<?xml version="1.0" encoding="UTF-8"?><!DOCTYPE article  PUBLIC "-//NLM//DTD Journal Publishing DTD v3.0 20080202//EN" "http://dtd.nlm.nih.gov/publishing/3.0/journalpublishing3.dtd"><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" dtd-version="3.0" xml:lang="en" article-type="research article"><front><journal-meta><journal-id journal-id-type="publisher-id">OJCE</journal-id><journal-title-group><journal-title>Open Journal of Civil Engineering</journal-title></journal-title-group><issn pub-type="epub">2164-3164</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ojce.2013.32012</article-id><article-id pub-id-type="publisher-id">OJCE-32514</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Engineering</subject></subj-group></article-categories><title-group><article-title>
 
 
  Damage Detection Method Using Support Vector Machine and First Three Natural Frequencies for Shear Structures
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>ien</surname><given-names>HoThu</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Akira</surname><given-names>Mita</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of System Design Engineering, Keio University, Yokohama, Japan</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>thuhienjolie@gmail.com(IH)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>30</day><month>05</month><year>2013</year></pub-date><volume>03</volume><issue>02</issue><fpage>104</fpage><lpage>112</lpage><history><date date-type="received"><day>March</day>	<month>21,</month>	<year>2013</year></date><date date-type="rev-recd"><day>April</day>	<month>22,</month>	<year>2013</year>	</date><date date-type="accepted"><day>April</day>	<month>30,</month>	<year>2013</year></date></history><permissions><copyright-statement>&#169; Copyright  2014 by authors and Scientific Research Publishing Inc. </copyright-statement><copyright-year>2014</copyright-year><license><license-p>This work is licensed under the Creative Commons Attribution International License (CC BY). http://creativecommons.org/licenses/by/4.0/</license-p></license></permissions><abstract><p>
 
 
   A method is proposed for detecting damage to shear structures by using Support Vector Machine (SVM) and only the first three natural frequencies of the translational modes. This method is able to determine the damage location in any story of a shear building with only two vibration sensors; to obtain modal frequencies, one sensor on the ground detects an input and the other on the roof detects the output. Based on the shifts in the first three natural frequencies, damage location indicators are proposed, and used as new feature vectors for SVM. Simulations of five-story, nine-story and twenty-one-story shear structures and experiments on a five-story steel model were used to test the performance of the proposed method.
     
 
</p></abstract><kwd-group><kwd>Support Vector Machine; Damage Detection; Natural Frequency; System Identification; Damage Location Indicator</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Structural health monitoring (SHM) has become a major focus of research in the area of structural dynamics. Many damage detection algorithms based on the modal properties of a structure including the natural frequencies, mode shapes, curvature mode shapes and modal flexibilities have been studied for several decades. However, most algorithms have difficulty identifying the precise location and magnitude of the damage. Moreover, even if such identification is possible, the accuracy and reliability of the properties are not sufficient [<xref ref-type="bibr" rid="scirp.32514-ref1">1</xref>].</p><p>Although frequency shift methods are simple and easy to apply, they have significant practical limitations. For instance, the measurements have to be very precise if the level of damage is not great. In addition, the change in the natural frequency associated with a certain mode in a structure does not provide any spatial information about where the damage occurred, because modal frequencies are global properties of the structure. Salawu [<xref ref-type="bibr" rid="scirp.32514-ref2">2</xref>] presented a review on detection of structural damage through changes in frequency. The approach is based on the fact that natural frequencies are sensitive indicators of structural integrity. The relationship between frequency changes and structural damage was discussed.