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Technical Review
Beamforming No. 1 2004
Previously issued numbers of Brüel & Kjær Technical Review
Contents
Abstract
Introduction
Theory
Fig. 1. (a) A microphone array, a far-field focus direction, and a plane wave incident from the focus direction.
Fig. 2. A plane wave, with wave number vector k , incident from a direction different from the focus direction.
Fig. 3. Contour plot of the Array Pattern, eq.
Fig. 4. An example of a planar 66-channel beamformer array and its equivalent circular aperture (---).
Fig. 5. The curves show the beamformer output,
Fig. 6. The variation of the ratio between off-axis and on-axis resolution as given by eq. (16)
Fig. 7. Comparison of the aperture smoothing function, eq. (12),
Fig. 8. The sidelobe level profile, Wp , eq. (17)
Finite Focus Distance
Fig. 9. In near-field focusing,..................
Array Design
Fig. 10. Comparison of the output.............
Regular Arrays
Fig. 11. Examples of regular and.............
Fig. 12 Graph (a) illustrates the side-lobe structure............
Fig. 13 plot of the array pattern for a uniform linar..............
Fig. 14 Comparison of the Maximun Sidelobe Level............
Irregular Arrays
Optimised Arrays
Fig. 15. Wheel Array.
Fig. 16. Example of 90-channel wheel array................
Instrumentatation
Fig. 17. Contour plots simulation results of source reconstruction.....
Fig. 18. Contour plots showing simulation......
Data Acquisitions System and Beamforming Calculations
Practical Aspects of Designing and Using Beamformer Arrays
Table 1. Beamformer properties at 30º opening angle
Application Examples
Fig. 19. Car in a wind-tunnel at 130 km/h wind speed
Fig. 20. Mobile crane hoisting at maximum load
Fig. 21. Averaged 6.3 kHz, 1/3-octave band for a car engine
Fig. 22. Calculation Setup
Conclusions
Fig. 23. Non-Stationary beamforming. Stationary 2000 RPM. Shaft angle averaging in intervals of 5°
Appendix: The Cross-spectral Imaging Function
Fig. A1. For a source in the far field,......
Appendix: Resolution
References
Previously issued numbers of Brüel&Kjær Technical Review
BV0056-11_TR_Cover2004.qxd 23-03-2004 13:33 Page 1 TECHNICAL REVIEW Beamforming 1 2 6 2 – 7 0 0 0 N S S I 1 1 – 6 5 0 0 V B No.1 2004 HEADQUARTERS: DK-2850 Nærum · Denmark Telephone: +45 4580 0500 · Fax: +45 4580 14 05 www.bksv.com · info@bksv.com
bv005611.book Page i Tuesday, March 23, 2004 12:46 PM Previously issued numbers of Brüel & Kjær Technical Review 1 – 2002 A New Design Principle for Triaxial Piezoelectric Accelerometers Use of FE Models in the Optimisation of Accelerometer Designs System for Measurement of Microphone Distortion and Linearity from Medium to Very High Levels 1 – 2001 The Influence of Environmental Conditions on the Pressure Sensitivity of Measurement Microphones Reduction of Heat Conduction Error in Microphone Pressure Reciprocity Calibration Frequency Response for Measurement Microphones – a Question of Confidence Measurement of Microphone Random-incidence and Pressure-field Responses and Determination of their Uncertainties 1 – 2000 Non-stationary STSF 1 – 1999 Characteristics of the Vold-Kalman Order Tracking Filter 1 – 1998 Danish Primary Laboratory of Acoustics (DPLA) as Part of the National Metrology Organisation Pressure Reciprocity Calibration – Instrumentation, Results and Uncertainty MP.EXE, a Calculation Program for Pressure Reciprocity Calibration of Microphones 1 – 1997 A New Design Principle for Triaxial Piezoelectric Accelerometers A Simple QC Test for Knock Sensors Torsional Operational Deflection Shapes (TODS) Measurements 2 – 1996 Non-stationary Signal Analysis using Wavelet Transform, Short-time Fourier Transform and Wigner-Ville Distribution 1 – 1996 Calibration Uncertainties & Distortion of Microphones. Wide Band Intensity Probe. Accelerometer Mounted Resonance Test 2 – 1995 Order Tracking Analysis 1 – 1995 Use of Spatial Transformation of Sound Fields (STSF) Techniques in the Automative Industry 2 – 1994 The use of Impulse Response Function for Modal Parameter Estimation Complex Modulus and Damping Measurements using Resonant and Non- resonant Methods (Damping Part II) 1 – 1994 Digital Filter Techniques vs. FFT Techniques for Damping Measurements 2 – 1990 Optical Filters and their Use with the Type 1302 & Type 1306 1 – 1990 The Brüel & Kjær Photoacoustic Transducer System and its Physical 2 – 1989 STSF — Practical Instrumentation and Application Digital Filter Analysis: Real-time and Non Real-time Performance 1 – 1989 STSF — A Unique Technique for Scan Based Near-Field Acoustic Holography Without Restrictions on Coherence (Damping Part I) Photoacoustic Gas Monitors Properties (Continued on cover page 3)
