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(1)

A. Farina, A. Capra

Università di Parma

Strategie Tecnologiche

Centro Ricerche e Innovazione Tecnologica

MICROPHONES ARRAYS

(2)

General Approach

• Whatever theory or method is chosen, we always start with N microphones, providing N signals x

i

, and we derive from them M signals y

j

• And, in any case, each of these M outputs can be expressed by:

i N

1 i

ij

j h x

y 

processor N inputs

M outputs

(3)

Microphone arrays: target, processing

Is the time-domain sampled waveform of a wave with well defined spatial characteristics, for example:

• a spherical wave centered in a precise emission point Psource

• a plane wave with a certain direction

• a spherical harmonic referred to a receiver point Prec

Pre-calculated filters

i N

1 i

ij

j

h x

y 

x1(t) x2(t) x3(t) x4(t)

yj(t)

(4)

Traditional approaches

• The processing filters h

ij

are usually computed following one of several, complex mathematical

theories, based on the solution of the wave equation (often under certaing simplifications), and assuming that the microphones are ideal and identical

• In some implementations, the signal of each

microphone is processed through a digital filter for

compensating its deviation, at the expense of heavier

computational load

(5)

Novel approach

• No theory is assumed: the set of h

ij

filters are derived directly from a set of impulse response measurements, designed according to a least-squares principle.

• In practice, a matrix of filtering coefficients, is formed, and the matrix has to be numerically inverted (usually employing some regularization technique).

• This way, the outputs of the microphone array are maximally close to the ideal responses prescribed

• This method also inherently corrects for transducer deviations and acoustical artifacts (shielding,

diffractions, reflections, etc.)

(6)

The microphone array impulse responses ck,i , are measured for a number of P incoming directions.

…we get the filters to be applied to the

microphonic signals from processing the matrix of measured impulse responses

 

 

 

 

N , P N

, k N

, 2 N

, 1

i, P i,

k i,

2 i,

1

2 , P 2

, k 2

, 2 2

, 1

1 , P 1

, k 1

, 2 1

, 1

c c

c c

c c

c c

c c

c c

c c

c c

C

i=1…N mikes k=1…P sources

cki

Example: synthesizing 0-order shape

(7)

Example: synthesizing 0-order shape

N 1

i ,i0 P i,

N 1 i

i, k 0

,i N

1

i ,i0 2 i, N

1 i

i, 1 0

,i

c h

...

c h

...

c h

c h

We design the filters in such a way that the response of the system is the prescribed theoretical function vk for the k-th source (an unit-amplitude Dirac’s Delta function in the case of the example, as the 0th-order

function is omnidirectional).

So we set up a linear equation system of P equations, imposing that:

Lets call vk the right-hand vector of known results (they will be different for higher-order shapes).

Once this matrix of N inverse filters are computed (for example, employing the Nelson/Kirkeby

method), the output of the microphone array, synthesizing the prescribed 0th-order shape, will again be simply:

N

1 i

0 ,i i

0

x h

y

(8)

• For computing the matrix of N filtering coefficients h

i0

, a least-squares method is employed.

• A “total squared error” 

tot

is defined as:

 

     

 

  

P

1 k

2 k N

1 i

ki 0

i

tot h c v

• A set of N linear equations is formed by minimising 

tot

, imposing that:

) N ...

1 i

( h i 0 0

tot  

System’s least-squares inversion

(9)

System’s least-squares inversion

• For computing the matrix of N filtering coefficients h

ik

, a least-squares method is employed.

• A “total squared error” 

tot

is defined as:

 

 

 

 

  

P

1 k

2 k N

1 i

ki iK

tot

h c v

• A set of N linear equations is formed by minimising 

tot

, imposing that:

) N ...

1 i

( h

iK

0

tot

 

(10)

Kirkeby’s regularization

• During the computation of the inverse filter, usually operated in the frequency domain, one usually finds expressions

requiring to compute a ratio between complex spectra ( H=A/D ).

• Computing the reciprocal of the denominator D is generally not trivial, as the inverse of a complex, mixed-phase signal is generally unstable.

• The Nelson/Kirkeby regularization method is usually employed for this task:

     

      

 Conj D D

D InvD Conj

InvD A

H  

(11)

Spectral shape of the regularization parameter 

• At very low and very high frequencies it is advisable to increase the value of .

H

L

(12)

Critical aspects

• LOW frequencies: wavelength longer than array width - no phase difference between mikes - local approach provide low spatial

resolution (single, large lobe) - global approach simply fails (the linear system becomes singular)

• MID frequencies: wavelength comparable with array width -with local approach secondary lobes arise in spherical or plane wave detection (negligible if the total bandwidth is sufficiently wide) - the global approach works fine, suppressing the side lobes, and providing a narrow spot.

• HIGH frequencies: wavelength is shorter than twice the average mike spacing (Nyquist limit) - spatial undersampling - spatial

aliasing effects – random disposition of microphones can help

the local approach to still provide some meaningful result - the

global approach fails again

(13)

The R.A.I. project

• “Virtual” microphones with high directivity, controlled by a joystick in order to follow in realtime actors on the stage. They should be capable to modify their directivity in a sort of

“acoustical zoom”.

