<?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">ENG</journal-id><journal-title-group><journal-title>Engineering</journal-title></journal-title-group><issn pub-type="epub">1947-3931</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/eng.2021.1311041</article-id><article-id pub-id-type="publisher-id">ENG-113087</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>
 
 
  Determination of Correction Values of Operating Reliability of Assembly Components of the Assembly—Front Spinner Spinning Box (R1 Rieter) on the Basis of Operating Data
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Slobodan</surname><given-names>Stefanović</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Korabayev</surname><given-names>Sherzod Ahmadjonovich</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Shoxobiddinova</surname><given-names>Dilafruz Erkinzonqizi</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Academy of Technical and Educational Vocational Studies, Nis, Serbia</addr-line></aff><aff id="aff2"><addr-line>Department of Technology of Products of Textile Industry, Namangan Institute of Engineering and Technology, Namangan, Uzbekistan</addr-line></aff><pub-date pub-type="epub"><day>10</day><month>11</month><year>2021</year></pub-date><volume>13</volume><issue>11</issue><fpage>565</fpage><lpage>573</lpage><history><date date-type="received"><day>1,</day>	<month>July</month>	<year>2021</year></date><date date-type="rev-recd"><day>8,</day>	<month>November</month>	<year>2021</year>	</date><date date-type="accepted"><day>11,</day>	<month>November</month>	<year>2021</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>
 
 
  The optimal safety model includes the values of the operation of the components with the allowed risk, and it is clearly seen that the belt of absolutely safe operation of the analyzed circuit is located between the values of the displayed dependence curves M<sub>ξ</sub>(t)<sub>BP</sub>
   
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  es have been carried out to ensure the flawless operation of the OE machine and the consistency of product quality.
 
</p></abstract><kwd-group><kwd>Surrender Box</kwd><kwd> Open-End (OE)</kwd><kwd> Reliability</kwd><kwd> Exploitation</kwd><kwd> Spinning</kwd><kwd> Yarn</kwd><kwd> Tension</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction—Description of the Box Spinning Assembly (Heart OE Spinner)</title><p>The power transition system of the spinning box assembly is shown in <xref ref-type="fig" rid="fig1">Figure 1</xref> and consists of the following components which are classified on the basis of the processing flow of the carded sliver (raw material to be processed).</p><p>When the operational values of reliability are determined, which express the approximate values of reliability of the components of the analyzed assembly with maximum safety (areas of their safe operation time and areas of reduction</p><p>of their reliability), their correction values were used for more precise determination. This was aimed at obtaining the most accurate reliability values for determining the total transfer function of the reliability of the components of the analyzed assembly [<xref ref-type="bibr" rid="scirp.113087-ref1">1</xref>] [<xref ref-type="bibr" rid="scirp.113087-ref2">2</xref>] [<xref ref-type="bibr" rid="scirp.113087-ref3">3</xref>].</p><p>The correction values of reliability from the exploitation data are shown in <xref ref-type="fig" rid="fig2">Figure 2</xref> to <xref ref-type="fig" rid="fig3">Figure 3</xref>, and their tabular values within the presented figures.