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LOCATION AND IDENTIFICATION OF DAMPING PARAMETERS

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Incompleteness of data. Generally small effect on dynamics. 5. Identification techniques ... and modal incompleteness. Spatial incompleteness can be overcome ... – PowerPoint PPT presentation

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Title: LOCATION AND IDENTIFICATION OF DAMPING PARAMETERS


1
LOCATION AND IDENTIFICATION OF DAMPING PARAMETERS
2
Contents
  • Objectives of the research
  • Introduction on damping identification techniques
  • New energy-based method
  • Numerical simulation
  • Experimental results
  • Conclusions
  • Future works

3
Objectives of the research
  • - Better understanding of damping in structures
    from an engineering point of view
  • Defining a practical identification method
  • Validate the method with numerical simulations
  • Test the method on real structures

4
Damping in structures
  • Damping in structures can be caused by several
    factors
  • Material damping
  • Damping in joints
  • Dissipation in surrounding medium

5
Issues in damping identification
  • Absence of a mathematical model for all damping
    forces
  • Computational time
  • Incompleteness of data
  • Generally small effect on dynamics

6
Identification techniques
  • Techniques for identifying the viscous damping
    matrix
  • Perturbation method
  • Inversion of receptance matrix
  • Lancasters formula
  • Energy-dissipation method

Prandina, M., Mottershead, J. E., and Bonisoli,
E., An assessment of damping identification
methods, Journal of Sound and Vibration (in
press), 2009.
7
Theory
The new method is based on the energy-dissipation
method, starting from the equations of motion of
a MDOF system
  • The energy equation can be derived

8
Theory
In the case of periodic response, the
contribution of conservative forces to the total
energy over a full cycle of periodic motion is
zero. So if T1 T (period of the response)
And the energy equation can be reduced to
9
Diagonal viscous damping matrix
The simplest case is a system with diagonal
viscous damping matrix. In this case the energy
equation becomes
10
Diagonal viscous damping matrix
11
Underdetermined system
  • The energy system of equations is usually
    underdetermined since the number of DOF can be
    greater than the number of tests. To solve the
    problem there are different options
  • Change the parameterization of the damping
    matrix
  • Increase the number of different excitations
  • Define a criterion to select the best columns
    of matrix A

12
Smallest angle criterion
Angle between a column ai of matrix A and the
vector e
Similarly, an angle between a set of columns B
and the vector e can be calculated using SVD an
QR algorithm
13
Numerical example
Accelerometers (dof 7, 11 and 19)
Dashpots (dof 3, 5, 13 and 17)
2
4
6
8
10
12
14
16
18
20
3
5
9
13
15
17
19
1
7
11
14
Procedure
  • Accelerations are measured on DOF 7, 11 and 19
    for a set of 8 different excitations at
    frequencies close to first 8 modes, random noise
    is added.
  • Velocities in all DOF are obtained by expanding
    these 3 measurements using the undamped mode
    shapes
  • Best columns of A are selected using smallest
    angle criterion
  • The energy equation is solved using least
    squares non-negative algorithm (to assure the
    identified matrix is non-negative definite)

