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Proceedings of ICASI - 2004
                                                       International Conference on Advances in Structural Integrity
                                                     July 14-17, 2004, Indian Institute of Science, Bangalore, India


                                                                                               ICASI/XX-XXX


       Time domain structural health monitoring with
  magnetostrictive patches using five stage hierarchical neural
                           networks.
                              Ghosh D. P. (a) and Gopalakrishnan S. (b)

                             (a) Graduate student (b) Assoc. professor,
            Dept. of Aerospace Engineering, Indian Institute of Science, Bangalore 560012


                                               ABSTRACT

An integrated method for damage detection of composite laminates is presented in this paper using time
domain data obtained from magnetostrictive sensors and actuators and artificial neural networks (ANN)
identification with five stage hierarchical neural network (HNN). Magnetostrictive actuators are actuated
through an actuation coil, which vibrates the composite laminate. The presence of delamination, due to
induced magnetic field intensity, changes the stress response of the structure. This in turn changes the
magnetic flux intensity of the magnetostrictive sensor. The changes in the flux density are sensed through a
sensing coil as open circuit voltage. The ANN is applied to establish the mapping relationship between
structural damage status (location and severity) and sensor open circuit voltage. As ANN is prone to
overtraining and the dimension of input space is considerable high, a five-stage hierarchy of networks is
used for the identification procedure. The results of delamination damage detection for composite laminate
show that the method developed in this paper can be applied to structural damage detection and health
monitoring for various industrial structures. To demonstrate this approach, numerical simulations are
carried out on a composite cantilever beam to identify size and location of delamination using the sensor
data for a known actuation for a certain combination of sensor and actuator locations.

Keywords: Magnetostrictive, FEM, SHM, ANN, Hierarchical Neural Network, Inverse Problem.

            1. INTRODUCTION                               may broadly refer to as functional materials.
                                                          With the availability of functional materials and
Composites have revolutionized structural                 the feasibility of embedding them into or
construction. They are extensively used in                bonding them to composite structures, smart
aerospace, civil, mechanical and other industries.        structural concepts are emerging to be attractive
Present day aerospace vehicles have composites            for potential high performance structural
up to 60 % or more of the total material used.            applications.1 A smart structure may be generally
More recently, materials, which can give rise to          defined as one which has the ability to determine
mechanical response when subjected to non-                its current state, decides in a rational manner on a
mechanical loads such as PZTs, Terfenol-D,                set of actions that would change its state to a
SMAs, have become available. Such materials               more desirable state and carries out these actions
in a controlled manner over a short period of           important ways to ensure reliable operation and
time. With such features incorporated in a              reduced maintenance cost for in-service
structure by embedding functional materials, it is      structures. Magnetostrictive material such as
feasible to achieve technological advances such         Terfenol-D, hitherto considered as only actuator
as vibration and noise reduction, high pointing         material, was shown to be used for sensing
accuracy of antennae, damage detection, damage          application in reference.7 In this work, the
mitigation etc.2, 3                                     authors proved this capacity experimentally by
                                                        passing a magnetic field on to an actuator
During the operation of a structure, damages may        magnetostrictive patch and measured the voltage
develop, which will cause a change in the               across the sensing patch to infer the presence of
strain/stress state of the structure and the            damage.
vibration characteristics. By continuously              In this paper we take this approach not only to
monitoring one or more of these response                confirm its presence but also its location.
quantities, it is possible to assess the condition of   Noncontact magnetostrictive strain sensor was
the structure for its structural integrity. Such a      explored by Kleinke, D. K. et al.8 and the study
monitoring of the structure is called structural        of magnetostrictive particulate actuator was done
health monitoring. Health monitoring application        by Anjanappa, M. et al.9 Sensing of delamination
has been receiving great deal of attention all over     in composite laminates using embedded
the world, due to possible significant impact on        magnetostrictive material was studied by Krishna
safety and longevity of the structure. To               Murty, A. V. et al.10 Authors [18] had developed
implement health-monitoring concept it is               a new finite element formulation for inbuilt
necessary to have a number of sensors to                magnetostrictive      patches   for performing
measure response parameters. These responses            numerical simulations.
will then be post-processed to assess the               The mathematical relationships between sensor
condition of structure. Mark Lin and Fu-Kuo             open circuit voltage and structural damage status
Chang 4 built such a system when they developed         (i.e., damage location and severity) are very
a built-in monitoring system for composite              complex. It is not only strongly non-linear, but
structures using SMART layer containing a               also often has no analytical solution. Deduction
network of actuators or sensors.                        from sensor output to practical damage status is
Change of structural dynamic performance                mathematically classified as inverse problem,
caused by structural damage that is less than 1%        and is very hard to compute precise solution
of the total structural size is unnoticeable. Yan       using mathematical analysis. If one takes the
and Yam5 pointed out that when the crack length         inherent law between sensor output and practical
in a composite plate equals 1% of the plate             damage status as a black box, the mapping
length, the relative variation of structural natural    relationship between these two state spaces can
frequency is only about 0.01 to 0.1%. This was          be established using genetic algorithms (GAs) or
also shown by Nag et al.6 Therefore, using              artificial neural networks (ANN). Thus, one need
vibration modal parameters, e.g., natural               not know explicitly the inherent law in structural
frequencies, displacement or strain mode shapes,        damage detection. Moslem and Nafaspour11 and
and modal damping are generally ineffective in          Chou and Ghaboussi12 reported some researches
identifying small and incipient structural              on structural damage detection using GAs, and
damage. It has been theoretically and                   they were successful in determining the severity
experimentally proved that local damage in a            and locations of structural damage. However,
structure will cause the reduction of local             GAs-based structural damage detection requires
structural stiffness, which leads to variation of       repeatedly searching from numerous damage
dynamic performance of the whole structure. In          parameters so as to find the optimal solution of
industry, using the time domain measured                the objective function (measured data). The cost
structural vibration responses to identify and          of computation limits the use of GA for damage
monitor structural damage is one of the                 detection applications.
ANN has particular advantage in establishing         with different initial condition, learning rate,
accurate mapping relationships between sensor        momentum rate, learning algorithm and learning
data and physical parameters of structural           sequence.
damage. When classifications and identification
of structural damage needs to be carried out, the    In this study, an integrated damage detection
required task is only to train the ANN in advance    method is developed for composite laminate
using a set of known sensor data and damage          through theoretical study and numerical
physical parameters of the structures that needs     simulation. This method requires the generation
detection. Hung and Kao13 and Yun and Bahng14        of    excitation     and     structural  response
reported their researches on structural damage       measurement using bonded magnetostrictive
detection using ANN, and their results showed        patch actuator and sensors; which is used in
that ANN is a highly effective tool for              hierarchical ANN framework for classification
identifying structural damage.                       and identification of structural damage.