</p><p>Reliability correction values are obtained as a quotient of the empirical distribution density function from empirical values ( f e ( t ) ) and failure intensity functions ( λ e ( t ) ) for the time interval of the operational operation of the components of the assemblies (the analysis included the service life of the components of the assembly in the duration 13000 ≤ Δ t i ≤ 21000 hours) and are determined by the expression:</p><p>P i ( t ) = f e i ( t ) λ e i ( t ) .</p><p>The obtained correction values will further serve in the formation of tables of values of the transfer functions of the spinning box assembly G B P ( t ) on the basis of which the shapes of the curves are determined f ( G B P ( t ) , t ) which determine the form of statistical distribution of reliability, i.e. the shape of the curve adopts the distribution of reliability that best suits their shape [<xref ref-type="bibr" rid="scirp.113087-ref4">4</xref>] [<xref ref-type="bibr" rid="scirp.113087-ref5">5</xref>].</p><p>Conclusion: From the shape of the curve of the correction values of the reliability</p><p>of the components of the analyzed assembly P i ( t ) , i.e. according to the slope of the curve, confidence intervals can be analytically predicted which will later be used as a basis in determining the relevant reliability (reliability obtained from the statistical distribution) [<xref ref-type="bibr" rid="scirp.113087-ref6">6</xref>] [<xref ref-type="bibr" rid="scirp.113087-ref7">7</xref>] [<xref ref-type="bibr" rid="scirp.113087-ref8">8</xref>].</p><p>The analysis showed the following conclusions:</p><p>1) Analysis of the reliability of the operation of the components of the analyzed assemblies without the application of preventive maintenance technology procedures:</p><p>&#183; Components A8, A9, A10 have the highest reliability in operation, whose reliability is maximum and amounts P A 8 ( t ) = P A 9 ( t ) = P A 10 ( t ) = 1.0 and lasts in a time interval over Δ t i ≥ 20000 ( h ) .</p><p>&#183; Based on the shape of the curve f ( P i ( t ) , t ) , i.e. according to their slope, <xref ref-type="table" rid="table1">Table 1</xref> shows the order of reliability values and component operating times.</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Values of the correction reliability interval depending on the analyzed time interval of operation of the components of the analyzed assemblies on which the procedures of preventive maintenance technology have not been applied</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Component designation</th><th align="center" valign="middle" >Time interval of the analyzed work of the component Δ t 1 ≤ Δ t i ≤ Δ t 2</th><th align="center" valign="middle" >Confidence interval for the analyzed time interval Δ P i 1 ≤ Δ P i ≤ Δ P i 2</th></tr></thead><tr><td align="center" valign="middle"  colspan="3"  >Boxing spinning assembly</td></tr><tr><td align="center" valign="middle" >A6</td><td align="center" valign="middle" >13,000 &#247; 14,000</td><td align="center" valign="middle" >1.0 &#247; 0.828</td></tr><tr><td align="center" valign="middle" >A5</td><td align="center" valign="middle" >13,000 &#247; 14,000</td><td align="center" valign="middle" >1.0 &#247; 0.9 &#247; 0.868</td></tr><tr><td align="center" valign="middle" >A7</td><td align="center" valign="middle" >13,000 &#247; 16,000</td><td align="center" valign="middle" >1.0 &#247; 0.514</td></tr><tr><td align="center" valign="middle" >E1</td><td align="center" valign="middle" >13,000 &#247; 14,000</td><td align="center" valign="middle" >1.0 &#247; 0.615</td></tr><tr><td align="center" valign="middle" >A3</td><td align="center" valign="middle" >13,000 &#247; 14,000</td><td align="center" valign="middle" >1.0 &#247; 0.72</td></tr><tr><td align="center" valign="middle" >A4</td><td align="center" valign="middle" >13,000 &#247; 16,000</td><td align="center" valign="middle" >1.0 &#247; 0.523</td></tr><tr><td align="center" valign="middle" >A1</td><td align="center" valign="middle" >13,000 &#247; 14,000</td><td align="center" valign="middle" >1.0 &#247; 0.951 &#247; 0.927</td></tr><tr><td align="center" valign="middle" >A2</td><td align="center" valign="middle" >13,000 &#247; 14,000</td><td align="center" valign="middle" >1.0 &#247; 0.952 &#247; 0.927</td></tr><tr><td align="center" valign="middle" >E2</td><td align="center" valign="middle" >13,000 &#247; 16,000</td><td align="center" valign="middle" >1.0 &#247; 0.806</td></tr></tbody></table></table-wrap><p>The analysis included confidence intervals after the first lower value than the maximum.