bv005611.book Page ii Tuesday, March 23, 2004 12:46 PM Technical Review No. 1 – 2004
bv005611.book Page iii Tuesday, March 23, 2004 12:46 PM Contents Beamforming .......................................................................................................... 1 J.J. Christensen and J. Hald Copyright © 2004, Brüel & Kjær Sound & Vibration Measurement A/S All rights reserved. No part of this publication may be reproduced or distributed in any form, or by any means, without prior written permission of the publishers. For details, contact: Brüel & Kjær Sound & Vibration Measurement A/S, DK-2850 Nærum, Denmark. Editor: Harry K. Zaveri
bv005611.book Page 1 Tuesday, March 23, 2004 12:46 PM Beamforming by J.J. Christensen and J. Hald Abstract This article explains the basic principles of Beamforming, including the main per- formance parameters Resolution and Sidelobe Level. Special attention is given to the influence of array design and to cross-spectral beamforming. Different array designs, including Brüel & Kjær’s newly patented wheel array design, are described and compared, and the basic principle of Brüel & Kjær’s geometry optimisation method is outlined. A new, improved version of cross-spectral beamforming used in Beamforming Software Type 7768 is introduced and its benefits are verified. The article also provides some guidelines for performing good measurements and finally, describes a set of measurements representing typical applications. Résumé Cet article traite succintement du concept d’imagerie par formation de faisceaux, et notamment des principaux paramètres essentiels aux performances de l’antenne que sont la Résolution et le Niveau de lobe latéral. Une attention toute particulière est portée sur l’influence de la forme de l’antenne et sur la formation de faisceaux par approche interspectrale. Diverses conceptions d’antennes, dont l’antenne circu- laire Brüel & Kjær nouvellement brevetée, y sont présentées et comparées; les prin- cipes fondamentaux de la méthode propriétaire d’optimisation géométrique y sont soulignés. Une nouvelle version amendée de l’approche interspectrale implémen- tée dans le Logiciel Beamforming Software Type 7768 est également présentée et ses avantages sont vérifiés. Cet article inventorie par ailleurs les points contribuant à la réalisation de mesures de qualité, pour conclure par la description d’une série de mesures se rapportant à des applications typiques. Zusammenfassung Dieser Artikel erläutert die Grundprinzipien des Beamforming einschließlich der Hauptparameter Auflösung und Nebenmaxima (Sidelobe Level). Besondere Auf- merksamkeit wird dem Einfluss der Array-Konstruktion und dem Beamforming nach dem Kreuzspektrum-Verfahren gewidmet. Es werden verschiedene Array- 1
bv005611.book Page 2 Tuesday, March 23, 2004 12:46 PM Konstruktionen beschrieben und verglichen, darunter Brüel & Kjærs patentiertes Wheel Array. Außerdem wird das Grundprinzip der Geometrieoptimierung von Brüel & Kjær skizziert. Eine neue verbesserte Version des in der Beamforming Software Typ 7768 verwendeten Beamforming nach dem Kreuzspektrum-Verfah- ren wird vorgestellt und dessen Vorteile nachgewiesen. Der Artikel enthält auch Richtlinien zur Durchführung guter Messungen und beschreibt eine Serie von Mes- sungen, die typische Anwendungen repräsentieren. Introduction Planar Near-field Acoustical Holography (NAH) is an established technique for efficient and accurate noise source location [1, 2]. NAH can provide high-resolu- tion source maps on a planar source surface from measurements taken over a regu- lar rectangular grid of points close to the source. The measurement grid must capture the major part of the sound radiation into a half space and therefore com- pletely cover the noise source plus approximately a 45º solid angle. The grid spac- ing must be less than half a wavelength at the highest frequency of interest. Thus, the number of measurement points gets very high when the source is much larger than the wavelength, which always occurs at sufficiently high frequencies. The same problem arises when for some reason it is not possible to measure close to the source. Then, because of the required 45º coverage angle, the measurement area must be very large. In these cases, beamforming is an attractive alternative. Beamforming is an array-based measurement technique for sound-source loca- tion from medium to long measurement distances. Basically, the source location is performed by estimating the amplitudes of plane (or spherical) waves incident towards the