nass-micro-station-measurements/modal-analysis/measurement.org

Modal Analysis - Measurement

• ZIP file containing the data and matlab files
• Instrumentation Used
• Structure Preparation and Test Planning
  • Structure Preparation
  • Test Planing
  • Location of the Accelerometers
  • Hammer Impacts
• Signal Processing
  • Averaging
  • Windowing
• Force and Response signals
  • Raw Force Data
  • Raw Response Data
  • Computation of one Frequency Response Function
• Frequency Response Functions and Coherence Results
• Generation of a FRF matrix and a Coherence matrix from the measurements

ZIP file containing the data and matlab files   ignore

All the files (data and Matlab scripts) are accessible here.

Instrumentation Used

In order to perform to Modal Analysis and to obtain first a Response Model, the following devices are used:

• An acquisition system (OROS) with 24bits ADCs (figure fig:oros)
• 3 tri-axis Accelerometers (figure fig:accelero_M393B05) with parameters shown on table tab:accelero_M393B05
• An Instrumented Hammer with various Tips (figure fig:instrumented_hammer) (figure fig:hammer_tips)

Acquisition system: OROS

The acquisition system permits to auto-range the inputs (probably using variable gain amplifiers) the obtain the maximum dynamic range. This is done before each measurement. Anti-aliasing filters are also included in the system.

Accelerometer used: M393B05

Sensitivity	10V/g
Measurement Range	0.5 g pk
Broadband Resolution	0.000004 g rms
Frequency Range	0.7 to 450Hz
Resonance Frequency	> 2.5kHz

393B05 Accelerometer Data Sheet

Tests have been conducted to determine the most suitable Hammer tip. This has been found that the softer tip gives the best results. It excites more the low frequency range where the coherence is low, the overall coherence was improved.

Instrumented Hammer

Hammer tips

The accelerometers are glued on the structure.

Structure Preparation and Test Planning

Structure Preparation

All the stages are turned ON. This is done for two reasons:

• Be closer to the real dynamic of the station in used
• If the control system of stages are turned OFF, this would results in very low frequency modes un-identifiable with the current setup, and this will also decouple the dynamics which would not be the case in practice

This is critical for the translation stage and the spindle as their is no stiffness in the free DOF (air-bearing for the spindle for instance).

The alternative would have been to mechanically block the stages with screws, but this may result in changing the modes.

The stages turned ON are:

• Translation Stage
• Tilt Stage
• Spindle and Slip-Ring
• Hexapod

The top part representing the NASS and the sample platform have been removed in order to reduce the complexity of the dynamics and also because this will be further added in the model inside Simscape.

All the stages are moved to their zero position (Ty, Ry, Rz, Slip-Ring, Hexapod).

All other elements have been remove from the granite such as another heavy positioning system.

Test Planing

The goal is to identify the full $N \times N$ FRF matrix (where $N$ is the number of degree of freedom of the system).

However, the principle of reciprocity states that: \[ H_{jk} = \frac{X_j}{F_k} = H_{kj} = \frac{X_k}{F_j} \] Thus, only one column or one line of the matrix has to be identified.

Either we choose to identify $\frac{X_k}{F_i}$ or $\frac{X_i}{F_k}$ for any chosen $k$ and for $i = 1,\ ...,\ N$.

We here choose to identify $\frac{X_i}{F_k}$ for practical reasons:

• it is easier to glue the accelerometers on some stages than to excite this particular stage with the Hammer

The measurement thus consists of:

• always excite the structure at the same location with the Hammer
• Move the accelerometers to measure all the DOF of the structure

Location of the Accelerometers

4 tri-axis accelerometers are used for each solid body.

Only 2 could have been used as only 6DOF have to be measured, however, we have chosen to have some redundancy.

This could also help us identify measurement problems or flexible modes is present.

The position of the accelerometers are:

• 4 on the first granite
• 4 on the second granite (figure fig:accelerometers_granite2_overview)
• 4 on top of the translation stage (figure fig:accelerometers_ty_overview)
• 4 on top of the tilt stage
• 3 on top of the spindle
• 4 on top of the hexapod (figure fig:accelerometers_hexa_overview)

In total, 23 accelerometers are used: 69 DOFs are thus measured.

The position and orientation of all the accelerometers used are shown on figure fig:nass-modal-test.

The precise determination of the position of each accelerometer is done using the SolidWorks model (shown on figure fig:location_accelerometers).

Accelerometers located on the top granite

Accelerometers located on top of the translation stage

Accelerometers located on the Hexapod

Position and orientation of the accelerometer used

Position of the accelerometers using SolidWorks

The precise position of all the 23 accelerometer with respect to a frame located at the point of interest (located 270mm above the top platform of the hexapod) is shown below. The values are in meter. They are contained in the mat/id31_nanostation.cfg file.