</p><p>2) Analysis of the reliability of the components of the analyzed assemblies with the application of preventive maintenance technology procedures:</p><p>&#183; Components A8, A9, A10 have the highest reliability in operation, whose reliability is maximum and amounts P A 8 − 0 ( t ) = P A 9 − 0 ( t ) = P A 10 − 0 ( t ) = 1.0 and lasts in a time interval over Δ t i ≥ 20000 ( h ) .</p><p>&#183; And lasts in a time interval over f ( P i − 0 ( t ) , t ) , i.e. according to their slope, the order of values of reliability and operating time of components during these reliability is shown in the table (<xref ref-type="table" rid="table2">Table 2</xref>). The analysis included confidence intervals after the first lower value than the maximum.</p></sec><sec id="s2"><title>2. Determination of the Statistical Method of Reliability Distribution of the Analyzed Assembly</title><p>In order to determine the statistical method of reliability distribution, it is necessary to form models and determine the transfer reliability functions of the analyzed assembly [<xref ref-type="bibr" rid="scirp.113087-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.113087-ref10">10</xref>]. To determine the transfer function tables of the spinning box assembly G<sub>BP</sub>(t) reliability corrections were used P<sub>i</sub>(t)</p><sec id="s2_1"><title>2.1. Model Formation and Determination of Transfer Functions of Reliability of Analyzed Assembly Based on Empirical Data</title><p>The formation of the model included the arrangement of the components of the assemblies according to the processing of the yarn, i.e. according to the labels in the order of the components in the failure tree.</p><p>The components are arranged in sequence on the assembly, from the introductory</p><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Values of the correction reliability interval depending on the analyzed time interval of the components of the analyzed assemblies on which the procedures of preventive maintenance technology have been applied</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Component designation</th><th align="center" valign="middle" >Time interval of the analyzed work of the component Δ t 1 − 0 ≤ Δ t i − 0 ≤ Δ t 2 − 0</th><th align="center" valign="middle" >Confidence interval for the analyzed time interval Δ P i − 01 ≤ Δ P i − 0 ≤ Δ P i − 02</th></tr></thead><tr><td align="center" valign="middle"  colspan="3"  >Boxing spinning assembly</td></tr><tr><td align="center" valign="middle" >A6</td><td align="center" valign="middle" >13,000 &#247; 15,000</td><td align="center" valign="middle" >1.0 &#247; 0.8</td></tr><tr><td align="center" valign="middle" >A5</td><td align="center" valign="middle" >13,000 &#247; 15,000</td><td align="center" valign="middle" >1.0 &#247; 0.88</td></tr><tr><td align="center" valign="middle" >A7</td><td align="center" valign="middle" >13,000 &#247; 16,000</td><td align="center" valign="middle" >1.0 &#247; 0.7</td></tr><tr><td align="center" valign="middle" >E1</td><td align="center" valign="middle" >13,000 &#247; 15,000</td><td align="center" valign="middle" >1.0 &#247; 0.475</td></tr><tr><td align="center" valign="middle" >A3</td><td align="center" valign="middle" >13,000 &#247; 15,000</td><td align="center" valign="middle" >1.0 &#247; 