By using the hierarchical scheme, a complicated
large-scale system is decomposed into a set of               2. FORWARD ANALYSIS
lower order subsystems and a coordination            Application of magnetic field causes strain in the
process, and thus becomes tractable. Hierarchical    magnetostrictive material (Terfenol-D) and the
structures can have more than two levels.            stress, changes magnetic flux density of that
However, in practice, two-level structures are       material.15
usually popular. Here five stages of hierarchy are   The three-dimensional constitutive relationship
considered for structural health monitoring case.    for magnetostrictive material is generally written
As the original sensor output (open circuit          as
voltage) is high dimensional data hence the ANN
input space, it is quite impossible to train the                 {ε } = [ S {H } ]{σ } + [d ]T {H } (1)
network. To reduce the dimension of input space                  {B} = [d ]{σ } + [ µ {σ } ]{H } (2)
of ANN, different dimensional reduction
algorithms are used like ICA, PCA, peak value,       The Equation- (1) is used as actuator and
peak location etc. But some times due to this        Equation- (2) is used as sensor in the composite
dimensional reduction procedure, damage              structure. Using these two equations, the time
signatures are lost in the lower dimension data,     domain sensor response due to actuation in the
which leads to lose of the essential output          actuator can be computed through finite element
uniqueness of ANN mapping. Here to deal with         formulation [18]. In the forward analysis for a
this problem, output space is partitioned in         given actuation history and a given damage
different overlapped subspace and different          condition, sensor response history can be
experts are trained in these partitions. With in     obtained for a particular structure. Where as, in
every expert, a number of validator networks are     inverse problem, either actuation history or
trained. All of them have the same set of sample     damage condition is unknown. Detail procedure
data in higher dimensional input space, but with     for forward analysis can be obtained from [18].
different lower dimensional input space coming
from different dimensional reduction procedures.
Every ANN are trained and validated by a fixed                 3. INVERSE ANALYSIS
set of sample set. Single validator network is       Inverse problem can be classified in two
consisting of different ensembler network using      category, force inverse problem and geometry
different partitioning of training set and           inverse problem. In the force inverse problem,
validation set from the sample set. Similarly        actuation history is unknown but the structure
single ensembler network is also classified with     and its response is known. In geometry inverse
different multi layer perceptron (ANN). These        problem applied force and response of structure
ANNs have different network architecture             are known but structure is unknown. Damage
(hidden layers, hidden nodes), and are trained       identification is the geometric inverse problem,
                                                     which can be solved by artificial neural network.
3.1 Artificial Neural Network                          the minimal training error. A small learning rate
Artificial neural networks (ANNs) can provide          results in long learning times. A relatively large
non-linear parameterized mapping between a set         learning rate results in faster learning but can
of inputs and a set of outputs with unknown            also result in a chaotically learning behavior
function relationship. Thus ANNs are universal         during training of the network. The function of
function approximators and are therefore               the momentum term is to increase the size of the
attractive for automatically learning of the (non-     learning steps when the direction in the weight
linear) functional relation between the input          update is the same as the direction in the
variables and the output variables. A three-layer      previous step. As with the learning rate, if the
network (Figure-1) with the sigmoid activation         momentum term is too large the network will
functions can approximate any smooth mapping.          display a chaotic learning behavior.
A typical supervised feed-forward multi layer          If many training epochs are used, an ANN tends
neural network is called as a back propagation         to overtrain the learning material (i.e. the
(BP) neural network. The structure of a BP             accuracy on the training material is very high
neural network mainly includes the input layer         whereas the accuracy on new instances is much
for receiving input data; the hidden layer for         lower). In this work over training is avoided by
processing data; and the output layer to indicate      dividing the training set into two groups, and
the identified results. In this study, ability of      using one group of patterns to train the network
identifying structural damage status for an ANN        while the other one is used for validating the
is acquired through training the neural network        performance of the trained network. It was
using the known samples. Normally, many                observed that the training error decreases along
training epochs are required before a set of           with number of epoch while the validation error
weights is found that accurately fit the training      decreases at first, bounces around, and then starts
material.                                              increasing. The optimal learning is achieved at
The training of a BP neural network is a two-step      the global minimum of validation error.
procedure. In the first step, the network              If the number of hidden units in ANN is too
propagates input through each layer until an           small, the modeling capacity of the network is
output is generated. The error between the output      too low, and it is impossible for the learning rule
and the target output is then computed. In the         to find an adequate model. If, on the other hand,
second step, the calculated error is transmitted       the number of hidden units is too large, the
backwards from the output layer and the weights        modeling capacity of the network is too
are adjusted to minimize the error. The training       substantial, resulting in a strong inclination
process is terminated when the error is                towards overlearning.
sufficiently small for all training samples. The       Committee Machine
data set is separated into two parts, one for          It is perhaps impossible to combine simplicity
training and the other for testing or validating the   and accuracy in a single model of ANN. Single
network performance. The network parameters            multi-layered perceptron (MLP) uses a black box
are determined, as is common practice, through         approach to globally fit a single function into the
experimentation. This includes the number of           data, thereby losing insight into the problem.
hidden nodes and the learning rates. Data              This problem was studied [19] by partitioning
obtained from the magnetostrictive sensors             the input and output space into a piecewise set of
described above, is used to train conventional         subspaces, with each subspace having its own
back propagation networks to identify the              expert.
delamination size and location of the composite        Hierarchical Neural Network
laminate.                                              With the common three-layer neural network
The accuracy of a trained network is measured          architectures, networks lack internal structure; as
by calculating the mean square error (MSE) on          a consequence, it is very difficult to discern
the training sample. The learning rate determines      characteristics of the knowledge acquired by a
the size of the steps in the search space to find      network in order to evaluate its reliability and
applicability.     Alternative     neural-network      error gives more weightage of the neural
architecture is presented, based on a hierarchical     network. In the execution phase, these
organization shown in Figure-3. By using the           weightages are used to get weighted average of
hierarchical scheme, a complicated large-scale         all neural networks output as the output of
system is decomposed into a set of lower order         ensemble network. From the distribution of the
subsystems and a coordination process, and thus        output of different neural networks and their
becomes tractable. A five-stage hierarchical           corresponding weightage one measure of
neural network is designed by combining a              overtraining can be computed. If the outputs of
multilayer perceptron first stage and mixture-of-      different neural network are close (at least for
experts in the subsequent stages. The second           those has more weightage) then networks are
stage mixture-of-experts, ensembler network,           well trained otherwise it is overtrained. Every
learns to minimize the overtraining errors. The        trained neural network is tested through the test
third stage mixture-of-experts, validation             data set, which gives the testing errors as a
network, learns to minimize the validation errors.     measure of generalization of the neural networks.
