<?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">OALibJ</journal-id><journal-title-group><journal-title>Open Access Library Journal</journal-title></journal-title-group><issn pub-type="epub">2333-9705</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/oalib.1106075</article-id><article-id pub-id-type="publisher-id">OALibJ-98569</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Biomedical&amp;Life Sciences</subject><subject> Business&amp;Economics</subject><subject> Chemistry&amp;Materials Science</subject><subject> Computer Science&amp;Communications</subject><subject> Earth&amp;Environmental Sciences</subject><subject> Engineering</subject><subject> Medicine&amp;Healthcare</subject><subject> Physics&amp;Mathematics</subject><subject> Social Sciences&amp;Humanities</subject></subj-group></article-categories><title-group><article-title>
 
 
  Stability and Adaptive Control with Sychronization of 3-D Dynamical System
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Maysoon</surname><given-names>M. Aziz</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>Dalya</surname><given-names>M. Merie</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>Department of Mathematics, College of Computer Sciences and Mathematics, University of Mosul, Mosul, Iraq</addr-line></aff><pub-date pub-type="epub"><day>03</day><month>02</month><year>2020</year></pub-date><volume>07</volume><issue>02</issue><fpage>1</fpage><lpage>18</lpage><history><date date-type="received"><day>14,</day>	<month>January</month>	<year>2020</year></date><date date-type="rev-recd"><day>25,</day>	<month>February</month>	<year>2020</year>	</date><date date-type="accepted"><day>28,</day>	<month>February</month>	<year>2020</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 three-dimensional system is presented with unknown parameters that employs two nonlinearities terms. The basic characteristics of the system are studied. The stability is measured by Characteristic equation roots, Routh stability criteria, Hurwitz stability criteria and Lapiynov function, all show that the system unstable. Then, Chaoticity is measured by maximum Lapiynov exponent of (<em>L</em><sub>max</sub>=2.509426) and “Kaplan-Yorke” dimension (<em>D<sub>L</sub></em>=2.22349544). The system is controlled effectively and synchronized by designed adaptive controllers. Furthermore, the theoretical and graphic results of the system before and after control are compared. 
 
</p></abstract><kwd-group><kwd>Stabilization</kwd><kwd> Dissipative System</kwd><kwd> Adaptive Control</kwd><kwd> Lapiynov Exponent</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>Researches in recent years on chaotic phenomena have increased a lot, because of the increasing frontiers of applications of chaos in engineering and non-engineering systems. “Chaos is a phenomenon which results from the exhibits sensitivity to perturbation in the structural parameters and initial conditions of some classes of dynamical systems” [<xref ref-type="bibr" rid="scirp.98569-ref1">1</xref>]. “Chaotic signals have a random-like nature and broadband spectrum and are non-periodic” [<xref ref-type="bibr" rid="scirp.98569-ref2">2</xref>]. “For a system to be chaotic, the following conditions must be satisfied. Firstly, it must be sensitive to perturbation in its initial conditions which should lead to unpredictability of its future trajectories, secondly, it is not topologically transitive and thirdly, the chaotic orbits are dense in the phase space” [<xref ref-type="bibr" rid="scirp.98569-ref3">3</xref>]. “Among some evolved chaotic attractors in the literature are the Chen’s” [<xref ref-type="bibr" rid="scirp.98569-ref4">4</xref>], “3-D, 4-wing attractor” [<xref ref-type="bibr" rid="scirp.98569-ref5">5</xref>], “Sundarapandian-Pehlivan” [<xref ref-type="bibr" rid="scirp.98569-ref6">6</xref>], “Morphous one parameter attractor” [<xref