<?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">IJMNTA</journal-id><journal-title-group><journal-title>International Journal of Modern Nonlinear Theory and Application</journal-title></journal-title-group><issn pub-type="epub">2167-9479</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/ijmnta.2014.33014</article-id><article-id pub-id-type="publisher-id">IJMNTA-48264</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><subject>PHYSICS &amp; MATHEMATICS</subject></subj-group></article-categories><title-group><article-title>Validity of Approach to Maximize the ASR of the Order Superiorly Two in Discrete Nonlinear Systems</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>Samia</surname><given-names>Charfeddine</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>Lassaad</surname><given-names>Sbita</given-names></name><xref ref-type="aff" rid="aff1"><sup>1</sup></xref></contrib></contrib-group><aff id="aff1"><addr-line>College of Engineering/Electrical Engineering, Unit of Photovoltaic, Wind and Geothermal Systems, ENIG, Gabés, Tunisia</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>samia.charfedine@yahoo.fr,(SC)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>14</day><month>07</month><year>2014</year></pub-date><volume>03</volume><issue>03</issue><fpage>124</fpage><lpage>135</lpage><history><date date-type="received"><day>24</day>	<month>May</month>	<year>2014</year></date><date date-type="rev-recd"><day>25</day>	<month>June</month>	<year>2014</year>	</date><date date-type="accepted"><day>3</day>	<month>July</month>	<year>2014</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>
	This paper is, in fact, a proposal of a polynomial approach to the
nonlinear systems control by using the concept of linearization by state
feedback. In this context, a discretization method is presented. We developed a
discrete control scheme based on an approximate feedback linearization method
and the reversing trajectory method. The proposed control strategy sits on the
methods of widening the stability domains of operating points. Such domains are
expanded through the use of the non Lyapunov stability synthesis methods.
Additionally, the developed technique is employed for the control of the class
of systems with an order higher than two; more precisely, the example of a
synchronous generator featured in a strongly nonlinear model. 


	  
</p></abstract><kwd-group><kwd>Discrete-Time Systems</kwd><kwd> Reverse Trajectory Method</kwd><kwd> Nonlinear Polynomial Systems</kwd><kwd> Asymptotic Stability Region (ASR)</kwd><kwd> Synchronous Generateur</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>It is widely believed that in the field of automation, several constraints of physical nature have an effect on the dynamic behavior of non-linear systems. Consequently, the study of a system-dynamics comprises a preliminary and important phase so that we can find out about the strategy of a powerful and reliable order. Obviously, the study and analysis of the stability of dynamic systems involves an essential stage for any resourceful study. Thus, the concept of asymptotic stability of autonomous continuous systems is elaborated today. In 19th century, this notion came into existence with the theory of Lyapunov in an attempt to create an interest-center to a huge number of research-works and research-works; in this, the theory of Zubov [<xref ref-type="bibr" rid="scirp.48264-ref1">1</xref>] -[<xref ref-type="bibr" rid="scirp.48264-ref3">3</xref>] is a case in point. Such a theory, in fact, provides a common scope for study of all the nonlinear autonomous continuous systems. Hence, the two following issues are regarded as major problems:</p><p>• The analysis of the stability of nonlinear dynamic systems.</p><p>• The estimate of a relatively exact region of the state-space ensuring the stability of nonlinear-system va- riables.</p><p>When we are inclined to the study of stability in continuous time, we can perceive the richness of the litera- ture which is teeming with results, methods and approaches dealing with these themes [<xref ref-type="bibr" rid="scirp.48264-ref4">4</xref>] -[<xref ref-type="bibr" rid="scirp.48264-ref6">6</xref>] .</p><p>Nevertheless, when dealing with the problems of analysis and stability of the discrete autonomous nonlinear systems, we note that a few works address such problems [<xref ref-type="bibr" rid="scirp.48264-ref7">7</xref>] -[<xref ref-type="bibr" rid="scirp.48264-ref10">10</xref>] .</p><p>In this, this article is aimed to study the stability and to determine a field of stability of the discrete autonom- ous nonlinear dynamic systems.</p><p>We also realize that most of the studies dealing with this subject are based on the Lyapunov theory. We insist on the fact that, for a nonlinear system, the determination of an asymptotic stability region around an equili- brium point is generally a hard task. Again, we are appealed to the synthesis of a numerical technique so as to analyze the asymptotic stability in the neighborhood of the discrete systems stable equilibrium points.