And the fourth stage mixture-of-experts, expert        These testing errors with the weightages of the
networks, learns to minimize the error of network      neural networks give the weighted average of
due to loss of information for input space             testing error, as a measure of testing error of the
dimension reduction. And Finally fifth stage           ensemble network. Next issue in the neural
committee machine choose the appropriate expert        network is the generalization of the network
network from all expert networks. Each lower           using the testing error of ensemble network.
level subsystem is solved independently for a           Validation Network
fixed value of the coordination variable whose         As, every neural network within the ensemble
value is adjusted by the upper level coordination      network is trained with same training sample;
unit in an appropriate fashion so that the lower       these neural networks need testing for
level subsystems resolve their problems. The           generalization of the ensemble network. For
coordination is to provide a solution to the           testing of network, sample data set is separated
overall system. Continuous exchange of                 into two groups, one for training and other for
information between the lower subsystems and           testing (validation). After training of neural
the upper coordination unit will finally lead to a     networks, with the training sample, the neural
better solution. The whole procedure is discussed      networks simulate the testing sample and get the
as follows.                                            testing error. These testing errors with their
 Ensemble Network                                      weightages give the measure of generalization of
Often artificial neural networks are prone to          the ensemble network. However, every network
overtraining, where network trains the                 in the ensemble network is trained and tested
computational and experimental noises. And             through the same set of training data set and
there is no direct rule to draw the line between       testing data set respectively. To get a more
well training and overtraining for a set of training   general input-output mapping from a set of
examples and network architecture. One of the          sample data set, different division of training
indirect ways to get a measure of overtraining of      sample and testing sample is essential. This can
the network is Ensemble Network. In ensemble           be done through a systematic manner using
network, a number of neural networks are train         validation network. Validation Network consists
with the same training samples but with different      of some number of ensemble networks. These
initial condition, learning rate, training             ensemble networks are trained and tested with
algorithm, network architecture and training           same sample data set with different partition for
sequence (for sequential learning). In training        training data set and testing data set. However,
phase, each network trains and generates training      every validation network is train for a fixed set
error for the training samples. On the basis of        of sample data set.
these training errors, weightages of the trained       Dimensional Reduction of Input Space
neural network is determined, where less training
In time domain structural health monitoring, time     and actuation combination. But as the input
histories of the sensor outputs (open circuit         space subdivision is known a’ priory, committee
voltages) are the original input space for the        machine for input space subdivision is not
input-output mapping, which is very high              required.
dimensional. So, it is not possible to train the      Conditional Expert
network taking full dimension of the original         Always some dimension of output space is
input space (sensor output). To address this          difficult to train than other dimension of output
issue, different dimension reduction procedures       space. In SHM of composite laminate, depth
are available in the literature, which can reduce     wise training is difficult than span wise training.
the dimension of the original input space keeping     To solve this kind of problem some conditional
main features of the high dimensional data. But       experts are trained. If the dimension of output
for structural health monitoring, suitable            subset of some expert is less than the original
dimension reduction procedure is not available,       dimension of output space, the value for the
which will reduce the dimension of the input          missing dimension is required a ‘priory to
space preserving the signature of damage from         execute the network. These experts are called
the high dimensional sensor output data. To           Conditional Expert. Conditional experts are used
overcome this problem a number of reductions          to get finer location for some dimensions in the
procedure is taken to increase the chance of          output space, when locations for remaining
preserving the damage signature in the reduced        dimensions are already known by other type of
input data sets. In the next section this issue is    experts. For structural health monitoring problem
discussed in a systematic manner.                     in composite laminate, identification of layer
Expert                                                wise location of the delamination is difficult
Expert consists of a number of validation             using general type of experts. Ones the span wise
networks, which are train and tested through          location is determined using general type of
same output of a sample data set but with             experts, these conditional experts are trained
different lower dimensional input of the data set.    taking samples from within that location.
These different input data sets come from             Training and Testing of hierarchical network
different dimension reduction procedure of the        In training phase, every multilayer perceptrons
original input set, which is high dimensional         (MLP) are trained and tested with their
sensor output. So, every expert is a mapping          corresponding training and testing samples.
from sensor output to the damage properties of        These training will give their training and testing
the structure and performance of the expert           error. Although network architectures and
depends on the performances of its validation         learning algorithms are same, due to different
networks,      which       is    trained    through   initial condition, learning rate, momentum rate
dimensionally reduced input sample set.               and learning sequence the trained MLPs will be
Committee Machine                                     different. Depending upon the training error
But some times, due to this reduction procedure       every trained MLP is associated with their
the mapping looses the output uniqueness, which       weightage. In the ensemble network these
is essential for the training of neural network. To   weightages and their testing errors are considered
overcome this problem, output space is divided        to calculate average testing error. These testing
with a set of overlapped subsets. Size of these       errors are for every ensembler network. All
subsets are such that the output uniqueness           ensemble networks within one validation
within a subset is preserved as well as sufficient    network calculate are weighted average testing
number of sample data is available to train and       error. This is the training and testing phase of the
test the network. Then for every subset one           hierarchical network. Training and testing phase
expert is trained and tested taking sample data       is limited within ANN and ensembler network.
from these subsets. Similar to the division of        Execution of hierarchical network
output space, input space can be divided in           In identification phase, execution samples (time
different subsets on the basis of sensor, actuator    domain sensor output) are feed into every expert
to get their opinion and confidence. From this       In this paper a numerical study on 12 layered
mutual information the location and size of the      beam containing two patches, one acting as an
delamination is obtained with the level of           actuator and the other as a sensor has been
confidence. Every expert pass on these execution     presented. In order to evaluate the influence of
samples to their subordinates, validation            delamination location and extent on structural
networks after assigned dimension reduction.         dynamic characteristics, the situation with only
These validation networks also pass on the           one delamination is considered in this study. In
sample to ensembler network. Similarly               the finite element model, the delamination is
ensembler network gives these samples to their       modeled keeping two elements in the same
subordinate MLP (ANN) network. These MLP             location, and integrated bottom element from
execute these samples and give their opinion. As     bottom layer to delamination layer and top
different MLP are trained differently, their         element from delaminated layer to top layer. At
opinion will also be different. These opinion and    delaminated zone, two nodes are created in the
their corresponding training weightage will          same places, one is connected with top elements
create opinion and variance for the ensembler        and other is connected with bottom elements.
