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Airfoil in open jet β steering vectors.#
Demonstrates different steering vectors in Acoular and CSM diagonal removal. Uses measured data in file example_data.h5, calibration in file example_calib.xml, microphone geometry in array_56.xml (part of Acoular).
from pathlib import Path
import acoular as ac
from acoular.tools.helpers import get_data_file
The 4 kHz third-octave band is used for the example.
Obtain necessary data
time_data_file = get_data_file('example_data.h5')
calib_file = get_data_file('example_calib.xml')
First, we define the time samples using the MaskedTimeSamples class that
provides masking of channels and samples. Here, we exclude the channels with index 1 and 7 and
only process the first 16000 samples of the time signals. Alternatively, we could use the
TimeSamples class that provides no masking at all.
t1 = ac.MaskedTimeSamples(file=time_data_file)
t1.start = 0
t1.stop = 16000
invalid = [1, 7]
t1.invalid_channels = invalid
Calibration is usually needed and can be set as a separate processing block with the
Calib object. Invalid channels can be set here as well, by setting the
invalid_channels attribute.
calib = ac.Calib(source=t1, file=calib_file, invalid_channels=invalid)
The microphone geometry must have the same number of valid channels as the
MaskedTimeSamples object has. It also must be defined, which channels
are invalid.
micgeofile = Path(ac.__file__).parent / 'xml' / 'array_56.xml'
m = ac.MicGeom(file=micgeofile)
m.invalid_channels = invalid
Next, we define a planar rectangular grid for calculating the beamforming map (the example grid is
very coarse for computational efficiency). A 3D grid is also available via the
RectGrid3D class.
g = ac.RectGrid(x_min=-0.6, x_max=-0.0, y_min=-0.3, y_max=0.3, z=-0.68, increment=0.05)
For frequency domain methods, PowerSpectra provides the cross spectral
matrix (and its eigenvalues and eigenvectors). Here, we use the Welchβs method with a block size
of 128 samples, Hanning window and 50% overlap.
f = ac.PowerSpectra(source=calib, window='Hanning', overlap='50%', block_size=128)
To define the measurement environment, i.e. medium characteristics, the
Environment class is used. (in this case, only the speed of sound
is set)
env = ac.Environment(c=346.04)
The SteeringVector class provides the standard freefield sound
propagation model in the steering vectors.
st = ac.SteeringVector(grid=g, mics=m, env=env)
Finally, we define two different beamformers and subsequently calculate the maps for different
steering vector formulations. Diagonal removal for the CSM can be performed via the
r_diag parameter.
bb = ac.BeamformerBase(freq_data=f, steer=st, r_diag=True)
bs = ac.BeamformerCleansc(freq_data=f, steer=st, r_diag=True)
Plot result maps for different beamformers in frequency domain (left: with diagonal removal, right: without diagonal removal).
import matplotlib.pyplot as plt
fi = 1 # no of figure
for r_diag in (True, False):
plt.figure(fi, (5, 6))
fi += 1
i1 = 1 # no of subplot
for steer in ('true level', 'true location', 'classic', 'inverse'):
st.steer_type = steer
for b in (bb, bs):
plt.subplot(4, 2, i1)
i1 += 1
b.r_diag = r_diag
map = b.synthetic(cfreq, num)
mx = ac.L_p(map.max())
plt.imshow(ac.L_p(map.T), vmax=mx, vmin=mx - 15, origin='lower', interpolation='nearest', extent=g.extent)
plt.colorbar()
plt.title(b.__class__.__name__, fontsize='small')
plt.tight_layout()
plt.show()
[('example_data_cache.h5', 3)]
[('example_data_cache.h5', 4)]
[('example_data_cache.h5', 5)]
See also
Airfoil in open jet β Frequency domain beamforming methods. for an application of further frequency domain methods on the same data.
Total running time of the script: (0 minutes 2.338 seconds)