ref-type="bibr" rid="scirp.98569-ref7">7</xref>], “Rabinovich system” [<xref ref-type="bibr" rid="scirp.98569-ref8">8</xref>]. “When chaotic attractors possess one positive Lapiynov exponent, then the system is chaotic. However, the system which has two or more positive Lapiynov exponents it is a highly chaotic system and becomes hypersensitive to small perturbations in its system dynamics” [<xref ref-type="bibr" rid="scirp.98569-ref9">9</xref>] [<xref ref-type="bibr" rid="scirp.98569-ref10">10</xref>]. “Chaos Control subject has received widespread attention of research because controllability and synchronizability of chaotic attractors are index of utility in different designs such as in secure communications and robotics” [<xref ref-type="bibr" rid="scirp.98569-ref11">11</xref>] [<xref ref-type="bibr" rid="scirp.98569-ref12">12</xref>] [<xref ref-type="bibr" rid="scirp.98569-ref13">13</xref>].</p><p>“In the context of stability and stabilization, the principle of Lapiynov stability continued to enjoy large applications; it can effectively stabilize the dissipative systems” [<xref ref-type="bibr" rid="scirp.98569-ref14">14</xref>] [<xref ref-type="bibr" rid="scirp.98569-ref15">15</xref>].</p><p>This paper is organized as: Section 2, present a description of 3-d system. Section 3, basic analysis such as stability, dissipativity, Lapiynov dimension ‘‘Kaplan-Yοrke dimension’’. Section 4, we designed adaptive control law of the chaotic system. Section 5, a comparison of the analysis results before and after control. Section 6, we derive results for the adaptive synchronization of identical highly chaotic system. Finally Section 7, summarization of the main results.</p></sec><sec id="s2"><title>2. System Description</title><p>A three-dimensional dynamical system [<xref ref-type="bibr" rid="scirp.98569-ref16">16</xref>] consist of three ordinary differential equations with state variables x i , (i = 1, 2, 3) and four unknown parameters (ρ, α, δ and φ), employs six terms include two quadratic cross-product nonlinear terms. Given by:</p><p>x ˙ 1 = ρ ( x 2 − x 1 ) x ˙ 2 = a x 1 − δ x 1 x 3 x ˙ 3 = φ x 1 x 2 − x 3 (1)</p><p>The parameters values are taken as</p><p>ρ = 10 , δ = 40 , a = 296.5 , φ = 10 (2)</p></sec><sec id="s3"><title>3. System Analysis</title><p>In this section essential, the system (1) is invested and has the following characteristics.</p><sec id="s3_1"><title>3.1. Equilibrium Points</title><p>The first step to analyze a system is to find its equilibrium points, so we need to solve the nonlinear equations as follows</p><p>− 10 x 1 + 10 x 2 = 0</p><p>296.5 x 1 − 40 x 1 x 3 = 0</p><p>10 x 1 x 2 − x 3 = 0</p><p>We get the following equilibrium points:</p><p>E 0 = ( 0 , 0 , 0 ) , E 1 = ( 593 2 20 , 593 2 20 , 593 80 ) , E 2 = ( − 593 2 20 , − 593 2 20 , 593 80 )</p></sec><sec id="s3_2"><title>3.2. Stability Analysis</title><sec id="s3_2_1"><title>3.2.1. Characteristic Equation Roots</title><p>“A necessary and sufficient condition for the system to be stable is that the real parts of the characteristic equation have negative real parts”.</p><p>When the parameters values are taken as in (2), the Jacobian matrix of system (1) at E 0 = ( 0 , 0 , 0 ) is:</p><p>J = [ − 10 10 0 296.5 0 0 0 0 − 1 ]</p><p>det ( J − λ I ) = 0</p><p>⇒ λ 3 + 11 λ 2 − 2955 λ − 2965 = 0 (3)</p><p>By using Horner’s Ruffini method [<xref ref-type="bibr" rid="scirp.98569-ref17">17</xref>] we get:</p><p>λ 1 = − 1 , λ 2 = 49.68089 , λ 3 = − 59.68089</p><p>Similarly, we find Jacobian matrix at E 1 and E 2 , then we obtain the eigenvalues, as shown in <xref ref-type="table" rid="table1">Table 1</xref>.</p><p>So the system (1) is unstable.</p></sec><sec id="s3_2_2"><title>3.2.2. Routh Stability Criteria</title><p>“The system is considered stable by the Routh stability states (all poles in OLHP (Open Loop Half plane)) if and only if all elements of the first column in the Routh array are positive. In addition, number of poles not in the OLHP is equal to the number of sign changes in the first column” [<xref ref-type="bibr" rid="scirp.98569-ref18">18</xref>].