network. After getting all the ensembler level
information, information on validation network       Forward Analysis
will be created by fusing this ensembler level       Numerical simulation is carried out by
information. In the execution phase of validation    considering a unidirectional laminated composite
network, the opinion and variance of ensembler       beam of total thickness 1.8 mm as shown in
network is used. Opinion of validation network       Figure-1. Length and width of the beam is 500
is created by the opinion of ensembler network       mm and 50 mm respectively. The beam is made
and their corresponding weighted average testing     of 12 layers with thickness of each layer being
error. Similarly variance of validation network is   0.15 mm. Delamination is modeled as explained
created from variance of ensembler network with      in the last section. Parametric studies are done by
their weighted average testing error. If this        changing delamination size span wise of the
opinion is with in the range of inherited expert     cantilever beam for each layer. Position of sensor
and variance is with in their accepted limit, this   is fixed at 9th layer from bottom of the beam and
validation network is considered as active           near the support of the beam, while the position
validation network. As the dimension reduction       of actuator is fixed at 1st layer from bottom of
algorithm is different between different             the beam and 425 mm apart from support. Size
validation networks, one weightage for               of the actuator is 50 mm X 50 mm with 0.15 mm
dimension reduction is used to give more             thickness and size of the sensor is 50 mm X 50
weightage for better algorithm. This operation       mm with 0.3 mm thickness. Elastic modulus of
will be done for all experts. For execution in the   composite is assumed 181 GPa and 10.3 GPa in
expert level, information are fused from             parallel (E1) and perpendicular (E2) direction of
subordinate, validation networks. Active experts     fiber. Poison ratio (ν), density (ρ) and shear
are determined depending upon the maximum            modulus (G12) of composite are taken as 0.0, 1.6
number of active validation network within that      gm/c.c. and 28 GPa respectively. Elastic
expert. Then weighted opinion and weighted           modulus (Em), poison ratio (νm), shear modulus
variance among active validation network are         (Gm) and density (ρm) of magnetostrictive
calculated, as the opinion and variance of the       material are assumed 30 GPa, 0.0, 23 GPa and
hierarchical network (HNN). If more than one         9.25 gm/c.c. respectively. Magneto-mechanical
active expert are available, committee machine       coupling coefficient is 15E-09 m/amp. Direct
calculate the opinion and variance of the HNN        transient dynamic analysis has been done with
considering variance of all active experts.          500 time steps to calculate open circuit voltage
                                                     of the sensor in each time steps. Relative
      4. NUMERICAL EXAMPLES                          permeability µr is the ratio of permeability of the
                                                     material and permeability of air is assumed as 10
for magnetostrictive material. Permeability at       their time integrals are taken as the input space
vacuum or air is 400π nano-Henry/m. Number of        of the four type of validation neural network.
coil turn in sensor (Ns) and actuator (N) is         Every validation network consists of four
assumed 1000. Actuation current at actuator (I) is   ensemble networks. These ensemble networks
taken as 1.0 Amp at three different frequencies.     are trained and tested by same sample data set
                                                     but with different random partitioning between
Result and Discussion                                training and testing data sets. So every ensemble
Numerical results have been simulated for a          network is trained and tested by a fixed set of
fixed position of sensor and actuator (x1 =25mm,     training and testing data sets respectively. In
y1 =0.45mm, w1 =50mm, d1 =0.3mm, x2                  order to identify the delamination length at each
=425mm, y2 =-0.825mm, w2 =50mm, d2                   layer, one BP neural network with 15 inputs and
=0.15mm) combination, for different locations of     2 outputs are designed. One hidden layer of node
the delamination. Open circuit voltages in the       strength 10 is taken as the net architecture.
sensor have been shown in 3-D plot. Figure-2         Every expert is trained by the sample data within
shows open circuit voltages in the sensor when       their expertise location. These samples are for
the delamination is between 4th and 5th layer,       the delamination in the corresponding location.
between 8th and 9th layer with input frequency       Thus there are thirty experts for each actuation
5000Hz.                                              frequency to predict the size and location of the
                                                     delamination. One numerical example is shown
Inverse Problem                                      in the Table-1 for 200mm mid plane
As structural damage information is distributed      delamination. Out of 30 experts, 8 experts are
in different vibration modes, and vibration          active. Committee machine has fused the
modes with high frequencies are generally more       information of these active experts and get the
sensitive to small damage, three different           opinion and variance of HNN. Results give sub-
frequencies (50, 500, 5000Hz) are considered to      mili-meter accuracy in span direction and 5
actuate the actuator. Thus input space is            micrometer accuracy in depth wise direction. As
subdivided in three different subspaces. In this     expert #8 gives the better result hence weightage
study, sinusoidal actuation current is considered    is more. Table-2 shows the result for all
in the actuation coil. Three sin wave excitation     validators of expert #8 and validator #1 gives the
with different frequencies are exerted on the        better result. Table-3 showh the result for all
dynamic model of the composite laminate, and         ensembler and ensembler #4 shows better result.
the vibration responses of 550 different cases are   Table-4 shows the all multi layer perceptron
numerically simulated for each frequency. These      (ANN) for expert #8, validator #1 and ensembler
550 cases include the intact laminate, laminates     #4.
with delamination damage at different layers and     A number of delamination identification is
of 50 different delamination sizes (10 mm to 500     performed using proposed Hierarchical neural
mm) at each layer.                                   network and shown in the Figure-5. It is shown
For structural health monitoring Hierarchical        that depth identification is difficult than span
Neural Network (HNN) is used. Training, testing      wise identification.
and execution procedure of hierarchical neural
network is shown in Figure-4. Vibration                           5. CONCLUSIONS
responses of higher dimension (500 time steps)
for a given delamination (open circuit voltage in    The study demonstrates the use of vibration
magnetostrictive sensor), is preprocessed for        response using magnetostrictive sensor and
dimension reduction in the input space of the        actuator of an in-service structure for health
neural network. Different type of dimension          information of the structure. The study also
reduction (PCA, ICA) can be used. Here for           shows the feasibility of online damage detection
simplicity first fifteen optimum values and their    and health monitoring using hierarchical ANN-
location of the sensor open circuit voltage and      based identification. This study is successful in
classifying and identifying structural damage       10. Krishna Murty, A. V., Anjanappa, M.,
location and severity using the designed                Wang, Z. and Chen, X. Sensing of
hierarchical neural network (HNN). The results          delaminations in composite laminates
show that HNN is a powerful tool for                    using     embedded        magnetostrictive
establishing the mapping relationships between          particle layers, Journal of Intelligent
open circuit voltages and the structural damage         Material Systems Structures, Vol-10
status, and demonstrate the ability of HNN for          October 1999,pp 825-835
structural damage detection.                        11. K. Moslem and R. Nafaspour, Structural
                                                        damage detection by genetic algorithms.