</p><p>In 1998, Doebling et al. [<xref ref-type="bibr" rid="scirp.32514-ref3">3</xref>] reviewed the literature on vibration-based damage identification methods. Many of the methods use changes in the natural frequencies to detect damage. The amount of literature is large; they comprise not only applications to various structures, but also theoretical work on the use of frequency shifts for damage detection.</p><p>Many methods perform well at frequency-based damage identification in small degrees of freedom. For larger engineering structures, the number of obtained natural frequencies is less than the number of structural elements. This is one of the reasons why frequency change methods have limited abilities to detect damage [<xref ref-type="bibr" rid="scirp.32514-ref4">4</xref>]. To overcome these problems, some researchers have been using the substructure method [<xref ref-type="bibr" rid="scirp.32514-ref5">5</xref>], error matrix method [<xref ref-type="bibr" rid="scirp.32514-ref6">6</xref>], sensitivity-based method [<xref ref-type="bibr" rid="scirp.32514-ref7">7</xref>], combine sensitivity and statistical-based methods [<xref ref-type="bibr" rid="scirp.32514-ref8">8</xref>], and so on.</p><p>The SVM is a powerful tool for pattern recognition and it seems useful for detecting the location of damage. This requires data from the undamaged and damaged structure successfully train and classify the structure into damaged and undamaged classes. SVM has better generalization performance than other methods of problems of damage detection and location [<xref ref-type="bibr" rid="scirp.32514-ref9">9</xref>]. Meyer [<xref ref-type="bibr" rid="scirp.32514-ref10">10</xref>] presented a benchmark study comparing the performance of SVMs with other classification techniques for natural and artificial datasets.</p><p>Previous studies [11-15] conducted at the Mita Laboratory of Keio University, demonstrated that damage detection methods using SVM worked well in many cases. The scope of this work is to develop an improved method to identify the location of damage by using a limited number of sensors. We know that a natural frequency change associated with a certain mode does not provide spatial information about structural damage, but multiple natural frequency changes can give such information. However, in practical situations, the obtained natural frequencies are usually smaller than the degrees of freedoms. The proposed method only requires the first three natural frequencies. The first three natural frequencies are used to obtain the new damage location indicators. These indicators are the feature vectors for pattern recognition.</p></sec><sec id="s2"><title>2. Damage Detection of Structures Using Support Vector Machine</title><sec id="s2_1"><title>2.1. Sensitivity of Damage Location Indicators</title><p>The r<sup>th</sup> natural circular frequency,&#160;<img src="6-1880092\7d44eb5b-8592-482d-910d-66233dc71a6f.jpg" />, of an N-degreeof-freedom (as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>) undamaged structure was given as Equation (9) in [<xref ref-type="bibr" rid="scirp.32514-ref16">16</xref>]:</p><disp-formula id="scirp.32514-formula121002"><label>(1)</label><graphic position="anchor" xlink:href="6-1880092\798d7858-094e-4379-9272-3e28942d6c64.jpg"  xlink:type="simple"/></disp-formula><p>where <img src="6-1880092\914c9d49-828f-4a50-8b46-1c68e19596fc.jpg" /> is the first frequency of undamaged structure.</p><disp-formula id="scirp.32514-formula121003"><label>(2)</label><graphic position="anchor" xlink:href="6-1880092\76c9a83c-45d9-4789-9b3e-0a1ca4709397.jpg"  xlink:type="simple"/></disp-formula><p>The wave propagation constant <img src="6-1880092\07c861df-797f-442b-b21b-d12ff84275fb.jpg" /> mode of safe state can be defined as:</p><disp-formula id="scirp.32514-formula121004"><label>(3)</label><graphic position="anchor" xlink:href="6-1880092\76bd368d-164a-4cff-8186-683bf6322640.jpg"  xlink:type="simple"/></disp-formula><p>Moreover, the <img src="6-1880092\7a990c34-5d99-428a-b3eb-607e84a7b151.jpg" /> mode of the i<sup>th</sup> element damaged state was calculated by:</p><disp-formula id="scirp.32514-formula121005"><label>(4)</label><graphic position="anchor" xlink:href="6-1880092\0d009a16-7add-4fff-beaf-9612ed32be6d.jpg"  xlink:type="simple"/></disp-formula><p>The change <img src="6-1880092\16c1a7c3-c4f4-476b-b917-26d0dcb8e852.jpg" /> due to damage <img src="6-1880092\3d52ed09-f293-4966-bd9a-831c8cef1d1c.jpg" /> to the i<sup>th</sup> element, can be obtained from Equation (28) in [<xref ref-type="bibr" rid="scirp.32514-ref17">17</xref>]:</p><disp-formula id="scirp.32514-formula121006"><label>(5)</label><graphic position="anchor" xlink:href="6-1880092\2271ac03-f8f6-4bed-ac65-a6d0006921bb.jpg"  xlink:type="simple"/></disp-formula><p>From Equation (5) above, it can be seen that the change, <img src="6-1880092\db8e503b-dfc5-4758-87fe-5d6061a4d843.jpg" />, depends only on the location of damage (i) and the degree of freedom N.