• Surround recordings with microphones that can be modified (directivity, angle, gain, ecc..) in post-production.

AIMS:

(14)

R.A.I. state of art

• The Holophone H2 Pro is a microphone system equipped with 8 capsules placed on a egg-shaped framework. The audio signals are delivered directly in G-format or using an audio mixer.

• The directivity of each Holophone capsule was measured in the

Anechoic Room of “Università’ di

Ferrara” (Italy)

(15)

Holophone polar patterns

(16)

HOLOPHONE PROBLEMS:

• Directivity and angles between single capsules are not changeable in post-processing.

• There isn’t enough separation between sources because of the

low directivity of the capsules. For this reason the probe should

be placed very close to the scene that is object of recordins

(17)

Acoustical measurements on Eigenmike

TM

• Sine-sweep technique was used in order to obtain a flat response for the full-range coaxial woofer.

In this step a Bruel&Kjaer microphone was used.

• With the Inversion Technique of Kirkeby we obtained a filter that should be applied to the sine- sweep.

(1

st

step: source optimization)

(18)

Acoustical measurements on Eigenmike

TM

(2

nd

step: planar measurements)

• A framework was assembled in order to have the center of rotation in axis with the center of the probe. This

framework was placed on a rotating table controlled by the audio soundcard.

• Sine-sweep technique was used in order to

obtain 32 impulse responses of the capsules

for every angle step (72 step = 5°)

(19)

Acoustical measurements on Eigenmike

TM

(3

rd

step: 3D measurements)

• A second framework was assembled in order to have the capability of a 2

nd

order of freedom in the rotation of the probe. Also this framework was placed on a

rotating table controlled by the audio soundcard.

Angular step = 10° Enough for 4

th

order

Complete rotation of elevation…

… for every step

of azimuth

(20)

PROBLEM: the rotation of azimuth is made by hand. This could cause little movements off the rotation center of elevation. This could cause bad results in terms of phase coherence with a non perfect reconstruction of the sound field.

Movements of the acoustical center of the probe in relation to the source, varying the angle of the rotation table

[mm][samples] Estimation of the number of samples

optimal for tha compensation of the error

(21)

[mm]

Position of the rotating table [°]

RESULT: the variation is reduced to 2 mm. This small error becomes relevant for frequencies higher then 170 kHz.

BEFORE AFTER

(22)

Processing of the measurements

SOFTWARE: we used a script in Matlab to derive the directivity of the single capsule of the probe and to implement the “multi-channel Kirkeby Inversion”

Directivity of capsules

(23)

Synthesis of directivities

InvD A

H  

From Kirkeby’s formula we have a matrix of filters (H) to apply to the 32 capsule signals in rder to obtain the desired signal. The desired signal is “forced” by the target function (A).

Omni microphone with our processing

(24)

Second order cardioid

“EM32 VST”

Second order cardioid

“multichannel Kirkeby Inversion”

(25)

Third order cardioid

“EM32 VST”

Third order cardioid

“multichannel Kirkeby Inversion”

(26)

4th order cardioid

“multichannel Kirkeby Inversion”

6th order cardioid

“multichannel Kirkeby Inversion”

(27)

Spherical Harmonics

(28)

The real-time microphone system

(29)

Pointing GUI for the virtual microphones

• Moving the joystick the corrispondent pointer moves

• The pointer increases its dimensions in relation to the directivty

(30)

Linear array

• 16 omnidirectional mikes mounted on a 1.2m aluminium beam, with exponential spacing

• 16 channels acquisition system:

2 Behringer A/D converters + RME Hammerfall digital sound card

• Sound recording with Adobe Audition

• Filter calculation, off-line processing and visualization with Aurora plugins

(31)

Linear array - calibration

• The array was mounted on a rotating table, outdoor

• A Mackie HR24 loudspeaker was used

• A set of 72 impulse responses was measured employing Aurora plugins under Adobe Audition (log sweep method) - the sound card controls the rotating table.

• The inverse filters were designed with the local approach (separate inversion of the 16 on-axis responses, employing Aurora’s “Kirkeby4” plugin)

(32)

Linear array - polar plots

8000 Hz

-30 -25 -20 -15 -10 -5 0 0

5 10 1520 2530

35 40

45 50

55 60

65 70

75 80 85 90 95 100 105 110 115 120 125 130 135 140 150145 160155 170165 175 180 190185 200195 210205 215 220 225 230 235 240 245 250 255 260 265 270 275 280 285

290 295

300 305

310

315320325330335340345350355

250 Hz

-30 -25 -20 -15 -10 -5 0 0

5 10 1520 2530

3540 45

50 55

60 65

70 75

80 85 90 95 100 105 110 115 120 125 130 135 145140 155150 165160 175170 180 190185 200195 210205 220215 225 230 235 240 245 250 255 260 265 270 275 280 285