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    5.   Y.J. Yan and L.H. Yam, Online              15. Butler, J.L, Application manual for the
         detection of crack damage in composite         design of Terfenol-D magnetostrictive
         plates using embedded piezoelectric            transducers, Edge Technologies Inc.,
         actuators/sensors and wavelet analysis.        Ames Iowa, 1988.
         Compos. Struct. 58 (2002), pp. 29-38.      16. Kraus, John D. Electromagnetics,
    6.   Nag, A. Roy Mahapatra, D. and                  Fourth      Edition,     McGRAW-HILL
         Gopalakrishnan, S. Identification of           International     Editions,     Electrical
         delamination in a composite beam using         Engineering Series
         a damaged spectral element. Structural     17. Kumar, M., and Krishna Murty, A. V.
         Health Monitoring. Vol-1(2).                   Sensing of delaminations in smart
    7.   Saidha     E.,    Naik     G   N    and        composite laminates, J. Aero. Soc. Of
         Gopalakrishnan, S. An experimental             India, Vol 51, p 7-9, February 1999.
         investigation of a smart laminated         18. Ghosh D. P. and Gopalakrishnan S.;
         composite beam with magnetostrictive           Structural health monitoring in a
         patch      for     health     monitoring       composite beam using magnetostrictive
         applications.      Structural     Health       material through a new FE formulation.
         Minitoring.                                    International Conference on Smart
    8.   Kleinke, D.K and Uras, H.M. A                  Materials, Structures and Systems;
         noncontacting magnetostrictive strain          Dec’12-14, 2002, Indian Institute of
         sensor, Rev. Sci. Instrum. 64, pp.             Science, Bangalore, India.
         2361-2367, 1993.                           19. Ghosh D. P. and Gopalakrishnan S.;
    9.   Anjanappa, M., and Wu, Y. F.                   Identification of delamination size and
         Magnetostrictive particulate actuators:        location of composite laminate from
         configuration,        modeling      and        time domain data of magnetostrictive
         charaterization, Smart Material and            sensor and actuator using artificial
         Structures, 6, 1997, pp. 393-402.              neural network. Proceeding of the SEC
2003,   December   12-14,    structural              engineering convention an international
                                                        meet.


                               FIGURES AND TABLES




            Figure 1: Laminated Beam with Actuator, Sensor and Delamination.




Figure 2: Actuation frequency 5000 Hz                                Figure-3

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Icasi2004

  • 1. Proceedings of ICASI - 2004 International Conference on Advances in Structural Integrity July 14-17, 2004, Indian Institute of Science, Bangalore, India ICASI/XX-XXX Time domain structural health monitoring with magnetostrictive patches using five stage hierarchical neural networks. Ghosh D. P. (a) and Gopalakrishnan S. (b) (a) Graduate student (b) Assoc. professor, Dept. of Aerospace Engineering, Indian Institute of Science, Bangalore 560012 ABSTRACT An integrated method for damage detection of composite laminates is presented in this paper using time domain data obtained from magnetostrictive sensors and actuators and artificial neural networks (ANN) identification with five stage hierarchical neural network (HNN). Magnetostrictive actuators are actuated through an actuation coil, which vibrates the composite laminate. The presence of delamination, due to induced magnetic field intensity, changes the stress response of the structure. This in turn changes the magnetic flux intensity of the magnetostrictive sensor. The changes in the flux density are sensed through a sensing coil as open circuit voltage. The ANN is applied to establish the mapping relationship between structural damage status (location and severity) and sensor open circuit voltage. As ANN is prone to overtraining and the dimension of input space is considerable high, a five-stage hierarchy of networks is used for the identification procedure. The results of delamination damage detection for composite laminate show that the method developed in this paper can be applied to structural damage detection and health monitoring for various industrial structures. To demonstrate this approach, numerical simulations are carried out on a composite cantilever beam to identify size and location of delamination using the sensor data for a known actuation for a certain combination of sensor and actuator locations. Keywords: Magnetostrictive, FEM, SHM, ANN, Hierarchical Neural Network, Inverse Problem. 1. INTRODUCTION may broadly refer to as functional materials. With the availability of functional materials and Composites have revolutionized structural the feasibility of embedding them into or construction. They are extensively used in bonding them to composite structures, smart aerospace, civil, mechanical and other industries. structural concepts are emerging to be attractive Present day aerospace vehicles have composites for potential high performance structural up to 60 % or more of the total material used. applications.1 A smart structure may be generally More recently, materials, which can give rise to defined as one which has the ability to determine mechanical response when subjected to non- its current state, decides in a rational manner on a mechanical loads such as PZTs, Terfenol-D, set of actions that would change its state to a SMAs, have become available. Such materials more desirable state and carries out these actions
  • 2. in a controlled manner over a short period of important ways to ensure reliable operation and time. With such features incorporated in a reduced maintenance cost for in-service structure by embedding functional materials, it is structures. Magnetostrictive material such as feasible to achieve technological advances such Terfenol-D, hitherto considered as only actuator as vibration and noise reduction, high pointing material, was shown to be used for sensing accuracy of antennae, damage detection, damage application in reference.7 In this work, the mitigation etc.2, 3 authors proved this capacity experimentally by passing a magnetic field on to an actuator During the operation of a structure, damages may magnetostrictive patch and measured the voltage develop, which will cause a change in the across the sensing patch to infer the presence of strain/stress state of the structure and the damage. vibration characteristics. By continuously In this paper we take this approach not only to monitoring one or more of these response confirm its presence but also its location. quantities, it is possible to assess the condition of Noncontact magnetostrictive strain sensor was the structure for its structural integrity. Such a explored by Kleinke, D. K. et al.8 and the study monitoring of the structure is called structural of magnetostrictive particulate actuator was done health monitoring. Health monitoring application by Anjanappa, M. et al.9 Sensing of delamination has been receiving great deal of attention all over in composite laminates using embedded the world, due to possible significant impact on magnetostrictive material was studied by Krishna safety and longevity of the structure. To Murty, A. V. et al.10 Authors [18] had developed implement health-monitoring concept it is a new finite element formulation for inbuilt necessary to have a number of sensors to magnetostrictive patches for performing measure response parameters. These responses numerical simulations. will then be post-processed to assess the The mathematical relationships between sensor condition of structure. Mark Lin and Fu-Kuo open circuit voltage and structural damage status Chang 4 built such a system when they developed (i.e., damage location and severity) are very a built-in monitoring system for composite complex. It is not only strongly non-linear, but structures using SMART layer containing a also often has no analytical solution. Deduction network of actuators or sensors. from sensor output to practical damage status is Change of structural dynamic performance mathematically classified as inverse problem, caused by structural damage that is less than 1% and is very hard to compute precise solution of the total structural size is unnoticeable. Yan using mathematical analysis. If one takes the and Yam5 pointed out that when the crack length inherent law between sensor output and practical in a composite plate equals 1% of the plate damage status as a black box, the mapping length, the relative variation of structural natural relationship between these two state spaces can frequency is only about 0.01 to 0.1%. This was be established using genetic algorithms (GAs) or also shown by Nag et al.6 Therefore, using artificial neural networks (ANN). Thus, one need vibration modal parameters, e.g., natural not know explicitly the inherent law in structural frequencies, displacement or strain mode shapes, damage detection. Moslem and Nafaspour11 and and modal damping are generally ineffective in Chou and Ghaboussi12 reported some researches identifying small and incipient structural on structural damage detection using GAs, and damage. It has been theoretically and they were successful in determining the severity experimentally proved that local damage in a and locations of structural damage. However, structure will cause the reduction of local GAs-based structural damage detection requires structural stiffness, which leads to variation of repeatedly searching from numerous damage dynamic performance of the whole structure. In parameters so as to find the optimal solution of industry, using the time domain measured the objective function (measured data). The cost structural vibration responses to identify and of computation limits the use of GA for damage monitor structural damage is one of the detection applications.