</p><p>a 0 = − 2965</p><p>a 1 = − 2955</p><p>a 2 = 11</p><p>a 3 = 1</p><p>b 1 = a 1 − a 3 a 0 a 2 = − 2685.4545</p><p>Since, there are two negative elements in the first column. Therefore, the system (1) is unstable.</p></sec><sec id="s3_2_3"><title>3.2.3. Hurwitz Stability Criteria</title><p>“This criterion is applied using determinants formed from coefficients of the characteristic equation. If the small minors of the square matrix J of the system (1) are all positive then the system (1) is stable, otherwise it’s unstable” [<xref ref-type="bibr" rid="scirp.98569-ref18">18</xref>].</p><p>If n = 3 (n denote the degree of the square matrix)</p><p>From Equation (3) we find:</p><p>Δ 1 = a 2 = 11 &gt; 0</p><p>Δ 2 = | a 2 a 0 a 3 a 1 | = a 2 a 1 − a 3 a 0 = − 29.540 &lt; 0</p><p>Δ 3 = | a 2 a 0 0 a 3 a 1 0 0 a 2 a 0 | = a 2 a 1 a 0 − a 0 2 a 3 = 87586100 &gt; 0</p><p>Since the values of one minors is less than zero, so the system (1) is unstable.</p></sec><sec id="s3_2_4"><title>3.2.4. Lapiynov Function</title><p>We can use quadratic function for system (1).</p><p>We assume that</p><p>V ( x 1 , x 2 , x 3 ) = 1 2 ( x 1 2 + x 2 2 + x 3 2 )</p><p>V ˙ ( x 1 , x 2 , x 3 ) = x 1 x ˙ 1 + x 2 x ˙ 2 + x 3 x ˙ 3 (4)</p><p>If V ˙ ( x 1 , x 2 , x 3 ) &lt; 0 then the system is stable.</p><p>By substituting (1) in Equation (4) we get:</p><p>V ˙ ( x 1 , x 2 , x 3 ) = − 10 x 1 2 + 306.5 x 1 x 2 − 30 x 1 x 2 x 3 − x 3 2</p><p>Since V ˙ ( x 1 , x 2 , x 3 ) &gt; 0 therefore the system (1) is unstable.</p></sec></sec><sec id="s3_3"><title>3.3. Dissipativity</title><p>Let f 1 = d x 1 d t , f 2 = d x 2 d t and f 3 = d x 3 d t in the system (1).</p><p>Then we get for the vector field</p><p>( x ˙ 1 , x ˙ 2 , x ˙ 3 ) T = ( f 1 , f 2 , f 3 ) T</p><p>thus the divergence of the vector field V on R 3 yields to:</p><p>∇ ⋅ ( x ˙ 1 , x ˙ 2 , x ˙ 3 ) T = ∂ f 1 ∂ x 1 + ∂ f 2 ∂ x 2 + ∂ f 3 ∂ x 3 = − ( ρ + 1 ) = f</p><p>Note that f = − ( ρ + 1 ) = − 11 , so the systеm (1) is dissipative for all positive values of ρ , and an exponential rate is:</p><p>d V d t = f V ⇒ V ( t ) = V 0 e f t = V 0 e − 11 t</p><p>From above equation, the volume element V 0 is contracted by the flow into a volume element V 0 e − 11 t at the time t.</p></sec><sec id="s3_4"><title>3.4. Numerical and Graphical Results</title><p>For the numerical solution, we use Runge-Kutta method of order 5<sup>th</sup> to solve system (1). With initial states x | x 1 ( 0 ) , x 2 ( 0 ) , x 3 ( 0 ) = [ − 2 , 7 , 12 ]</p><sec id="s3_4_1"><title>3.4.1. Wave Form of the System (1)</title><p>The wave-form x 1 ( t ) , x 2 ( t ) , x 3 ( t ) for the system (1) is characteristic with non-periodic shape, shown in Figures 1(a)-(c) which is one of the basic characteristic behaviors of chaotic dynamical system.</p></sec><sec id="s3_4_2"><title>3.4.2. Phase Portrait of the System (1)</title><p>Figures 2(a)-(d) and Figures 3(a)-(c) are shows chaotic attractor for system (1) in ( x 1 , x 2 , x 3 ) , ( x 1 , x 3 , x 2 ) , ( x 2 , x 1 , x 3 ) , ( x 3 , x 1 , x 2 ) space, and 2-D attractor of system (1) in ( x 1 , x 3 ) , ( x 1 , x 2 ) , ( x 2 , x 3 ) plane.</p><p>The orbit is dense in each graph which means the system exhibit two-scroll hyper chaotic attractor.</p></sec></sec><sec id="s3_5"><title>3.5. Lapiynov Exponent and Lapiynov Dimension</title><p>“As a rule the Lapiynov exponents refer to the average exponential rates of divergence or convergence of nearby trajectories in the phase space. The system is chaotic if there is at least one Lapiynov exponent greater than zero”. The values of lapiynov exponents are: ( L 1 = 2.509426 , L 2 = 0.132019 and L 3 = − 11.818787 ). Therefore, the Lapiynov dimension ‘‘Kaplan-Yοrke dimension’’ is:</p><p>D L = 2 + L 1 + L 2 | L 3 | = 2.22349544</p><p>So the system (1) is Highly Chaotic System, as shown in <xref ref-type="fig" rid="fig4">Figure 4</xref>.