0.831</td></tr><tr><td align="center" valign="middle" >A4</td><td align="center" valign="middle" >13,000 &#247; 16,300</td><td align="center" valign="middle" >1.0 &#247; 0.67</td></tr><tr><td align="center" valign="middle" >A1</td><td align="center" valign="middle" >13,000 &#247; 15,000</td><td align="center" valign="middle" >1.0 &#247; 0.376</td></tr><tr><td align="center" valign="middle" >A2</td><td align="center" valign="middle" >13,000 &#247; 15,000</td><td align="center" valign="middle" >1.0 &#247; 0.522</td></tr><tr><td align="center" valign="middle" >E2</td><td align="center" valign="middle" >13,000 &#247; 16,300</td><td align="center" valign="middle" >1.0 &#247; 0.8</td></tr></tbody></table></table-wrap><p>channel to the yarn waxing mechanism in the spinning box.</p><p>For these reasons, the block diagram model is shown. The model is more complex and includes the arrangement of components in the spinning box, taking into account their functionality and purpose, so that the reduction of complex block diagram structures has been performed.</p><p>Based on the obtained final expressions of the transfer functions of the analyzed circuits G<sub>P</sub>(t)<sub>BP</sub> for boxing spinning), and in them by replacing the reliability values of the components P<sub>i</sub>(t) for time intervals 13000 ( h ) ≤ Δ t i ≤ 20000 ( h ) tabular values are obtained by reliability significance belts, from which the reliability curves of the transfer functions of the analyzed assembly are constructed (<xref ref-type="table" rid="table3">Table 3</xref>).</p><p>1) Block diagram model of the transmission reliability function in a spinning box assembly</p><p>For solving reduction of this model, its step-by-step solution will be performed when obtaining the transfer function of the circuit reliability G<sub>P</sub>(t)<sub>BP</sub>. As can be seen from <xref ref-type="fig" rid="fig4">Figure 4</xref>, this is an open system of automatic reliability management [<xref ref-type="bibr" rid="scirp.113087-ref11">11</xref>] [<xref ref-type="bibr" rid="scirp.113087-ref12">12</xref>].</p><p>X(t)</p><p>Step I: Determining partial reliability blocks</p><p>P p 1 ( t ) = P E 1 ( t ) ⋅ P A 7 ( t ) , P p 2 ( t ) = P A 4 ( t ) + P A 3 ( t ) , P p 3 ( t ) = P A 1 ( t ) ⋅ P A 2 ( t ) , P p 4 ( t ) = P A 8 ( t ) + P E 2 ( t ) , P P 5 ( t ) = P A 9 ( t ) + P A 10 ( t )</p><p>Step II (<xref ref-type="fig" rid="fig5">Figure 5</xref>)</p><p>The values of the partial reliability blocks are:</p><p>P p 6 ( t ) = P A 6 ( t ) + P P 1 ( t ) , P P 7 ( t ) = P p 4 ( t ) + P p 1 ( t ) .</p><table-wrap id="table3" ><label><xref ref-type="table" rid="table3">Table 3</xref></label><caption><title> Values of transmission reliability functions of spinning box assembly depending on the value of its reliability</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Reliability values P<sub>i</sub>(t)</th><th align="center" valign="middle"  colspan="2"  >Portable spinning subsystem reliability function G<sub>P</sub>(t)<sub>BP</sub></th></tr></thead><tr><td align="center" valign="middle" >1.0</td><td align="center" valign="middle"  rowspan="9"  >Shaded areas represent the ultimate limit of satisfactory reliability in the analysis</td><td align="center" valign="middle" >16</td></tr><tr><td align="center" valign="middle" >0.9</td><td align="center" valign="middle" >8.078</td></tr><tr><td align="center" valign="middle" >0.8</td><td align="center" valign="middle" >3.775</td></tr><tr><td align="center" valign="middle" >0.7</td><td align="center" valign="middle" >1.6</td></tr><tr><td align="center" valign="middle" >0.6</td><td align="center" valign="middle" >0.5972</td></tr><tr><td align="center" valign="middle" >0.5</td><td align="center" valign="middle" >0.1875</td></tr><tr><td align="center" valign="middle" >0.4</td><td align="center" valign="middle" >0.0458</td></tr><tr><td align="center" valign="middle" >0.2</td><td align="center" valign="middle" >0.0006</td></tr><tr><td align="center" valign="middle" >0</td><td align="center" valign="middle" >0</td></tr></tbody></table></table-wrap><p>Note: The shaded areas included values because values below this limit are not taken into account (they include areas in which the assembly needs to be repaired, which will be discussed more when determining the reliability values in cases of selected statistical distribution).