  • 3. ANN has particular advantage in establishing with different initial condition, learning rate, accurate mapping relationships between sensor momentum rate, learning algorithm and learning data and physical parameters of structural sequence. damage. When classifications and identification of structural damage needs to be carried out, the In this study, an integrated damage detection required task is only to train the ANN in advance method is developed for composite laminate using a set of known sensor data and damage through theoretical study and numerical physical parameters of the structures that needs simulation. This method requires the generation detection. Hung and Kao13 and Yun and Bahng14 of excitation and structural response reported their researches on structural damage measurement using bonded magnetostrictive detection using ANN, and their results showed patch actuator and sensors; which is used in that ANN is a highly effective tool for hierarchical ANN framework for classification identifying structural damage. and identification of structural damage. By using the hierarchical scheme, a complicated large-scale system is decomposed into a set of 2. FORWARD ANALYSIS lower order subsystems and a coordination Application of magnetic field causes strain in the process, and thus becomes tractable. Hierarchical magnetostrictive material (Terfenol-D) and the structures can have more than two levels. stress, changes magnetic flux density of that However, in practice, two-level structures are material.15 usually popular. Here five stages of hierarchy are The three-dimensional constitutive relationship considered for structural health monitoring case. for magnetostrictive material is generally written As the original sensor output (open circuit as voltage) is high dimensional data hence the ANN input space, it is quite impossible to train the {ε } = [ S {H } ]{σ } + [d ]T {H } (1) network. To reduce the dimension of input space {B} = [d ]{σ } + [ µ {σ } ]{H } (2) of ANN, different dimensional reduction algorithms are used like ICA, PCA, peak value, The Equation- (1) is used as actuator and peak location etc. But some times due to this Equation- (2) is used as sensor in the composite dimensional reduction procedure, damage structure. Using these two equations, the time signatures are lost in the lower dimension data, domain sensor response due to actuation in the which leads to lose of the essential output actuator can be computed through finite element uniqueness of ANN mapping. Here to deal with formulation [18]. In the forward analysis for a this problem, output space is partitioned in given actuation history and a given damage different overlapped subspace and different condition, sensor response history can be experts are trained in these partitions. With in obtained for a particular structure. Where as, in every expert, a number of validator networks are inverse problem, either actuation history or trained. All of them have the same set of sample damage condition is unknown. Detail procedure data in higher dimensional input space, but with for forward analysis can be obtained from [18]. different lower dimensional input space coming from different dimensional reduction procedures. Every ANN are trained and validated by a fixed 3. INVERSE ANALYSIS set of sample set. Single validator network is Inverse problem can be classified in two consisting of different ensembler network using category, force inverse problem and geometry different partitioning of training set and inverse problem. In the force inverse problem, validation set from the sample set. Similarly actuation history is unknown but the structure single ensembler network is also classified with and its response is known. In geometry inverse different multi layer perceptron (ANN). These problem applied force and response of structure ANNs have different network architecture are known but structure is unknown. Damage (hidden layers, hidden nodes), and are trained identification is the geometric inverse problem, which can be solved by artificial neural network.
  • 4. 3.1 Artificial Neural Network the minimal training error. A small learning rate Artificial neural networks (ANNs) can provide results in long learning times. A relatively large non-linear parameterized mapping between a set learning rate results in faster learning but can of inputs and a set of outputs with unknown also result in a chaotically learning behavior function relationship. Thus ANNs are universal during training of the network. The function of function approximators and are therefore the momentum term is to increase the size of the attractive for automatically learning of the (non- learning steps when the direction in the weight linear) functional relation between the input update is the same as the direction in the variables and the output variables. A three-layer previous step. As with the learning rate, if the network (Figure-1) with the sigmoid activation momentum term is too large the network will functions can approximate any smooth mapping. display a chaotic learning behavior. A typical supervised feed-forward multi layer If many training epochs are used, an ANN tends neural network is called as a back propagation to overtrain the learning material (i.e. the (BP) neural network. The structure of a BP accuracy on the training material is very high neural network mainly includes the input layer whereas the accuracy on new instances is much for receiving input data; the hidden layer for lower). In this work over training is avoided by processing data; and the output layer to indicate dividing the training set into two groups, and the identified results. In this study, ability of using one group of patterns to train the network identifying structural damage status for an ANN while the other one is used for validating the is acquired through training the neural network performance of the trained network. It was using the known samples. Normally, many observed that the training error decreases along training epochs are required before a set of with number of epoch while the validation error weights is found that accurately fit the training decreases at first, bounces around, and then starts material. increasing. The optimal learning is achieved at The training of a BP neural network is a two-step the global minimum of validation error. procedure. In the first step, the network If the number of hidden units in ANN is too propagates input through each layer until an small, the modeling capacity of the network is output is generated. The error between the output too low, and it is impossible for the learning rule and the target output is then computed. In the to find an adequate model. If, on the other hand, second step, the calculated error is transmitted the number of hidden units is too large, the backwards from the output layer and the weights modeling capacity of the network is too are adjusted to minimize the error. The training substantial, resulting in a strong inclination process is terminated when the error is towards overlearning. sufficiently small for all training samples. The Committee Machine data set is separated into two parts, one for It is perhaps impossible to combine simplicity training and the other for testing or validating the and accuracy in a single model of ANN. Single network performance. The network parameters multi-layered perceptron (MLP) uses a black box are determined, as is common practice, through approach to globally fit a single function into the experimentation. This includes the number of data, thereby losing insight into the problem. hidden nodes and the learning rates. Data This problem was studied [19] by partitioning obtained from the magnetostrictive sensors the input and output space into a piecewise set of described above, is used to train conventional subspaces, with each subspace having its own back propagation networks to identify the expert. delamination size and location of the composite Hierarchical Neural Network laminate. With the common three-layer neural network The accuracy of a trained network is measured architectures, networks lack internal structure; as by calculating the mean square error (MSE) on a consequence, it is very difficult to discern the training sample. The learning rate determines characteristics of the knowledge acquired by a the size of the steps in the search space to find network in order to evaluate its reliability and
