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  <front>
    <journal-meta>
      <issn pub-type="ppub">1613-0073</issn>
    </journal-meta>
    <article-meta>
      <title-group>
        <article-title>of structural properties of Ni-Ti shape memory alloy by the supervised machine learning methods</article-title>
      </title-group>
      <contrib-group>
        <contrib contrib-type="author">
          <string-name>Oleh Yasniy</string-name>
          <email>oleh.yasniy@gmail.com</email>
          <xref ref-type="aff" rid="aff1">1</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Nadiia Lutsyk</string-name>
          <email>lutsyk.nadiia@gmail.com</email>
          <xref ref-type="aff" rid="aff1">1</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Vladyslav D</string-name>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Halyna Osukhivsk</string-name>
          <email>osukhivska@tntu.edu.ua</email>
          <xref ref-type="aff" rid="aff1">1</xref>
        </contrib>
        <contrib contrib-type="author">
          <string-name>Workshop</string-name>
        </contrib>
        <aff id="aff0">
          <label>0</label>
          <institution>Ivano-Frankivsk National Medical University</institution>
          ,
          <addr-line>Galytska Str. 2, Ivano-Frankivsk, 76018</addr-line>
          ,
          <country country="UA">Ukraine</country>
        </aff>
        <aff id="aff1">
          <label>1</label>
          <institution>Ternopil Ivan Puluj National Technical University</institution>
          ,
          <addr-line>Ruska str. 56, Ternopil, 46008</addr-line>
          ,
          <country country="UA">Ukraine</country>
        </aff>
      </contrib-group>
      <abstract>
        <p>Shape memory alloys (SMAs) possess unique properties, namely, they retain their original form after loading while being, for instance, heated. The structural properties of pseudoelastic NiTi SMA, such as the dependencies of stress and strain range upon the number of loading cycles, were studied by employing the methods of supervised machine learning (ML). The obtained results are quite accurate, which can be seen from the calculated mean average error (MSE) and root mean squared error (RMSE). In general, ML methods can be utilized to solve such kinds of tasks very efficiently. machine learning, neural network, random forest, NiTi shape memory alloy, stress and strain Shape memory alloys (SMAs) 'memorise' or retain their initial shape when under the action of thermomechanical or magnetic fields [1]. SMAs have gained vast attention recently in a wide range of applications, that are based on their peculiar properties, namely, in products [2], structural elements [3], automotive [4], aerospace [5, 6], mini actuators and micro-electromechanical systems (MEMS) [7, 8], etc. Therefore, due to their ubiquitous widespread, it is highly important to study their structural properties, namely, the dependencies of stress and strain upon the number of loading cycles. A number of related computer modelling and simulations was performed in the studies [9-11]. Since the testing procedures are often quite costly and time-consuming, it is advisable to use the methods of artificial intelligence (AI), specifically, machine learning (ML) approaches. The number of tasks was solved efficiently by ML methods in the papers [12-14]. Thus, the aim of this paper was to predict the dependencies of stress and strain ranges upon number of loading cycles for NiTi SMA utilizing the supervised ML methods. Proceedings ITTAP'2023: 3rd International Workshop on Information Technologies: Theoretical and Applied Problems, November 22-24, ORCID: 0000-0002-9820-9093 (A. 1); 0000-0002-0361-6471 (A. 2); 0000-0002-7663-9332 (A. 3); 0000-0003-0132-1378 (A. 4); 0000-0003Proceedings</p>
      </abstract>
    </article-meta>
  </front>
  <body>
    <sec id="sec-1">
      <title>-</title>
      <p>ranges</p>
    </sec>
    <sec id="sec-2">
      <title>1. Introduction</title>
    </sec>
    <sec id="sec-3">
      <title>Methods</title>
      <p>The dependencies of stress range and strain on the number of loading cycles for the four specimens,
that were taken from study [15] were predicted by methods of machine learning in the programming
platform Orange 3.34.0 [16]. This software allows to build visually the flowcharts and obtain the results
in the form of models, numerical data and plots.</p>
      <p>2020 Copyright for this paper by its authors.
CEUR</p>
      <p>ceur-ws.org</p>
      <p>In general, for each of four specimens, two model were built. On the input of each model there were
given the dependencies of the respective physical quantity on the number of loading cycles. The number
of loading cycles was treated as an independent variable, and the physical quantity was chosen as a
dependent variable. To increase the accuracy of modelling results, the dataset was augmented. The data
augmentation was performed by interpolating the original experimental data by 1-Dimensional Akima
spline. Akima spline is a type of non-smoothing spline that gives good fits to curves where the second
derivative is changing fast [17].</p>
      <p>For each specimen, the dataset was split into two unequal parts. The training dataset contained 66%
of the total dataset. The regression dependencies were built by methods of random forests, neural
networks, gradient boosting, support vector machines (SVM), AdaBoost, and k-nearest neigbors
methods. Each of the obtained models was checked additionally by k-fold cross-validation method 10
times. Fig. 1 shows the flowchart of one model, built in the programming environment Orange.</p>
    </sec>
    <sec id="sec-4">
      <title>3. Results and discussion</title>
      <p>There was performed the estimation of structural properties of specimens, made of NiTi SMAs. In
general, there were tested 4 specimens. The number of specimen, as well as the sample size for stress
and strain range versus the number of loading cycles are presented in Table 1.</p>
      <p>Table 1. Specimen number and sample sizes for stress and strain ranges versus the number of loading
cycles.