</p></sec></sec><sec id="s4"><title>4. Adaptive Control Strategy</title><sec id="s4_1"><title>4.1. Theoretical Results</title><p>To stabilize highly chaotic system (1), an adaptive control law is designed with unknown parameter α.</p><p>As follows:</p><p>x ˙ 1 = 10 ( x 2 − x 1 ) + α 1 x ˙ 2 = a x 1 − 40 x 1 x 3 + α 2 x ˙ 3 = 10 x 1 x 2 − x 3 + α 3 (5)</p><p>when α 1 , α 2 , α 3 are the feedback controllers.</p><p>The adaptive control functions are:</p><p>α 1 = − 10 ( x 2 − x 1 ) − μ 1 x 1 α 2 = − a ^ x 1 + 40 x 1 x 3 − μ 2 x 2 α 3 = − 10 x 1 x 2 + x 3 − μ 3 x 3 (6)</p><p>where the constants μ i , (i = 1, 2,3) are positive , a ^ is the parameter estimate of α.</p><p>Substituting (6) into (5), we get</p><p>x ˙ 1 = − μ 1 x 1 x ˙ 2 = ( a − a ^ ) x 1 − μ 2 x 2 x ˙ 3 = − μ 3 x 3 (7)</p><p>Let the parameter estimation error</p><p>e a = a − a ^ (8)</p><p>Using (8), the dynamics (7) can be written compactly as</p><p>x ˙ 1 = − μ 1 x 1 x ˙ 2 = e a x 1 − μ 2 x 2 x ˙ 3 = − μ 3 x 3 (9)</p><p>The Lapiynov approach is used for derivation of update law for adjusting the parameter estimate a ^ .</p><p>Consider the lapiynov function</p><p>V ( x 1 , x 2 , x 3 ) = 1 2 ( x 1 2 + x 2 2 + x 3 2 + e a 2 ) (10)</p><p>Notice V is positive-definite on R 4 .</p><p>Also</p><p>e ˙ a = − a ^ ˙ (11)</p><p>Differentiating V with substituting (9) and (11), we get:</p><p>V ˙ = − μ 1 x 1 2 − μ 2 x 2 2 − μ 3 x 3 2 + e a [ x 1 x 2 − a ^ ˙ ] (12)</p><p>In Equation (12), we update estimated parameter by:</p><p>a ^ ˙ = x 1 x 2 + μ 4 e a (13)</p><p>where the constant μ 4 is a positive.</p><p>Now, we substitute (13) into (12), we obtain</p><p>V ˙ = − μ 1 x 1 2 − μ 2 x 2 2 − μ 3 x 3 2 − μ 4 e a 2 (14)</p><p>Notice V ˙ is negative definite on R 4 .</p><p>Thus, by lapiynov stability, Routh-array criteria, Eigenvalues and Hurwitz stability criteria we get the below result.</p><p>Proposition 1. The chaotic system (5) with unknown parameter is stabilized for every initial value by adaptive control (6), where the estimated parameter is obtained by (13) and μ 1 , μ 2 , μ 3 , μ 4 are greater than zero.</p></sec><sec id="s4_2"><title>4.2. Numerical Results</title><p>To simulate the controlled highly chaotic system (7) we take the initial values x | x 1 ( 0 ) , x 2 ( 0 ) , x 3 ( 0 ) = [ 12 , 9 , 17 ] and [ μ 1 , μ 2 , μ 3 ] = [ 30 , 50 , 30 ] .</p><p><xref ref-type="fig" rid="fig5">Figure 5</xref> shows Controlled trajectories of system (1).</p></sec></sec><sec id="s5"><title>5. System Comparison Tables before &amp; after Control</title><p>See Tables 1-6.</p><table-wrap id="table1" ><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Eigenvalues of the system (1) before and after control</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Equilibrium point</th><th align="center" valign="middle" >Before control</th><th align="center" valign="middle" >After control</th></tr></thead><tr><td align="center" valign="middle" >( 0 , 0 , 0 )</td><td align="center" valign="middle" >λ 1 = − 1 λ 2 = 49.68089 λ 3 = − 59.68089</td><td align="center" valign="middle" >λ 1 = − 30 λ 2 = − 50 λ 3 = − 30</td></tr><tr><td align="center" valign="middle" >( 593 2 20 , 593 2 20 , 593 80 )</td><td align="center" valign="middle" >λ 1 = 1.39097 λ 2 = 42.622 λ 3 = − 55.013</td><td align="center" valign="middle" >λ 1 = − 30 λ 2 = − 50 λ 3 = − 30</td></tr><tr><td align="center" valign="middle" >( − 593 2 20 , − 593 2 20 , 593 80 )</td><td align="center" valign="middle" >λ 1 = 1.39097 λ 2 = 42.622 λ 3 = − 55.013</td><td align="center" valign="middle" >λ 1 = − 30 λ 2 = − 50 λ 3 = − 30</td></tr></tbody></table></table-wrap><table-wrap id="table2" ><label><xref ref-type="table" rid="table2">Table 2</xref></label><caption><title> Hurwitz criteria of the system (1) before and after control</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Equilibrium point</th><th align="center" valign="middle" >Before