate output signals in response thereto, wherein further the signals are: a) sampled in time at a predetermined rate during an interval between said pulses, b) converted from analog to digital form, c) processed by means of a set of one or more optimised digital quadrature filters so as to generate a composite signal for each pixel in the insonified target area requiring to be imaged, and d) match-filtered in the frequency domain with an estimated source pulse signature. 16. Apparatus for use in an acoustic imaging method as claimed in any of claims 1 to 14.

Inventors: SHIPPEY GEOFFREY, SHIPPEY, GEOFFREY
Applicants: QUEENSFERRY CONSULTANTS LIMITE, SHIPPEY GEOFFREY, QUEENSFERRY CONSULTANTS LIMITED, SHIPPEY, GEOFFREY
Application year: 1995
Main classification: G01S15
IPC codes: G01S15