  • 5. applicability. Alternative neural-network error gives more weightage of the neural architecture is presented, based on a hierarchical network. In the execution phase, these organization shown in Figure-3. By using the weightages are used to get weighted average of hierarchical scheme, a complicated large-scale all neural networks output as the output of system is decomposed into a set of lower order ensemble network. From the distribution of the subsystems and a coordination process, and thus output of different neural networks and their becomes tractable. A five-stage hierarchical corresponding weightage one measure of neural network is designed by combining a overtraining can be computed. If the outputs of multilayer perceptron first stage and mixture-of- different neural network are close (at least for experts in the subsequent stages. The second those has more weightage) then networks are stage mixture-of-experts, ensembler network, well trained otherwise it is overtrained. Every learns to minimize the overtraining errors. The trained neural network is tested through the test third stage mixture-of-experts, validation data set, which gives the testing errors as a network, learns to minimize the validation errors. measure of generalization of the neural networks. And the fourth stage mixture-of-experts, expert These testing errors with the weightages of the networks, learns to minimize the error of network neural networks give the weighted average of due to loss of information for input space testing error, as a measure of testing error of the dimension reduction. And Finally fifth stage ensemble network. Next issue in the neural committee machine choose the appropriate expert network is the generalization of the network network from all expert networks. Each lower using the testing error of ensemble network. level subsystem is solved independently for a Validation Network fixed value of the coordination variable whose As, every neural network within the ensemble value is adjusted by the upper level coordination network is trained with same training sample; unit in an appropriate fashion so that the lower these neural networks need testing for level subsystems resolve their problems. The generalization of the ensemble network. For coordination is to provide a solution to the testing of network, sample data set is separated overall system. Continuous exchange of into two groups, one for training and other for information between the lower subsystems and testing (validation). After training of neural the upper coordination unit will finally lead to a networks, with the training sample, the neural better solution. The whole procedure is discussed networks simulate the testing sample and get the as follows. testing error. These testing errors with their Ensemble Network weightages give the measure of generalization of Often artificial neural networks are prone to the ensemble network. However, every network overtraining, where network trains the in the ensemble network is trained and tested computational and experimental noises. And through the same set of training data set and there is no direct rule to draw the line between testing data set respectively. To get a more well training and overtraining for a set of training general input-output mapping from a set of examples and network architecture. One of the sample data set, different division of training indirect ways to get a measure of overtraining of sample and testing sample is essential. This can the network is Ensemble Network. In ensemble be done through a systematic manner using network, a number of neural networks are train validation network. Validation Network consists with the same training samples but with different of some number of ensemble networks. These initial condition, learning rate, training ensemble networks are trained and tested with algorithm, network architecture and training same sample data set with different partition for sequence (for sequential learning). In training training data set and testing data set. However, phase, each network trains and generates training every validation network is train for a fixed set error for the training samples. On the basis of of sample data set. these training errors, weightages of the trained Dimensional Reduction of Input Space neural network is determined, where less training
  • 6. In time domain structural health monitoring, time and actuation combination. But as the input histories of the sensor outputs (open circuit space subdivision is known a’ priory, committee voltages) are the original input space for the machine for input space subdivision is not input-output mapping, which is very high required. dimensional. So, it is not possible to train the Conditional Expert network taking full dimension of the original Always some dimension of output space is input space (sensor output). To address this difficult to train than other dimension of output issue, different dimension reduction procedures space. In SHM of composite laminate, depth are available in the literature, which can reduce wise training is difficult than span wise training. the dimension of the original input space keeping To solve this kind of problem some conditional main features of the high dimensional data. But experts are trained. If the dimension of output for structural health monitoring, suitable subset of some expert is less than the original dimension reduction procedure is not available, dimension of output space, the value for the which will reduce the dimension of the input missing dimension is required a ‘priory to space preserving the signature of damage from execute the network. These experts are called the high dimensional sensor output data. To Conditional Expert. Conditional experts are used overcome this problem a number of reductions to get finer location for some dimensions in the procedure is taken to increase the chance of output space, when locations for remaining preserving the damage signature in the reduced dimensions are already known by other type of input data sets. In the next section this issue is experts. For structural health monitoring problem discussed in a systematic manner. in composite laminate, identification of layer Expert wise location of the delamination is difficult Expert consists of a number of validation using general type of experts. Ones the span wise networks, which are train and tested through location is determined using general type of same output of a sample data set but with experts, these conditional experts are trained different lower dimensional input of the data set. taking samples from within that location. These different input data sets come from Training and Testing of hierarchical network different dimension reduction procedure of the In training phase, every multilayer perceptrons original input set, which is high dimensional (MLP) are trained and tested with their sensor output. So, every expert is a mapping corresponding training and testing samples. from sensor output to the damage properties of These training will give their training and testing the structure and performance of the expert error. Although network architectures and depends on the performances of its validation learning algorithms are same, due to different networks, which is trained through initial condition, learning rate, momentum rate dimensionally reduced input sample set. and learning sequence the trained MLPs will be Committee Machine different. Depending upon the training error But some times, due to this reduction procedure every trained MLP is associated with their the mapping looses the output uniqueness, which weightage. In the ensemble network these is essential for the training of neural network. To weightages and their testing errors are considered overcome this problem, output space is divided to calculate average testing error. These testing with a set of overlapped subsets. Size of these errors are for every ensembler network. All subsets are such that the output uniqueness ensemble networks within one validation within a subset is preserved as well as sufficient network calculate are weighted average testing number of sample data is available to train and error. This is the training and testing phase of the test the network. Then for every subset one hierarchical network. Training and testing phase expert is trained and tested taking sample data is limited within ANN and ensembler network. from these subsets. Similar to the division of Execution of hierarchical network output space, input space can be divided in In identification phase, execution samples (time different subsets on the basis of sensor, actuator domain sensor output) are feed into every expert