control</th><th align="center" valign="middle" >After control</th></tr></thead><tr><td align="center" valign="middle" >( 0 , 0 , 0 )</td><td align="center" valign="middle" >Δ 1 = 11 Δ 2 = − 29.540 Δ 3 = 87586100</td><td align="center" valign="middle" >Δ 1 = 110 Δ 2 = 384000 Δ 3 = 1728 &#215; 10 10</td></tr><tr><td align="center" valign="middle" >( 593 2 20 , 593 2 20 , 593 80 )</td><td align="center" valign="middle" >Δ 1 = 11 Δ 2 = − 29243.5 Δ 3 = − 95377675.25</td><td align="center" valign="middle" >Δ 1 = 110 Δ 2 = 384000 Δ 3 = 1728 &#215; 10 10</td></tr><tr><td align="center" valign="middle" >( − 593 2 20 , − 593 2 20 , 593 80 )</td><td align="center" valign="middle" >Δ 1 = 11 Δ 2 = − 29243.5 Δ 3 = − 95377675.25</td><td align="center" valign="middle" >Δ 1 = 110 Δ 2 = 384000 Δ 3 = 1728 &#215; 10 10</td></tr></tbody></table></table-wrap><table-wrap id="table3" ><label><xref ref-type="table" rid="table3">Table 3</xref></label><caption><title> Routh array criteria of the system (1) before and after control</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Equilibrium point</th><th align="center" valign="middle" >λ</th><th align="center" valign="middle"  colspan="2"  >Before Control</th><th align="center" valign="middle"  colspan="2"  >After Control</th></tr></thead><tr><td align="center" valign="middle"  rowspan="4"  >( 0 , 0 , 0 )</td><td align="center" valign="middle" >λ 3</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >−2955</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >3900</td></tr><tr><td align="center" valign="middle" >λ 2</td><td align="center" valign="middle" >11</td><td align="center" valign="middle" >−2965</td><td align="center" valign="middle" >110</td><td align="center" valign="middle" >45,000</td></tr><tr><td align="center" valign="middle" >λ 1</td><td align="center" valign="middle" >−2685.5</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >3490.9</td><td align="center" valign="middle" >0</td></tr><tr><td align="center" valign="middle" >λ 0</td><td align="center" valign="middle" >−2965</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >45,000</td><td align="center" valign="middle" >0</td></tr><tr><td align="center" valign="middle"  rowspan="4"  >( 593 2 20 , 593 2 20 , 593 80 )</td><td align="center" valign="middle" >λ 3</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >−2362</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >3900</td></tr><tr><td align="center" valign="middle" >λ 2</td><td align="center" valign="middle" >11</td><td align="center" valign="middle" >3261.5</td><td align="center" valign="middle" >110</td><td align="center" valign="middle" >45,000</td></tr><tr><td align="center" valign="middle" >λ 1</td><td align="center" valign="middle" >−5634.5</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >3490.9</td><td align="center" valign="middle" >0</td></tr><tr><td align="center" valign="middle" >λ 0</td><td align="center" valign="middle" >3261.5</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >45,000</td><td align="center" valign="middle" >0</td></tr><tr><td align="center" valign="middle"  rowspan="4"  >( − 593 2 20 , − 593 2 20 , 593 80 )</td><td align="center" valign="middle" >λ 3</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >−2362</td><td align="center" valign="middle" >1</td><td align="center" valign="middle" >3900</td></tr><tr><td align="center" valign="middle" >λ 2</td><td align="center" valign="middle" >11</td><td align="center" valign="middle" >3261.5</td><td align="center" valign="middle" >110</td><td align="center" valign="middle" >45,000</td></tr><tr><td align="center" valign="middle" >λ 1</td><td align="center" valign="middle" >−5634.5</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >3490.9</td><td align="center" valign="middle" >0</td></tr><tr><td align="center" valign="middle" >λ 0</td><td align="center" valign="middle" >3261.5</td><td align="center" valign="middle" >0</td><td