The lowest errors for specimen # 10 were shown by Ada Boost and kNN for Δε, and random forest
and kNN for Δσ. Fig. 2 (a, b, c, d) displays the plots of predicted versus true values of the respective
physical quantities, built by the afore-mentioned ML methods.</p>
      <sec id="sec-4-1">
        <title>a) Δε Ada Boost b) Δε kNN</title>
      </sec>
      <sec id="sec-4-2">
        <title>c) Δσ Random Forest d) Δσ kNN Figure 2: The predicted versus true values of physical quantities. a) built for Δε by means of Ada boost method; b) built for Δε by means of kNN method; c) built for Δσ using Random Forest method; d) built for Δσ using kNN method</title>
        <p>As it can seen from Fig. 2, the calculated points are very close to the bisector of the first coordinate
angle, that confirms the high prediction accuracy.</p>
        <p>The modelling was also performed for the specimen #13.</p>
        <p>Table 3 contains the prediction errors and correlation coefficient for Δε and Δσ, estimated for
specimen # 13 using various ML methods.</p>
      </sec>
      <sec id="sec-4-3">
        <title>Prediction errors and correlation coefficient for Δε and Δσ, built for specimen # 13 using various supervised ML methods</title>
      </sec>
      <sec id="sec-4-4">
        <title>Specimen # 13 Δε Δσ</title>
      </sec>
      <sec id="sec-4-5">
        <title>Model RMSE MAE R2 RMSE MAE R2</title>
        <p>Ada Boost 0.071 0.008 0.981 0.607 0.176 1.000
Gradient Boosting 0.071 0.010 0.981 0.619 0.225 1.000
kNN 0.078 0.007 0.977 0.557 0.112 1.000
Neural Network 0.235 0.176 0.796 1.165 0.718 0.998
Random Forest 0.074 0.008 0.980 0.544 0.155 1.000</p>
        <p>SVM 0.144 0.080 0.923 13.615 12.797 0.770
For this particular specimen, the lowest errors were obtained by employing Ada Boost and kNN for
Δε, and random forest and kNN for Δσ.</p>
        <p>The plots of predicted versus true values of the respective physical quantities, built by the
aforementioned ML methods for specimen # 13 can be seen on Fig 3 (a, b, c, d).</p>
      </sec>
      <sec id="sec-4-6">
        <title>a) Δε Ada Boost b) Δε kNN</title>
      </sec>
      <sec id="sec-4-7">
        <title>c) Δσ Random Forest d) Δσ kNN Figure 3: The predicted versus true values of physical quantities for specimen # 13 a) built for Δε by means of Ada boost method; b) built for Δε by means of kNN method; c) built for Δσ using Random</title>
        <p>Table 4 contains the forecast errors and correlation coefficient for Δε and Δσ, built for specimen #
16 using several supervised ML methods.</p>
        <p>For the specimen # 16, the lowest errors were obtained by employing Ada Boost and kNN for Δε,
and random forest and kNN for Δσ.</p>
        <p>Table 5 presents the errors and correlation coefficient for Δε and Δσ, obtained for specimen # 17 by
means of different ML methods.</p>
        <p>For the specimen #17, the lowest errors were obtained by Random Forest and kNN for Δε and Δσ.</p>
      </sec>
    </sec>
    <sec id="sec-5">
      <title>4. Conclusions</title>
      <p>There were predicted the structural properties of pseudoelastic NiTi SMA, namely, the dependencies
of stress and strain range upon the number of loading cycles, by employing the methods of supervised
learning methods. The predicted versus true values of those two physical quantities were built. They
are very close to the bisector of the first coordinate angle, which confirms high prediction accuracy.
The best results in terms of RMSE and MSE were shown by Ada Boost and kNN for Δε, and by Random
forest and kNN for Δσ. It can be further concluded, that the methods of supervised ML can efficiently
predict the afore-mentioned dependencies, and are the promising method to solve such kinds of tasks.
5. References
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the Institution of Mechanical Engineers, Part G: Journal of Aerospace Engineering, vol. 221, no.
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[7] L. Sun et al., Stimulus-responsive shape memory materials: A review, Materials in Engineering,
vol. 33, Jan. (2012): 577–640, doi: 10.1016/j.matdes.2011.04.065.
[8] M. Kohl. Shape Memory Microactuators (Microtechnology and MEMS). 1 ed. Heidelberg:</p>
      <p>Springer-Verlag Berlin, (2010).
[9] Petryk, M.R., Khimich, A., Petryk, M.M., Fraissard, J. Experimental and computer simulation
studies of dehydration on microporous adsorbent of natural gas used as motor fuel, 2019. Fuel239,
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[10] Okipnyi, I.B., Maruschak, P.O., Zakiev, V.I. et al. Fracture Mechanism Analysis of the
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[12] Alyamani, A., &amp; Yasniy, O. Classification of EEG signal by methods of machine learning. Applied</p>
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[13] O. Yasniy, I. Didych, and Y. Lapusta, Prediction of fatigue crack growth diagrams by methods of
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[15] Volodymyr Iasnii, Petro Yasniy, Yuri Lapusta, Tetiana Shnitsar. Experimental study of
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      </p>
    </sec>
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