290 295

300 305

310

315320325330335340345350355

500 Hz

-30 -25 -20 -15 -10 -5 0 0

5 10 1520 25

3035 40

45 50

55 60

65 70

75 80 85 90 95 100 105 110 115 120 125 130 135 140 150145 160155 170165 175 180 190185 200195 205 215210 220 225 230 235 240 245 250 255 260 265 270 275 280 285

290 295

300 305

310 315

320

325330335340 345350 355

1000 Hz

-30 -25 -20 -15 -10 -5 0 0

5 10 1520 25

3035 40

45 50

55 60

65 70

75 80 85 90 95 100 105 110 115 120 125 130 135 140 150145 160155 170165 175 180 190185 200195 205 215210 220 225 230 235 240 245 250 255 260 265 270 275 280 285

290 295

300 305

310 315

320

325330335340 345350 355

2000 Hz

-30 -25 -20 -15 -10 -5 0 0

5 10 1520 25

3035 40

45 50

55 60

65 70

75 80 85 90 95 100 105 110 115 120 125 130 135 140 145 150 160155 170165 175 180 190185 200195 205 210 215 220 225 230 235 240 245 250 255 260 265 270 275 280 285

290 295

300 305

310 315

320

325330335340 345350 355

4000 Hz

-30 -25 -20 -15 -10 -5 0 0

5 10 1520 2530

35 40

45 50

55 60

65 70

75 80 85 90 95 100 105 110 115 120 125 130 135 140 150145 160155 170165 175 180 190185 200195 210205 215 220 225 230 235 240 245 250 255 260 265 270 275 280 285 290

295 300

305 310

315320325330335340345350355

(33)

Linear array - practical usage

• The array was mounted on an X-Y scanning apparatus

• a Polytec laser vibrometer is mounted along the array

• The system is used for mapping the velocity and sound pressure along a thin board of “resonance” wood (Abete della val di Fiemme, the wood employed for building high-quality musical instruments)

• A National Instruments board controls the step motors through a Labview interface

• The system is currently in usage at IVALSA (CNR laboratory on wood, San Michele all’Adige, Trento, Italy)

(34)

Linear array - practical usage

• The wood panel is excited by a small piezoelectric transducer

• When scanning a wood panel, two types of results are obtained:

-A spatially-averaged spectrum of either radiated pressure, vibration velocity, or of their product (which provides an estimate of the radiated sound power)

-A colour map of the radiated pressure or of the vibration velocity at each resonance frequency of the board

(35)

Linear array - test results (small loudspeaker)

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

2 5 0 H z

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

5 0 0 H z

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

1 0 0 0 H z

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

2 0 0 0 H z

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

4 0 0 0 H z

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

- 5 0 - 4 0 - 3 0 - 2 0 - 1 0 0 1 0 2 0 3 0 4 0 5 0

8 0 0 0 H z

(36)

Linear array - test results (rectangular wood panel)

0 1 0 2 0 3 0 4 0 5 0

0 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0

4 6 8 H z

0 1 0 2 0 3 0 4 0 5 0

0 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0

4 6 9 H z

0 1 0 2 0 3 0 4 0 5 0

0 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0

1 3 5 9 H z

0 1 0 2 0 3 0 4 0 5 0

0 1 0 2 0 3 0 4 0 5 0 6 0 7 0 8 0

1 3 1 2 H z

SPL (dB) velocity (m/s) SPL (dB) velocity (m/s)

(37)

Planar array (“acoustic camera”)

• 24 omnidirectional mikes

mounted on a 1m square foldable wooden baffle with an optimized random disposition (new version with 32 Bruel&Kjaer

microphones)

• 24 channels acquisition system:

Behringer A/D converters + RME Hammerfall digital audio card

• Filters calculation, off-line processing and visualization with MATLAB

(38)

Circular array vs. Random array

The optimal randomized positions were found by running 10000 Matlab simulations, and chosing the one providing the better peak-to-noise ratio

Simulated matrix inversion - 3 kHz

(39)

Beamforming vs. Inverse filters

Random Array - Matrix inversion - 1 kHz

(40)

Effect of the regularization parameter

= 0.01 = 0.1

Random Array - Matrix Inversion - 5 kHz

(41)

Indoor application (source localisation)

• The array is equipped with a webcam

• The filtering process discriminates each

spherical wave (Tr’k(t)) coming by the pixels of a virtual screen placed on the plane where machine to be tested lyes

•At each pixel is associated the A-weighted equivalent level (LAeq, in dB) of each soundtrack extracted

•The dB(A) color map is

matched and superimposed to the webcam image

(42)

Outdoor application

The array is placed behind a noise barrier

• The colour map of the SPL

shows the leakage under the

barrier

(43)

Real time processing: work on progress

MATRIX CONVOLUTION

32-channels inputs

, 1

hn kHC

M-channels output

MAPS ARRAY

Virtual Microphone with high directivity

BROADCAST

Riferimenti

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