ID	X[m]	Y[m]	Z[m]
1	-6.4000e-002	-6.4000e-002	-2.7000e-001
2	-6.4000e-002	6.4000e-002	-2.7000e-001
3	6.4000e-002	6.4000e-002	-2.7000e-001
4	6.4000e-002	-6.4000e-002	-2.7000e-001
5	-3.8500e-001	-3.0000e-001	-4.1680e-001
6	-4.2000e-001	2.8000e-001	-4.1680e-001
7	4.2000e-001	2.8000e-001	-4.1680e-001
8	3.8000e-001	-3.0000e-001	-4.1680e-001
9	-4.7500e-001	-4.1400e-001	-4.2730e-001
10	-4.6500e-001	4.0700e-001	-4.2730e-001
11	4.7500e-001	4.2400e-001	-4.2730e-001
12	4.7500e-001	-4.1900e-001	-4.2730e-001
13	-3.2000e-001	-4.4600e-001	-7.8560e-001
14	-4.8000e-001	5.3400e-001	-7.8560e-001
15	4.5000e-001	5.3400e-001	-7.8560e-001
16	2.9500e-001	-4.8100e-001	-7.8560e-001
17	-7.3000e-001	-5.2600e-001	-9.5060e-001
18	-7.3500e-001	8.1400e-001	-9.5060e-001
19	8.7500e-001	7.9900e-001	-9.5060e-001
20	8.6490e-001	-5.0600e-001	-9.5060e-001
21	-1.5500e-001	-9.0000e-002	-5.9400e-001
22	0.0000e+000	1.8000e-001	-5.9400e-001
23	1.5500e-001	-9.0000e-002	-5.9400e-001

Hammer Impacts

Only 3 impact points are used.

The impact points are shown on figures fig:hammer_x, fig:hammer_y and fig:hammer_z.

We chose this excitation point as it seems to excite all the modes in the frequency band of interest and because it provides good coherence for all the accelerometers.

Hammer Blow in the X direction

Hammer Blow in the Y direction

Hammer Blow in the Z direction

Signal Processing

Averaging

The measurements are averaged 10 times corresponding to 10 hammer impacts in order to reduce the effect of random noise. The parameters for the impact test are shown on table tab:meas_parameters.

Start Delay	-5%
Number of lines	801 lines
Trigger Threshold	300N
Trigger Hysteresis	100mN
FRF Average	10

Impact test parameters

Windowing

Windowing is used on the force and response signals.

A boxcar window (figure fig:windowing_force_signal) is used for the force signal as once the impact on the structure is done, the measured signal is meaningless. The parameters are:

• Start: $3\%$
• Stop: $7\%$

  <<plt-matlab>>

Window used for the force signal

An exponential window (figure fig:windowing_response_signal) is used for the response signal as we are measuring transient signals and most of the information is located at the beginning of the signal. The parameters are:

• FlatTop:

  • Start: $3\%$
  • Stop: $2.96\%$

• Decreasing point:

  • X: $60.4\%$
  • Y: $14.7\%$

  <<plt-matlab>>

Window used for the response signals

Force and Response signals

Let's load some obtained data to look at the force and response signals.

  meas1_raw = load('mat/meas_raw_1.mat');

Raw Force Data

The force input for the first measurement is shown on figure fig:raw_data_force. We can see 10 impacts, one zoom on one impact is shown on figure fig:raw_data_force_zoom.

The Fourier transform of the force is shown on figure fig:fourier_transfor_force_impact. This has been obtained without any windowing.

  <<plt-matlab>>

Raw Force Data from Hammer Blow

  <<plt-matlab>>

Raw Force Data from Hammer Blow - Zoom

  <<plt-matlab>>

Fourier Transform of the 10 force impacts for the first measurement

Raw Response Data

The response signal for the first measurement is shown on figure fig:raw_data_acceleration. One zoom on one response is shown on figure fig:raw_data_acceleration_zoom.

The Fourier transform of the response signals is shown on figure fig:fourier_transform_response_signals. This has been obtained without any windowing.

  <<plt-matlab>>

Raw Acceleration Data from Accelerometer

  <<plt-matlab>>

Raw Acceleration Data from Accelerometer - Zoom

  <<plt-matlab>>

Fourier transform of the measured response signals

Computation of one Frequency Response Function

Now that we have obtained the Fourier transform of both the force input and the response signal, we can compute the Frequency Response Function from the force to the acceleration.

We then compare the result obtained with the FRF computed by the modal software (figure fig:frf_comparison_software).

The slight difference can probably be explained by the use of windows.

In the following analysis, FRF computed from the software will be used.

  meas1 = load('mat/meas_frf_coh_1.mat');

  <<plt-matlab>>

Comparison of the computed FRF from the Fourier transform and using the modal software

Frequency Response Functions and Coherence Results

Let's see one computed Frequency Response Function and one coherence in order to attest the quality of the measurement.