</p><p>The change <img src="6-1880092\ae77f1f1-b42d-45f1-a930-0dd43251d306.jpg" /> in the r<sup>th</sup> natural circular frequency due to <img src="6-1880092\a478c5d5-59eb-445c-9b75-165ed34d824b.jpg" /> can be found by combining Equations (3)- (5):</p><disp-formula id="scirp.32514-formula121007"><label>(6)</label><graphic position="anchor" xlink:href="6-1880092\d1cdccc7-5be0-47df-83c4-119d589a8abe.jpg"  xlink:type="simple"/></disp-formula><p>The change in the natural frequency can be calculated from Equations (1) and (6):</p><disp-formula id="scirp.32514-formula121008"><label>(7)</label><graphic position="anchor" xlink:href="6-1880092\6916f23e-d55c-4e3a-a00e-5f5ba3d059cb.jpg"  xlink:type="simple"/></disp-formula><p>which is the same as Equation (29b) in [<xref ref-type="bibr" rid="scirp.32514-ref17">17</xref>].</p><p>The above relation showed that the damage was related to the shifts in the natural frequencies. The ratio of the change in the r<sup>th</sup> and s<sup>th</sup> frequencies can be used as a pattern depending on the location of the damage:</p><disp-formula id="scirp.32514-formula121009"><label>(8)</label><graphic position="anchor" xlink:href="6-1880092\16e5ac84-5418-4dc6-94ab-3717e7f44df9.jpg"  xlink:type="simple"/></disp-formula><p>Equation (8) demonstrates the sensitivity of the change in ratio of the shift of a few natural frequencies to the location of the damage. This should be able to be used as a damage location index.</p></sec><sec id="s2_2"><title>2.2. Construction of Feature Vectors for Support Vector Machine</title><p>The sensitivity analysis ideally involves all natural frequencies. However, in some cases, not all of the natural frequencies are available. Therefore, the errors due to incomplete mode parameters should be accounted.</p><p>To solve this problem, we define new damage location indicators that have good pattern recognition ability with only the first three natural frequencies. By using the ratio in Equation (8), we defined two damage location indicators:</p><disp-formula id="scirp.32514-formula121010"><label>(9a)</label><graphic position="anchor" xlink:href="6-1880092\ea8f4f9b-962a-451f-833d-687a0240d74d.jpg"  xlink:type="simple"/></disp-formula><disp-formula id="scirp.32514-formula121011"><label>(9b)</label><graphic position="anchor" xlink:href="6-1880092\72155bfd-1c90-46eb-9788-0265a9f7c0e0.jpg"  xlink:type="simple"/></disp-formula><p>The changes in <img src="6-1880092\0a0381ce-b8c5-4556-974f-5d5df0f0e085.jpg" /> and <img src="6-1880092\b7efadfb-a677-457f-8236-09dbedf3fbb5.jpg" /> can be used as feature vectors. They may be able to be used as to identify the damage location by using a few lower modal frequencies.</p></sec><sec id="s2_3"><title>2.3. Support Vector Machine</title><p>The Support Vector Machine (SVM) is a mechanical learning system that uses a hypothesis space of linear functions in a high dimensional feature space [18,19]. It has been used for structural damage detection because of its ability to form an accurate boundary from a small amount of training data.</p><p>The simplest model, Linear SVM (LSVM), works when the data are linearly separable in the original feature space. In most cases, nonlinear classification using the same procedure as in LSVM is possible as a result of introducing nonlinear functions called Kernel functions without having to be conscious of the actual mapping space. This extension to nonlinear feature spaces is called Nonlinear SVM (NSVM) (<xref ref-type="fig" rid="fig2">Figure 2</xref>).</p></sec></sec><sec id="s3"><title>3. Numerical Verification</title><p>To show the feasibility of the proposed method, N-story structures were modeled as one-dimensional lumped mass shear models, as shown in <xref ref-type="fig" rid="fig1">Figure 1</xref>. Structures with N = 5, 9 and 21 stories were analyzed. Three percent was chosen as the damping ratio for all modes. The data sampling frequency was 200 Hz.</p><p>A reduction in the story stiffness was regarded as damage to the structure. Training feature vectors were generated by assuming three levels of stiffness reduction, 10%, 20%, and 30%, for each story, and the corresponding feature vectors <img src="6-1880092\e9d73e18-a923-4625-b698-7c0bc90b58f1.jpg" /> were generated for each damage pattern. A feature vector consisting of zero elements was used to indicate the undamaged structure.