align="center" valign="middle" >45,000</td><td align="center" valign="middle" >0</td></tr></tbody></table></table-wrap><table-wrap id="table4" ><label><xref ref-type="table" rid="table4">Table 4</xref></label><caption><title> Lapiynov function of system (1) before and after control</title></caption><table><tbody><thead><tr><th align="center" valign="middle"  rowspan="2"  ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x145.png" xlink:type="simple"/></inline-formula></th><th align="center" valign="middle"  colspan="2"  ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x146.png" xlink:type="simple"/></inline-formula></th></tr></thead><tr><td align="center" valign="middle" >Before control</td><td align="center" valign="middle" >After control</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x147.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >44.79278685</td><td align="center" valign="middle" >−1486.699813</td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x148.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" >565</td><td align="center" valign="middle" >−6925</td></tr></tbody></table></table-wrap><table-wrap id="table5" ><label><xref ref-type="table" rid="table5">Table 5</xref></label><caption><title> Lapiynov exponent of system (1) before and after control</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >Before control</th><th align="center" valign="middle" >After control</th></tr></thead><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x149.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x150.png" xlink:type="simple"/></inline-formula></td></tr></tbody></table></table-wrap><table-wrap id="table6" ><label><xref ref-type="table" rid="table6">Table 6</xref></label><caption><title> Of phase portrait of the system (1) before and after control</title></caption><table><tbody><thead><tr><th align="center" valign="middle" >After control</th><th align="center" valign="middle" >Before control</th></tr></thead><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x151.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x152.png" xlink:type="simple"/></inline-formula></td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x153.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x154.png" xlink:type="simple"/></inline-formula></td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x155.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x156.png" xlink:type="simple"/></inline-formula></td></tr><tr><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x157.png" xlink:type="simple"/></inline-formula></td><td align="center" valign="middle" ><inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x158.png" xlink:type="simple"/></inline-formula></td></tr></tbody></table></table-wrap></sec><sec id="s6"><title>6. Adaptive Synchronization Technique</title><sec id="s6_1"><title>6.1. Theoretical Results</title><p>We apply adaptive synchronization technique of highly chaotic system with unknown parameter α.</p><p>The drive system is</p><disp-formula id="scirp.98569-formula1"><label>(15)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x159.png"  xlink:type="simple"/></disp-formula><p>where<inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x160.png" xlink:type="simple"/></inline-formula>, (i = 1, 2, 3) are state variables.</p><p>As the response system, the controlled highly chaotic dynamics given by</p><disp-formula id="scirp.98569-formula2"><label>(16)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x161.png"  xlink:type="simple"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x162.png" xlink:type="simple"/></inline-formula> are nonlinear controllers to be designed, and the state variables are<inline-formula><inline-graphic xlink:href="/html.scirp.org/file/98569x163.png" xlink:type="simple"/></inline-formula>, (i = 1, 2, 3).