15
Results
Case 1
N DOF of dashpots DOF of dashpots DOF of dashpots DOF of dashpots Damping coefficients (Ns/m) Damping coefficients (Ns/m) Damping coefficients (Ns/m) Damping coefficients (Ns/m) Angle
Exact 3 5 13 17 0.01 0.5 0.1 1 0
N DOF of identified dashpots DOF of identified dashpots DOF of identified dashpots DOF of identified dashpots Identified damping coefficients (Ns/m) Identified damping coefficients (Ns/m) Identified damping coefficients (Ns/m) Identified damping coefficients (Ns/m) Angle
1 - - - 17 - - - 1.084 12.557
2 - 5 - 17 - 0.581 - 1.042 1.029
3 - 5 13 17 - 0.506 0.124 0.989 0.263
4 3 5 13 17 0.01 0.501 0.099 1.002 0.001
16
Results
Case 2
N DOF of dashpots DOF of dashpots DOF of dashpots DOF of dashpots Damping coefficients (Ns/m) Damping coefficients (Ns/m) Damping coefficients (Ns/m) Damping coefficients (Ns/m) Angle
Exact 3 5 13 17 0.1 0.1 0.1 0.1 0
N DOF of identified dashpots DOF of identified dashpots DOF of identified dashpots DOF of identified dashpots Identified damping coefficients (Ns/m) Identified damping coefficients (Ns/m) Identified damping coefficients (Ns/m) Identified damping coefficients (Ns/m) Angle
1 - - - 19 - - - 0.107 6.505
2 - - 13 19 - - 0.151 0.059 0.404
3 - 5 15 17 - 0.212 0.127 0.055 0.124
4 3 5 13 17 0.101 0.098 0.099 0.1 0.001
17
Results
18
Results
Case 2 Damping factors
Mode Correct N1 Error N2 Error N3 Error
1 0.014092 0.013534 3.96 0.014096 0.03 0.014092 0.00
2 0.001496 0.002160 44.33 0.001495 0.11 0.001496 0.03
3 0.001024 0.000772 24.65 0.000894 12.72 0.001035 1.07
4 0.000338 0.000395 16.81 0.000305 9.74 0.000341 0.94
5 0.000138 0.000240 73.36 0.000149 7.95 0.000134 2.88
6 0.000190 0.000162 14.71 0.000193 1.86 0.000181 4.69
7 0.000114 0.000117 2.82 0.000118 4.12 0.000100 11.59
8 0.000057 0.000089 54.20 0.000049 15.05 0.000048 15.93
9 0.000106 0.000068 35.40 0.000073 31.19 0.000105 0.61
10 0.000085 0.000044 47.89 0.000061 27.98 0.000087 2.50
19
Nonlinear identification
  • The method can be applied to identify any damping
    in the form

In case of viscous damping and Coulomb friction
together, for example, the energy equation can be
written as
20
Nonlinear identification
New matrix A
Viscous
Coulomb Friction
21
Experiment setup
22
Magnetic dashpot
23
Experiment procedure
  • The structure without magnetic dashpot is excited
    with a set of 16 different excitations with
    frequencies close to those of the first 8 modes
  • The complete set of accelerations is measured
    and an energy-equivalent viscous damping matrix
    is identified as the offset structural damping
  • The measurement is repeated with the magnetic
    dashpot attached with the purpose of locating
    and identifying it

24
Experiment procedure
  • Velocities are derived from accelerometer
    signals
  • Matrix A and vector e are calculated, the energy
    dissipated by the offset damping is subtracted
    from the total energy
  • The energy equation (In this case
    overdetermined, since there are 16 excitations
    and 10 DOFs) is solved using least square
    technique

25
Experimental results
  • Magnetic viscous dashpot on DOF 9

Damping coefficients Expected (Ns/m) Identified (Ns/m)
C1 0 0
C2 0 0
C3 0 0
C4 0 0
C5 0 0
C6 0 0
C7 0 0
C8 0 0
C9 1.515 1.320
C10 0 0.032
26
Further experiments
  • Further experiments currently running will
    include more magnetic dashpots in different DOFs.
  • They will also include nonlinear sources of
    damping such as Coulomb friction devices.

27
Coulomb friction device
28
Advantages of the new method
  • Estimation of mass and stiffness matrices is not
    required if a complete set of measurements is
    available
  • Can identify non-viscous damping in the form
  • Robustness against noise and modal incompleteness
  • Spatial incompleteness can be overcome using
    expansion techniques

29
Conclusions
  • New energy-based method has been proposed
  • Numerical simulation has validated the theory
  • Initial experiments on real structure give
    reasonably good results, further experiments are
    currently running

30
Future works
  • Coulomb friction experiment
  • Extend the method to include material damping
  • Try different parameterizations of the damping
    matrices

31
Acknowledgements
  • Prof John E Mottershead
  • Prof Ken Badcock
  • Dr Simon James
  • Marie Curie Actions
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