</p><p>Assuming five levels of stiffness reduction, 8%, 16%,</p><p>24%, 32% and 40% for each story, (5 &#215; N) feature vectors were used to verify the proposed method. The first five data corresponded to 8%, 16%, 24%, 32% and 40% stiffness reductions in the first story. The second five data are for the stiffness reduction in the second, third, etc., sets of five data were for the stiffness reductions in the second, third story, and so on. The last data indicated the no damage case.</p><p>SVMi denotes a machine that distinguishes the pattern with damage in the i<sup>th</sup> story from the other patterns.</p><sec id="s3_1"><title>3.1. Five-story Shear Structures (N = 5)</title><p>We considered a five-story structure with the same mass and the same stiffness for all stories: m<sub>i </sub>= 1000 ton, k<sub>i </sub>= 2 &#215; 10<sup>3</sup> MN/m.</p><p>The undamaged natural frequencies of the structure were obtained as 2.03, 5.91, 9.32, 11.98 and 13.66 Hz for the 1<sup>st</sup>, 2<sup>nd</sup>, 3<sup>rd</sup>, 4<sup>th</sup> and 5<sup>th</sup> modes, respectively.</p><p>As mentioned above, a reduction in story stiffness was regarded as damage to the structure. Five damage cases (damage to the 1<sup>st</sup>, 2<sup>nd</sup>, 3<sup>rd</sup>, 4<sup>th</sup> and 5<sup>th</sup> stories) were studied.</p><p><xref ref-type="fig" rid="fig3">Figure 3</xref> shows the output of SVMi with the feature vectors being the change in the first three modal frequencies <img src="6-1880092\4696ff40-1f9b-4aca-8bc5-b5d887e539e2.jpg" /> of the previous method [12-14]. Here, we can see some miss-classifications in the outputs of SVM1 and SVM3.</p></sec></sec></body><back><ref-list><title>References</title><ref id="scirp.32514-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">A. Mita, “Structural Dynamic for Health Monitoring,” Sankeisha Co., Ltd, Nagoya, 2003.</mixed-citation></ref><ref id="scirp.32514-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">O. S. Salawu, “Detection of Structural Damage through Changes in Frequency: A Review,” Engineering Structures, Vol. 19, No. 9, 1997, pp. 718-723.  
doi:10.1016/S0141-0296(96)00149-6</mixed-citation></ref><ref id="scirp.32514-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">S. Doebling, et al., “Damage Identification and Health Monitoring of Structural and Mechanical Systems from Changes in Their Vibration Characteristics: A Literature Review,” Los Alamos National Laboratory, Los Alamos, 1998.</mixed-citation></ref><ref id="scirp.32514-ref4"><label>4</label><mixed-citation publication-type="other" xlink:type="simple">N. Stubbs, T. H. Broome and R. Osegueda, “Non-Destructive Construction Error Detection in Large Space Structures,” AIAA Journal, Vol. 28, No. 1, 1990, pp. 146-152. doi:10.2514/3.10365</mixed-citation></ref><ref id="scirp.32514-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">Z. Xing and A. Mita, “A Substructure Approach to Local Damage Detection of Shear Structure,” Structural Control and Health Monitoring, Vol. 19, No. 2, 2011, pp. 309-318. doi:10.1002/stc.439</mixed-citation></ref><ref id="scirp.32514-ref6"><label>6</label><mixed-citation publication-type="other" xlink:type="simple">J. Sidhu and D. J. Ewins, “Correlation of Finite and Model Test Studies of a Practical Structure,” Proceedings of the 2nd International Modal Analysis Conference, Society for Experimental Mechanics, USA, 1984, pp. 756-762.</mixed-citation></ref><ref id="scirp.32514-ref7"><label>7</label><mixed-citation publication-type="other" xlink:type="simple">H. P. Zhu and Y. L. Xu, “Damage Detection of Mono Coupled Periodic Structures Based on Sensitivity Analysis of Modal Parameter,” Journal of Sound and Vibration, Vol. 285, No. 1-2, 2005, pp. 365-390. 
doi:10.1016/j.jsv.2004.08.012</mixed-citation></ref><ref id="scirp.32514-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">A. Messina, E. J. Williams and T. Contursi, “Structural Damage Detection by a Sensitivity and Statistical-Based Method,” Journal of Sound and Vibration, Vol. 216, No. 5, 1998, pp. 791-808. doi:10.1006/jsvi.1998.1728</mixed-citation></ref><ref id="scirp.32514-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">B. Samanta, K. B. Al-Balushi and S. A. Al-Araimi, “Artificial Neural Networks and Support Vector Machines with Genetic Algorithm for Bearing Fault Detection,” Engineering Applications of Artificial Intelligence, Vol. 16, No. 7-8, 2003, pp. 657-665. 