First, we load the data.

  meas1 = load('mat/meas_frf_coh_1.mat');

And we plot on figure fig:frf_result_example the frequency response function from the force applied in the $X$ direction at the location of the accelerometer number 11 to the acceleration in the $X$ direction as measured by the first accelerometer located on the top platform of the hexapod.

The coherence associated is shown on figure fig:frf_result_example.

  <<plt-matlab>>

Example of one measured FRF

  <<plt-matlab>>

Example of one measured Coherence

Generation of a FRF matrix and a Coherence matrix from the measurements

We want here to combine all the Frequency Response Functions measured into one big array called the Frequency Response Matrix.

The frequency response matrix is an $n \times p \times q$:

• $n$ is the number of measurements: $23 \times 3$ (23 accelerometers measuring 3 directions each)
• $p$ is the number of excitation inputs: $3$
• $q$ is the number of frequency points $\omega_i$

Thus, the FRF matrix is an $69 \times 3 \times 801$ matrix.

For each frequency point $\omega_i$, we obtain a 2D matrix:

\begin{equation} \text{FRF}(\omega_i) = \begin{bmatrix} \frac{D_{1_x}}{F_x}(\omega_i) & \frac{D_{1_x}}{F_y}(\omega_i) & \frac{D_{1_x}}{F_z}(\omega_i) \\ \frac{D_{1_y}}{F_x}(\omega_i) & \frac{D_{1_y}}{F_y}(\omega_i) & \frac{D_{1_y}}{F_z}(\omega_i) \\ \frac{D_{1_z}}{F_x}(\omega_i) & \frac{D_{1_z}}{F_y}(\omega_i) & \frac{D_{1_z}}{F_z}(\omega_i) \\ \frac{D_{2_x}}{F_x}(\omega_i) & \frac{D_{2_x}}{F_y}(\omega_i) & \frac{D_{2_x}}{F_z}(\omega_i) \\ \vdots & \vdots & \vdots \\ \frac{D_{23_z}}{F_x}(\omega_i) & \frac{D_{23_z}}{F_y}(\omega_i) & \frac{D_{23_z}}{F_z}(\omega_i) \\ \end{bmatrix} \end{equation}

We generate such FRF matrix from the measurements using the following script.

  n_meas = 24;
  n_acc = 23;

  dirs = 'XYZ';

  % Number of Accelerometer * DOF for each acccelerometer / Number of excitation / frequency points
  FRFs = zeros(3*n_acc, 3, 801);
  COHs = zeros(3*n_acc, 3, 801);

  % Loop through measurements
  for i = 1:n_meas
    % Load the measurement file
    meas = load(sprintf('mat/meas_frf_coh_%i.mat', i));

    % First: determine what is the exitation (direction and sign)
    exc_dir = meas.FFT1_AvXSpc_2_1_RMS_RfName(end);
    exc_sign = meas.FFT1_AvXSpc_2_1_RMS_RfName(end-1);
    % Determine what is the correct excitation sign
    exc_factor = str2num([exc_sign, '1']);
    if exc_dir ~= 'Z'
      exc_factor = exc_factor*(-1);
    end

    % Then: loop through the nine measurements and store them at the correct location
    for j = 2:10
      % Determine what is the accelerometer and direction
      [indices_acc_i] = strfind(meas.(sprintf('FFT1_H1_%i_1_RpName', j)), '.');
      acc_i = str2num(meas.(sprintf('FFT1_H1_%i_1_RpName', j))(indices_acc_i(1)+1:indices_acc_i(2)-1));

      meas_dir  = meas.(sprintf('FFT1_H1_%i_1_RpName', j))(end);
      meas_sign = meas.(sprintf('FFT1_H1_%i_1_RpName', j))(end-1);
      % Determine what is the correct measurement sign
      meas_factor = str2num([meas_sign, '1']);
      if meas_dir ~= 'Z'
        meas_factor = meas_factor*(-1);
      end

      % FRFs(acc_i+n_acc*(find(dirs==meas_dir)-1), find(dirs==exc_dir), :) = exc_factor*meas_factor*meas.(sprintf('FFT1_H1_%i_1_Y_ReIm', j));
      % COHs(acc_i+n_acc*(find(dirs==meas_dir)-1), find(dirs==exc_dir), :) = meas.(sprintf('FFT1_Coh_%i_1_RMS_Y_Val', j));

      FRFs(find(dirs==meas_dir)+3*(acc_i-1), find(dirs==exc_dir), :) = exc_factor*meas_factor*meas.(sprintf('FFT1_H1_%i_1_Y_ReIm', j));
      COHs(find(dirs==meas_dir)+3*(acc_i-1), find(dirs==exc_dir), :) = meas.(sprintf('FFT1_Coh_%i_1_RMS_Y_Val', j));
    end
  end
  freqs = meas.FFT1_Coh_10_1_RMS_X_Val;

And we save the obtained FRF matrix and Coherence matrix in a .mat file.

  save('./mat/frf_coh_matrices.mat', 'FRFs', 'COHs', 'freqs');