</p><p>The synchronization error is defined by</p><disp-formula id="scirp.98569-formula3"><label>(17)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x164.png"  xlink:type="simple"/></disp-formula><p>then the error dynamics is obtained as</p><disp-formula id="scirp.98569-formula4"><label>(18)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x165.png"  xlink:type="simple"/></disp-formula><p>The adaptive control functіοns <inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x166.png" xlink:type="simple"/></inline-formula> define as</p><disp-formula id="scirp.98569-formula5"><label>(19)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x167.png"  xlink:type="simple"/></disp-formula><p>where the constants <inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x168.png" xlink:type="simple"/></inline-formula> greater than zero, and <inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x168.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x169.png" xlink:type="simple"/></inline-formula> is the estimated value of the parameter α.</p><p>Substitute (19) into (18), to obtain the error dynamics as</p><disp-formula id="scirp.98569-formula6"><label>(20)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x170.png"  xlink:type="simple"/></disp-formula><p>Now, the parameter estimation error is</p><disp-formula id="scirp.98569-formula7"><label>(21)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x171.png"  xlink:type="simple"/></disp-formula><p>By substituting (21) into (20), the error dynamics simplifies to</p><disp-formula id="scirp.98569-formula8"><label>(22)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x172.png"  xlink:type="simple"/></disp-formula><p>From Lapiynov approach we derive the updated law to adjust the estimation of the parameter.</p><p>The quadratic lapiynov function is</p><disp-formula id="scirp.98569-formula9"><label>(23)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x173.png"  xlink:type="simple"/></disp-formula><p>which be a positive definite on<inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x174.png" xlink:type="simple"/></inline-formula>.</p><p>Note that</p><disp-formula id="scirp.98569-formula10"><label>(24)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x175.png"  xlink:type="simple"/></disp-formula><p>Differentiating V and substituting (22) &amp; (24) in it, we get:</p><disp-formula id="scirp.98569-formula11"><label>(25)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x176.png"  xlink:type="simple"/></disp-formula><p>update the estimated parameter in Equation (25) by the following</p><disp-formula id="scirp.98569-formula12"><label>(26)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x177.png"  xlink:type="simple"/></disp-formula><p>where the constant <inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x178.png" xlink:type="simple"/></inline-formula> is greater than zero.</p><p>From (25) and (26), we obtain:</p><disp-formula id="scirp.98569-formula13"><label>(27)</label><graphic position="anchor" xlink:href="//html.scirp.org/file/98569x179.png"  xlink:type="simple"/></disp-formula><p>We note that (27) is negative definite on<inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x180.png" xlink:type="simple"/></inline-formula>.</p><p>Hence, by Lapiynov stability [<xref ref-type="bibr" rid="scirp.98569-ref14">14</xref>], “it is immediate that the parameter error and synchronization error decay exponentially to zero with time for all initial values”.</p><p>Thus, we proved the results below.</p><p>Proposition 2. The drive and response identical chaotic systems (15) and (16) with unknown parameter α are synchronized for all initial values by adaptive control law (19), where the estimated parameter given by (26) and <inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x181.png" xlink:type="simple"/></inline-formula> are constants greater than zero.</p></sec><sec id="s6_2"><title>6.2. Numerical Results</title><p>To get the results numerically, we used the 4th-order Runge-Kutta method to solve systems (15) &amp; (16), and solve system (18) with adaptive control law (19).