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Attocube - Test Bench

Table of Contents

1 Estimation of the Spectral Density of the Attocube Noise

test-bench-schematic.png

Figure 1: Test Bench Schematic

IMG-7865.JPG

Figure 2: Picture of the test bench. The Attocube and mirror are covered by a “bubble sheet”

1.1 Long and Slow measurement

The first measurement was made during ~17 hours with a sampling time of \(T_s = 0.1\,s\).

load('./mat/long_test_plastic.mat', 'x', 't')
Ts = 0.1; % [s]

long_meas_time_domain_full.png

Figure 3: Long measurement time domain data

Let’s fit the data with a step response to a first order low pass filter (Figure 4).

f = @(b,x) b(1)*(1 - exp(-x/b(2)));

y_cur = x(t < 17.5*60*60);
t_cur = t(t < 17.5*60*60);

nrmrsd = @(b) norm(y_cur - f(b,t_cur)); % Residual Norm Cost Function
B0 = [400e-9, 2*60*60];                        % Choose Appropriate Initial Estimates
[B,rnrm] = fminsearch(nrmrsd, B0);     % Estimate Parameters ‘B’

The corresponding time constant is (in [h]):

2.0658

long_meas_time_domain_fit.png

Figure 4: Fit of the measurement data with a step response of a first order low pass filter

We can see in Figure 3 that there is a transient period where the measured displacement experiences some drifts. This is probably due to thermal effects. We only select the data between t1 and t2. The obtained displacement is shown in Figure 5.

t1 = 10.5; t2 = 17.5; % [h]

x = x(t > t1*60*60 & t < t2*60*60);
x = x - mean(x);
t = t(t > t1*60*60 & t < t2*60*60);
t = t - t(1);

long_meas_time_domain_zoom.png

Figure 5: Kept data (removed slow drifts during the first hours)

The Power Spectral Density of the measured displacement is computed

win = hann(ceil(length(x)/20));
[p_1, f_1] = pwelch(x, win, [], [], 1/Ts);

As a low pass filter was used in the measurement process, we multiply the PSD by the square of the inverse of the filter’s norm.

G_lpf = 1/(1 + s/2/pi);
p_1 = p_1./abs(squeeze(freqresp(G_lpf, f_1, 'Hz'))).^2;

Only frequencies below 2Hz are taken into account (high frequency noise will be measured afterwards).

p_1 = p_1(f_1 < 2);
f_1 = f_1(f_1 < 2);

1.2 Short and Fast measurement

An second measurement is done in order to estimate the high frequency noise of the interferometer. The measurement is done with a sampling time of \(T_s = 0.1\,ms\) and a duration of ~100s.

load('./mat/short_test_plastic.mat')
Ts = 1e-4; % [s]
x = detrend(x, 0);

The time domain measurement is shown in Figure 6.

short_meas_time_domain.png

Figure 6: Time domain measurement with the high sampling rate

The Power Spectral Density of the measured displacement is computed

win = hann(ceil(length(x)/20));
[p_2, f_2] = pwelch(x, win, [], [], 1/Ts);

1.3 Obtained Amplitude Spectral Density of the measured displacement

The computed ASD of the two measurements are combined in Figure 7.

psd_combined.png

Figure 7: Obtained Amplitude Spectral Density of the measured displacement

2 Effect of the “bubble sheet” and “Aluminium tube”

IMG-7864.JPG

Figure 8: Aluminium tube used to protect the beam path from disturbances

2.1 Aluminium Tube and Bubble Sheet

load('./mat/short_test_plastic.mat');
Ts = 1e-4; % [s]
x = detrend(x, 0);
win = hann(ceil(length(x)/10));
[p_1, f_1] = pwelch(x, win, [], [], 1/Ts);

2.2 Only Aluminium Tube

load('./mat/short_test_alu_tube.mat');
Ts = 1e-4; % [s]
x = detrend(x, 0);

The time domain measurement is shown in Figure 6.

win = hann(ceil(length(x)/10));
[p_2, f_2] = pwelch(x, win, [], [], 1/Ts);

2.3 Nothing

load('./mat/short_test_without_material.mat');
Ts = 1e-4; % [s]
x = detrend(x, 0);

The time domain measurement is shown in Figure 6.

win = hann(ceil(length(x)/10));
[p_3, f_3] = pwelch(x, win, [], [], 1/Ts);

2.4 Comparison

asd_noise_comp_bubble_aluminium.png

Figure 9: Comparison of the noise ASD with and without bubble sheet

3 Measurement of the Attocube’s non-linearity

The measurement setup is shown in Figure 10.