</p><p>Step III (<xref ref-type="fig" rid="fig6">Figure 6</xref>)</p><p>The values of the partial reliability blocks are: G B P = P P 6 ( t ) ⋅ P A 1 ( t ) ⋅ P P 2 ( t ) ⋅ P P 3 ( t ) ⋅ P P 7 ( t ) .</p><p>The final equation of the reliability value based on the partial reliability values for the box spinning assembly is:</p><p>G B P ( t ) = Y P ( t ) X P ( t ) = ( P A 6 ( t ) + P P 1 ( t ) ) ⋅ P A 5 ( t ) ⋅ ( P A 4 ( t ) + P A 3 ( t ) )     ⋅ P A 1 ( t ) ⋅ P A 2 ( t ) ⋅ ( P P 4 ( t ) + P P 5 ( t ) ) = ( P A 6 ( t ) + P E 1 ( t ) ⋅ P A 7 ( t ) ) ⋅ P A 5 ( t ) ⋅ ( P A 4 ( t ) + P A 3 ( t ) )       ⋅ P A 1 ( t ) ⋅ P A 2 ( t ) ⋅ ( P A 8 ( t ) + P E 2 ( t ) + P A 9 ( t ) + P A 10 ( t ) ) = P A 1 ( t ) ⋅ P A 2 ( t ) ⋅ P A 5 ( t ) ⋅ { ( P A 6 ( t ) + P E 1 ( t ) ⋅ P A 7 ( t ) ) } ( P A 4 ( t ) + P A 3 ( t ) )       ⋅ ( P A 8 ( t ) + P E 2 ( t ) + P A 9 ( t ) + P A 10 ( t ) )</p><p>G B P ( t ) p = P A 1 ( t ) ⋅ P A 2 ( t ) ⋅ P A 5 ( t ) ⋅ ( P A 4 ( t ) + P A 3 ( t ) )     ⋅ { ( P A 6 ( t ) + P E 1 ( t ) ⋅ P A 7 ( t ) ) } ( P A 8 ( t ) + P E 2 ( t ) + P A 9 ( t ) + P A 10 ( t ) )</p></sec><sec id="s2_2"><title>2.2. Tableof the Transmission Function of the Spinning Box Assembly with Approximation G<sub>P</sub>(T)<sub>BP</sub></title><p><xref ref-type="table" rid="table3">Table 3</xref> is formed on the basis of the final expressions of the transfer reliability functions depending on the time interval of operation of the circuits.</p><p>The value of the transmission function of the spinning box assembly reliability is shown in a table (<xref ref-type="table" rid="table3">Table 3</xref>). Based on the obtained values, a graphical representation of the dependence was performed f(G<sub>P</sub>(t)<sub>BP</sub>,t) (<xref ref-type="fig" rid="fig7">Figure 7</xref>).</p></sec></sec><sec id="s3"><title>3. Conclusion</title><p>Guilty f(G<sub>P</sub>(t)<sub>BP</sub>,t), corresponds to long normal curves according to their shape, so for that reason a long normal distribution will be taken for the selection of the statistical reliability distribution. According to this distribution, the reliability of each component of the analyzed assembly will be corrected. The optimal safety model includes the values of the operation of the components with the allowed risk, and it is clearly seen that the belt of absolutely safe operation of the analyzed circuit is located between the values of the displayed dependence curves M<sub>ξ</sub>(t)<sub>BP</sub> = f(t). And also, analyses have been carried out to ensure the flawless operation of the OE machine and the consistency of product quality.</p></sec><sec id="s4"><title>Conflicts of Interest</title><p>The authors declare no conflicts of interest regarding the publication of this paper.</p></sec><sec id="s5"><title>Cite this paper</title><p>Stefanović, S., Ahmadjonovich, K.S. and Erkinzonqizi, S.D. (2021) Determination of Correction Values of Operating Reliability of Assembly Components of the Assembly—Front Spinner Spinning Box (R1 Rieter) on the Basis of Operating Data. Engineering, 13, 565-573. https://doi.org/10.4236/eng.2021.1311041</p></sec></body><back><ref-list><title>References</title><ref id="scirp.113087-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Blanchard, B. And Fabrysky, W. (1981) System Engineering and Analysis. Prentice Hall Inc., New Jersey.