  • 7. to get their opinion and confidence. From this In this paper a numerical study on 12 layered mutual information the location and size of the beam containing two patches, one acting as an delamination is obtained with the level of actuator and the other as a sensor has been confidence. Every expert pass on these execution presented. In order to evaluate the influence of samples to their subordinates, validation delamination location and extent on structural networks after assigned dimension reduction. dynamic characteristics, the situation with only These validation networks also pass on the one delamination is considered in this study. In sample to ensembler network. Similarly the finite element model, the delamination is ensembler network gives these samples to their modeled keeping two elements in the same subordinate MLP (ANN) network. These MLP location, and integrated bottom element from execute these samples and give their opinion. As bottom layer to delamination layer and top different MLP are trained differently, their element from delaminated layer to top layer. At opinion will also be different. These opinion and delaminated zone, two nodes are created in the their corresponding training weightage will same places, one is connected with top elements create opinion and variance for the ensembler and other is connected with bottom elements. network. After getting all the ensembler level information, information on validation network Forward Analysis will be created by fusing this ensembler level Numerical simulation is carried out by information. In the execution phase of validation considering a unidirectional laminated composite network, the opinion and variance of ensembler beam of total thickness 1.8 mm as shown in network is used. Opinion of validation network Figure-1. Length and width of the beam is 500 is created by the opinion of ensembler network mm and 50 mm respectively. The beam is made and their corresponding weighted average testing of 12 layers with thickness of each layer being error. Similarly variance of validation network is 0.15 mm. Delamination is modeled as explained created from variance of ensembler network with in the last section. Parametric studies are done by their weighted average testing error. If this changing delamination size span wise of the opinion is with in the range of inherited expert cantilever beam for each layer. Position of sensor and variance is with in their accepted limit, this is fixed at 9th layer from bottom of the beam and validation network is considered as active near the support of the beam, while the position validation network. As the dimension reduction of actuator is fixed at 1st layer from bottom of algorithm is different between different the beam and 425 mm apart from support. Size validation networks, one weightage for of the actuator is 50 mm X 50 mm with 0.15 mm dimension reduction is used to give more thickness and size of the sensor is 50 mm X 50 weightage for better algorithm. This operation mm with 0.3 mm thickness. Elastic modulus of will be done for all experts. For execution in the composite is assumed 181 GPa and 10.3 GPa in expert level, information are fused from parallel (E1) and perpendicular (E2) direction of subordinate, validation networks. Active experts fiber. Poison ratio (ν), density (ρ) and shear are determined depending upon the maximum modulus (G12) of composite are taken as 0.0, 1.6 number of active validation network within that gm/c.c. and 28 GPa respectively. Elastic expert. Then weighted opinion and weighted modulus (Em), poison ratio (νm), shear modulus variance among active validation network are (Gm) and density (ρm) of magnetostrictive calculated, as the opinion and variance of the material are assumed 30 GPa, 0.0, 23 GPa and hierarchical network (HNN). If more than one 9.25 gm/c.c. respectively. Magneto-mechanical active expert are available, committee machine coupling coefficient is 15E-09 m/amp. Direct calculate the opinion and variance of the HNN transient dynamic analysis has been done with considering variance of all active experts. 500 time steps to calculate open circuit voltage of the sensor in each time steps. Relative 4. NUMERICAL EXAMPLES permeability µr is the ratio of permeability of the material and permeability of air is assumed as 10
  • 8. for magnetostrictive material. Permeability at their time integrals are taken as the input space vacuum or air is 400π nano-Henry/m. Number of of the four type of validation neural network. coil turn in sensor (Ns) and actuator (N) is Every validation network consists of four assumed 1000. Actuation current at actuator (I) is ensemble networks. These ensemble networks taken as 1.0 Amp at three different frequencies. are trained and tested by same sample data set but with different random partitioning between Result and Discussion training and testing data sets. So every ensemble Numerical results have been simulated for a network is trained and tested by a fixed set of fixed position of sensor and actuator (x1 =25mm, training and testing data sets respectively. In y1 =0.45mm, w1 =50mm, d1 =0.3mm, x2 order to identify the delamination length at each =425mm, y2 =-0.825mm, w2 =50mm, d2 layer, one BP neural network with 15 inputs and =0.15mm) combination, for different locations of 2 outputs are designed. One hidden layer of node the delamination. Open circuit voltages in the strength 10 is taken as the net architecture. sensor have been shown in 3-D plot. Figure-2 Every expert is trained by the sample data within shows open circuit voltages in the sensor when their expertise location. These samples are for the delamination is between 4th and 5th layer, the delamination in the corresponding location. between 8th and 9th layer with input frequency Thus there are thirty experts for each actuation 5000Hz. frequency to predict the size and location of the delamination. One numerical example is shown Inverse Problem in the Table-1 for 200mm mid plane As structural damage information is distributed delamination. Out of 30 experts, 8 experts are in different vibration modes, and vibration active. Committee machine has fused the modes with high frequencies are generally more information of these active experts and get the sensitive to small damage, three different opinion and variance of HNN. Results give sub- frequencies (50, 500, 5000Hz) are considered to mili-meter accuracy in span direction and 5 actuate the actuator. Thus input space is micrometer accuracy in depth wise direction. As subdivided in three different subspaces. In this expert #8 gives the better result hence weightage study, sinusoidal actuation current is considered is more. Table-2 shows the result for all in the actuation coil. Three sin wave excitation validators of expert #8 and validator #1 gives the with different frequencies are exerted on the better result. Table-3 showh the result for all dynamic model of the composite laminate, and ensembler and ensembler #4 shows better result. the vibration responses of 550 different cases are Table-4 shows the all multi layer perceptron numerically simulated for each frequency. These (ANN) for expert #8, validator #1 and ensembler 550 cases include the intact laminate, laminates #4. with delamination damage at different layers and A number of delamination identification is of 50 different delamination sizes (10 mm to 500 performed using proposed Hierarchical neural mm) at each layer. network and shown in the Figure-5. It is shown For structural health monitoring Hierarchical that depth identification is difficult than span Neural Network (HNN) is used. Training, testing wise identification. and execution procedure of hierarchical neural network is shown in Figure-4. Vibration 5. CONCLUSIONS responses of higher dimension (500 time steps) for a given delamination (open circuit voltage in The study demonstrates the use of vibration magnetostrictive sensor), is preprocessed for response using magnetostrictive sensor and dimension reduction in the input space of the actuator of an in-service structure for health neural network. Different type of dimension information of the structure. The study also reduction (PCA, ICA) can be used. Here for shows the feasibility of online damage detection simplicity first fifteen optimum values and their and health monitoring using hierarchical ANN- location of the sensor open circuit voltage and based identification. This study is successful in
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  • 10. 2003, December 12-14, structural engineering convention an international meet. FIGURES AND TABLES Figure 1: Laminated Beam with Actuator, Sensor and Delamination. Figure 2: Actuation frequency 5000 Hz Figure-3