</p><p>We take <inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x182.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x182.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x183.png" xlink:type="simple"/></inline-formula> as initial states of the drive system (15) and the response system (16) respectively. Also take α = 296.5 and <inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x182.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x183.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x184.png" xlink:type="simple"/></inline-formula> for i = 1, 2, 3, 4.</p><p><xref ref-type="fig" rid="fig6">Figure 6</xref> shows adaptive synchronization of the highly chaotic system.</p><p><xref ref-type="fig" rid="fig7">Figure 7</xref> shows the convergent for system (18) with controller (19).</p></sec></sec><sec id="s7"><title>7. Conclusion</title><p>A three-dimensional dynamical system is dealt in this paper, it has quadratic cross-product nonlinear terms. The basic characteristics are analyzed by equilibrium points, stability analysis (such as characteristic equation roots, Routh criterion, Hurwitz criterion and Lapiynov function) all methods of stability shows that the system is unstable. Then, dissipativity analysis indicates system (1) is dissipative for positive values of the parameter<inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x185.png" xlink:type="simple"/></inline-formula>. Lapiynov exponent, lapiynov dimension and wave-form analysis present the hyper chaos behavior when the</p><p>parameters taken as<inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x188.png" xlink:type="simple"/></inline-formula>, and the maximum values of lyapenov exponents are:<inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x188.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x189.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x188.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x189.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x190.png" xlink:type="simple"/></inline-formula>and<inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x188.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x189.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x190.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x191.png" xlink:type="simple"/></inline-formula>, lapiynov dimension “Kaplan-Yοrkе dimension” of the system is<inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x188.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x189.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x190.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x191.png" xlink:type="simple"/></inline-formula><inline-formula><inline-graphic xlink:href="//html.scirp.org/file/98569x192.png" xlink:type="simple"/></inline-formula>, which means that the system is highly chaotic system. Moreover, to stabilize the highly chaotic system, we produced an adaptive control strategy. Finally, we proposed adaptive synchronization scheme for identical highly chaotic system with upadate law for the estimiation of system parameter. Synchronization schemes are established by Lapiynov stability. Furthermore, we compared theoretical and graphical results of the system before and after control.</p></sec><sec id="s8"><title>Conflicts of Interest</title><p>The authors declare no conflicts of interest regarding the publication of this paper.</p></sec><sec id="s9"><title>Cite this paper</title><p>Aziz, M.M. and Merie, D.M. (2020) Stability and Adaptive Control with Sychronization of 3-D Dynamical System. Open Access Library Journal, 7: e6075. https://doi.org/10.4236/oalib.1106075</p></sec></body><back><ref-list><title>References</title><ref id="scirp.98569-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">Cuomo, K.M., Oppenheim, A.V. and Strogatz, H.S. 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