array from a chosen set of directions. The angular resolution is inversely proportional to the array diameter measured in units of wavelength, so the array should be much larger than wavelength to get a fine angular resolution. At low frequencies, this requirement usually cannot be met, so here the resolution will be poor. Unlike NAH, beamforming does not require the array to be larger than the sound source. For typical, irregular array designs, the beamforming method does not allow the measurement distance to be much smaller than the array diameter. On the other hand, the measurement distance should be kept as small as possible to achieve the finest possible resolution on the source surface. An important difference between beamforming and NAH is that beamforming can use irregular array geometries, for example, random array geometries. The use of a discrete set of measurement points on a plane can be seen as a spatial sampling 2
bv005611.book Page 3 Tuesday, March 23, 2004 12:46 PM of the sound field. NAH requires a regular, rectangular grid of points in order to apply a 2D spatial DFT. Outside the near-field region, such a regular grid will sup- press spatial aliasing effects very well, if the grid spacing is just less than half a wavelength. When the grid spacing exceeds half a wavelength, spatial aliasing components quickly get very disturbing. Irregular arrays on the other hand can potentially provide a much smoother transition: spatial aliasing effects can be kept at an acceptable level up to a much higher frequency with the same average spatial sampling density. This indicates why beamforming can measure up to high fre- quencies with a fairly low number of microphones. Theory Delay-And-Sum Beamforming for Infinite Focus Distance The principle of Beamforming is best introduced through a description of the basic Delay-and-Sum beamformer. As illustrated in Fig. 1, we consider a planar array of M microphones at locations rm (m = 1, 2, …, M) in the xy-plane of our coordinate system. When such an array is applied for Delay-and-Sum Beamforming, the measured pressure signals pm are individually delayed and then summed [3]: Fig.1. (a) A microphone array, a far-field focus direction, and a plane wave incident from the focus direction. (b) A typical directional sensitivity diagram with a main lobe in the focus direc- tion and lower sidelobes in other directions Plane wave Sidelobe – 30º 0º 30 dB Main lobe 30º ␬ – ␬ (a) – 60º –90º 20 dB 10 dB (b) 60º 90º 040009 3
bv005611.book Page 4 Tuesday, March 23, 2004 12:46 PM b ␬ t, ( ) = M∑ pm t ∆m wm –( m 1= ␬( ) ) (1) where wm are a set of weighting or shading coefficients applied to the individual microphone signals. The individual time delays ∆m are chosen with the aim of achieving selective directional sensitivity in a specific direction, characterised here by a unit vector ␬. This objective is met by adjusting the time delays in such a way that signals associated with a plane wave, incident from the direction ␬, will be aligned in time before they are summed. Geometrical considerations (Fig. 1) show that this can be obtained by choosing: ∆m = ␬ rm⋅ -------------- c (2) where c is the propagation speed of sound. Signals arriving from other far-field directions will not be aligned before the summation, and therefore they will not add up coherently. Thus, we have obtained a directional sensitivity, as illustrated in Fig. 1(b). The frequency domain version of eq. (1) for the Delay-and-Sum beamformer output is: B ␬ x, ( ) = M ∑ m 1= wmPm x( )e – jx∆m ␬( ) = M ∑ m 1= wmPm x( )e jk rm⋅ (3) Here, x is the temporal angular frequency, k ≡ –k␬ is the wave number vector of a plane wave incident from the direction ␬ in which the array is focused (see Fig. 1), and k = x/c is the wave number. In eq. (3) an implicit time factor equal to e jxt is assumed. Because k ≡ –k␬, we can write B(k, x) instead of B(␬, x). Through our choice of time delays ∆m(␬), or equivalently of the “preferred” wave number vector k ≡ –k␬, we have “tuned” the beamformer on the far-field direction ␬. Ideally, we would like to measure only signals arriving from that direc- tion, in order to get a perfect localisation of the sound sources. To investigate, how much “leakage” we will get from plane waves incident from other directions, we now assume a plane wave incident with a wave number vector k0 different from the preferred k ≡ –k␬, Fig. 2. The pressure measured by the microphones will then be: Pm x( ) = P0e – jk0 rm⋅ (4) which, according to eq. (3), will give the following output from the beamformer: 4
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