Here are the equipment used in the test bench:

  • Renishaw Resolution Encoder with 1nm resolution (doc)
  • Attocube interferometer (doc)
  • Cedrat Amplified Piezoelectric Actuator APA95ML (doc)
  • Voltage Amplifier LA75B (doc)
  • Speedgoat IO131 with 16bits ADC and DAC (doc)

exp_setup_schematic.png

Figure 10: Schematic of the Experiment

A DAC and voltage amplified are used to move the mass with the Amplified Piezoelectric Actuator (APA95ML). The encoder and the attocube are measure ring the same motion.

As will be shown shortly, this measurement permitted to measure the period non-linearity of the Attocube.

3.1 Load Data

The measurement data are loaded and the offset are removed using the detrend command.

load('mat/int_enc_comp.mat', 'interferometer', 'encoder', 'u', 't');
Ts = 1e-4; % Sampling Time [s]
interferometer = detrend(interferometer, 0);
encoder = detrend(encoder, 0);
u = detrend(u, 0);

3.2 Time Domain Results

One period of the displacement of the mass as measured by the encoder and interferometer are shown in Figure 11. It consist of the sinusoidal motion at 0.5Hz with an amplitude of approximately \(70\mu m\).

The frequency of the motion is chosen such that no resonance in the system is excited. This should improve the coherence between the measurements made by the encoder and interferometer.

int_enc_one_cycle.png

Figure 11: One cycle measurement

The difference between the two measurements during the same period is shown in Figure 12.

int_enc_one_cycle_error.png

Figure 12: Difference between the Encoder and the interferometer during one cycle

3.3 Difference between Encoder and Interferometer as a function of time

The data is filtered using a second order low pass filter with a cut-off frequency \(\omega_0\) as defined below.

w0 = 2*pi*5; % [rad/s]
xi = 0.7;

G_lpf = 1/(1 + 2*xi/w0*s + s^2/w0^2);

After filtering, the data is “re-shaped” such that we can superimpose all the measured periods as shown in Figure 13. This gives an idea of the measurement error as given by the Attocube during a \(70 \mu m\) motion.

d_err_mean = reshape(lsim(G_lpf, encoder - interferometer, t), [2/Ts floor(Ts/2*length(encoder))]);
d_err_mean = d_err_mean - mean(d_err_mean);

int_enc_error_mean_time.png

Figure 13: Difference between the two measurement in the time domain, averaged for all the cycles

3.4 Difference between Encoder and Interferometer as a function of position

Figure 13 gives the measurement error as a function of time. We here wish the compute this measurement error as a function of the position (as measured by the encoer).

To do so, all the attocube measurements corresponding to each position measured by the Encoder (resolution of \(1nm\)) are averaged. Figure 14 is obtained where we clearly see an error with a period comparable to the motion range and a much smaller period corresponding to the non-linear period errors that we wish the estimate.

[e_sorted, ~, e_ind] = unique(encoder);

i_mean = zeros(length(e_sorted), 1);
for i = 1:length(e_sorted)
  i_mean(i) = mean(interferometer(e_ind == i));
end

i_mean_error = (i_mean - e_sorted);

int_enc_error_mean_position.png

Figure 14: Difference between the two measurement as a function of the measured position by the encoder, averaged for all the cycles

The period of the non-linearity seems to be equal to \(765 nm\) which corresponds to half the wavelength of the Laser (\(1.53 \mu m\)). For the motion range done here, the non-linearity is measured over ~18 periods which permits to do some averaging.

win_length = 1530/2; % length of the windows (corresponds to 765 nm)
num_avg = floor(length(e_sorted)/win_length); % number of averaging

i_init = ceil((length(e_sorted) - win_length*num_avg)/2); % does not start at the extremity

e_sorted_mean_over_period = mean(reshape(i_mean_error(i_init:i_init+win_length*num_avg-1), [win_length num_avg]), 2);

The obtained periodic non-linearity is shown in Figure 15.

int_non_linearity_period_wavelength.png

Figure 15: Non-Linearity of the Interferometer over the period of the wavelength

Author: Dehaeze Thomas

Created: 2020-11-10 mar. 10:21