doi:10.1016/j.engappai.2003.09.006</mixed-citation></ref><ref id="scirp.32514-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">D. Meyer, F. Leisch and K. Hornik, “The Support Vector Machine under Test,” Neurocomputing, Vol. 55, No. 1-2, 2003, pp. 169-186. doi:10.1016/S0925-2312(03)00431-4</mixed-citation></ref><ref id="scirp.32514-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">A. Mita and H. Hagiwara, “Quantitative Damage Diagnosis of Shear Structures Using Support Vector Machine,” KSCE Journal of Civil Engineering, Vol. 7, No. 6, 2003, pp. 683-689. doi:10.1007/BF02829138</mixed-citation></ref><ref id="scirp.32514-ref12"><label>12</label><mixed-citation publication-type="other" xlink:type="simple">M. Shimada and A. Mita, “Damage Assessment of Bending Structures Using Support Vector Machine,” Smart Structures and Material 2005: Sensors and Smart Structures Technologies for Civil, Mechanical and Aerospace, San Diego, 2005, pp. 923-930.</mixed-citation></ref><ref id="scirp.32514-ref13"><label>13</label><mixed-citation publication-type="other" xlink:type="simple">M. Shimada, A. Mita and M. Q. Feng, “Damage Assessment of Structures Using Support Vector Machines under Various Boundary Conditions,” Smart Structures and Material 2006: Sensors and Smart Structures Technologies for Civil, Mechanical and Aerospace Systems, San Diego, 2006.</mixed-citation></ref><ref id="scirp.32514-ref14"><label>14</label><mixed-citation publication-type="other" xlink:type="simple">R. Taniguchi and A. Mita, “Support Vector Machine Based Active Damage Detection Method,” Proceedings of the 4th International Workshop on Structural Health Monitoring, Stanford University, Stanford, 2003, pp. 749-756.</mixed-citation></ref><ref id="scirp.32514-ref15"><label>15</label><mixed-citation publication-type="other" xlink:type="simple">A. Mita and A. Fujimoto, “Active Active Detection of Loosened Bolts Using Ultrasonic Waves and Support Vector Machines,” Proceeding of the 5th International Workshop on Structural Health Monitoring, Stanford University, Stanford, 2005, pp. 1017-1024.</mixed-citation></ref><ref id="scirp.32514-ref16"><label>16</label><mixed-citation publication-type="other" xlink:type="simple">J. E. Luco, H. L. Wong and A. Mita, “Active Control of the Seismic Response of Structures by Combined Use of Base Isolation and Absorbing Boundaries,” Earthquake Engineering and Structural Dynamics, Vol. 21, 1992, pp. 525-541. doi:10.1002/eqe.4290210606</mixed-citation></ref><ref id="scirp.32514-ref17"><label>17</label><mixed-citation publication-type="other" xlink:type="simple">H. Zhu and M. Wu, “The Characteristic Receptance Method for Damage Detection in Large Mono-Coupled Periodic Structures,” Journal of Sound and Vibration, Vol. 251, No. 2, 2002, pp. 241-259.  
doi:10.1006/jsvi.2001.3988</mixed-citation></ref><ref id="scirp.32514-ref18"><label>18</label><mixed-citation publication-type="other" xlink:type="simple">V. N. Vapnik, “The Nature of Statistical Learning Theory,” Springer, Berlin, 1995.  
doi:10.1007/978-1-4757-2440-0</mixed-citation></ref><ref id="scirp.32514-ref19"><label>19</label><mixed-citation publication-type="other" xlink:type="simple">N. Christianini and J. Shawe-Taylor, “Support Vector Machines and Other Kernel-Based Learning Methods,” Cam bridge University Press, Cambridge, 2000.</mixed-citation></ref><ref id="scirp.32514-ref20"><label>20</label><mixed-citation publication-type="other" xlink:type="simple">M. Verhaegen and P. Dewilde, “Subspace Model Identification Part 1: The Output-Error State-Space Model Identification Class of Algorithms,” International Journal of Control, Vol. 56, No. 5, 1992, pp. 1187-1210.  
doi:10.1080/00207179208934363</mixed-citation></ref></ref-list></back></article>