</mixed-citation></ref><ref id="scirp.113087-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">Brehmer, L. (1975) Technishe Diegnostik in der Flugzeuginstandhalting. Information der ziliven Luftfahrt, 11.</mixed-citation></ref><ref id="scirp.113087-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">Connor, P.M. (1981) Structured Analysis in Desing Technique. Sistems Analysis and Designa Foundation for the 1980, Norht_Holland, New York.</mixed-citation></ref><ref id="scirp.113087-ref4"><label>4</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Stefanovic</surname><given-names> S. </given-names></name>,<etal>et al</etal>. (<year>2012</year>)<article-title>Determination of the Value of Selected Oscillation Frequency Measurement Point Analyzed Parts OE Spinning—On the Box Spinning</article-title><source> International Journal of Mechanical Engineering Research and Development</source><volume> 2</volume>,<fpage> 27</fpage>-<lpage>37</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.113087-ref5"><label>5</label><mixed-citation publication-type="other" xlink:type="simple">Stefanovic, S. (2006) The Influence of Mechanical Vibration on the Occurrence of Functional Safety Circuits in the Power Transmission System of Textile Machines. Ph.D. Thesis, University of Novi Sad, Novi Sad.</mixed-citation></ref><ref id="scirp.113087-ref6"><label>6</label><mixed-citation publication-type="other" xlink:type="simple">Slobodan, S., et al. (2013) Research into the Causes of Inaccuracies of Components of Complex for Coil Winding with Finished Yern at OE. Journal of Process Management. New Technologies, 1, 16-26.</mixed-citation></ref><ref id="scirp.113087-ref7"><label>7</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>Stefanovic</surname><given-names> S. </given-names></name>,<etal>et al</etal>. (<year>2013</year>)<article-title>The Analysis of Functioning of Basic Components of OE— Technical System</article-title><source> International Journal of Engineering</source><volume> 11</volume>,<fpage> 237</fpage>-<lpage>244</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.113087-ref8"><label>8</label><mixed-citation publication-type="other" xlink:type="simple">Korabayev, Sh.A., Mardonovich, M. , Lolashbayevich, M. and Xaydarоvich, M. (2019) Determination of the Law of Motion of the Yarn in the Spin Intensifier. Engineering, 11, 300-306. https://doi.org/10.4236/eng.2019.115021https://www.scirp.org/journal/paperinformation.aspx?paperid=92784</mixed-citation></ref><ref id="scirp.113087-ref9"><label>9</label><mixed-citation publication-type="other" xlink:type="simple">Korabayev, Sh.A., Matismailov, S.L., Yuldashev, A.T. and Atanbayev D.D. (2020) Study of Fiber Movement Outside the Crater of Pnevmomechanical Spinning Machine. Solid State Technology, 63, 3460-3466. http://www.solidstatetechnology.us/index.php/JSST/article/view/3473</mixed-citation></ref><ref id="scirp.113087-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">Dimitrijevic, N., Stefanovic, S., Mladenovic, S. and Vojislav, V. (2019) Use of Intelligent Systems for Electronic Stability of Motor Vehicles. Knowledge International Journal, 35, 961-966.</mixed-citation></ref><ref id="scirp.113087-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">Dimitrijevic, N., Stefanovic, S., Mladenovic, S. and Krstic, V. (2019) Use Of Gps Systems for Movement and Monitoring Vehicle in Road Traffic. Knowledge International Journal, 35, 955-960.</mixed-citation></ref><ref id="scirp.113087-ref12"><label>12</label><mixed-citation publication-type="other" xlink:type="simple">Dimitrijevic, N., Stefanovic, S., Mladenovic, S. and Krstic, V. (2019) Use of Intelligent Systems on the Dynamic Stability of Cars. Knowledge International Journal, 35, 973-978.</mixed-citation></ref></ref-list></back></article>