</p><p>This approach is developed in other works [<xref ref-type="bibr" rid="scirp.48264-ref11">11</xref>] -[<xref ref-type="bibr" rid="scirp.48264-ref13">13</xref>] . Its principle aims at executing in the opposite directions of the iterations described by the recurring polynomial state equation. Such equation represents the dynamics of the studied autonomous discrete nonlinear systems. The reverse discrete system, then, will be characterized by the same samples belonging to the closed curves in the state space and which represent the same dynamics of the initial system. But its discrete direction of evolution is quite the reverse. Consequently, the origin becomes un- stable and the speed of the closed curves connecting the discrete points initialized in an asymptotic stability field is reduced. This, in fact, allows identifying a broader stability region.</p><p>Indeed, the reverse trajectory method paves us the way to reach the exact field of asymptotic stability of the nonlinear discrete systems of order 2. Nevertheless, it is applied to the systems of an order equal to or higher than 3 in orders to widen the initial field of stability without reaching the exact field of stability.</p><p>This paper is organized as follows: in the first section.</p></sec><sec id="s2"><title>2. The Discretization Method</title><p>The method of studying a discrete process looks like a transposition of the methods which are initially devel- oped for the continuous systems. This actually pushes us to study the analogy between the continuous and dis- crete process which paves us the way to use the numerical and analogue methods by control and simulation.</p><p>In this part, we are inclined to the determination of a discrete model of the continuous systems.</p><p>Initially, we consider the continuous model defined by the following equation:</p><disp-formula id="scirp.48264-formula2587"><label>(1)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\7bdd03f1-6db1-4633-bcba-d42e96350f6d.png"/></disp-formula><p>We employ the continuous model of order three which is defined by:</p><disp-formula id="scirp.48264-formula2588"><label>(2)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\d9ea51ee-05c6-47e0-a3f8-e062f62d9b45.png"/></disp-formula><p>By considering a discretization period T, which is properly selected and by adopting the following approxima-</p><p>tions in an interval<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\79586e0a-06c9-41b3-b3d0-7120d5e5ef79.png" xlink:type="simple"/></inline-formula>:</p><p>Let us consider, then, the following discretization method [<xref ref-type="bibr" rid="scirp.48264-ref14">14</xref>] [<xref ref-type="bibr" rid="scirp.48264-ref15">15</xref>] :</p><disp-formula id="scirp.48264-formula2589"><label>(3)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\3986095a-2121-43e5-88b3-b29344d68468.png"/></disp-formula><p>By including Equation (3) in Equation (2), here comes the discrete model given by:</p><disp-formula id="scirp.48264-formula2590"><label>(4)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\1f70dd75-4791-4fcf-bce0-939386cd77e1.png"/></disp-formula><p>where</p><disp-formula id="scirp.48264-formula2591"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\928c5273-9a0b-4f10-a198-2708290b51bd.png"/></disp-formula></sec><sec id="s3"><title>3. Linearizing Polynomial Control of the Discrete Nonlinear Systems</title><sec id="s3_1"><title>3.1. Description of the Studied Discrete Nonlinear Systems</title><p>The concept of the discrete NLGS approach is derived from the same methodology as the continuous NLGS one. In addition, we discredited the continuous model so as to simplify the analysis and to facilitate the task of asso- ciated calculation [<xref ref-type="bibr" rid="scirp.48264-ref16">16</xref>] . The discretization of continuous systems is particularly significant today as the current technology requires the implementation of discrete controls [<xref ref-type="bibr" rid="scirp.48264-ref17">17</xref>] .</p><p>The studied discrete nonlinear systems are defined by the state equations of the form [<xref ref-type="bibr" rid="scirp.48264-ref18">18</xref>] [<xref ref-type="bibr" rid="scirp.48264-ref19">19</xref>] :</p><disp-formula id="scirp.48264-formula2592"><label>(5)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\bbb2774d-0ced-4c97-b5b6-3025cd171acf.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\c7bc7253-d960-4081-8bc9-e6f943a885fe.png" xlink:type="simple"/></inline-formula> is the state vector<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\4ee108d5-3e69-4d52-b91d-4914693e7be6.png" xlink:type="simple"/></inline-formula>, <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\ea24327f-d453-4efc-af9e-890a50e34d8c.png" xlink:type="simple"/></inline-formula>is the control vector<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\19269486-2417-498b-b3bc-13e4c3e0efaa.png" xlink:type="simple"/></inline-formula>, the functions <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\adab366a-50f1-4c72-84be-9bdb128785dd.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\19ad5c6b-738a-451b-8542-5c8708269c89.png" xlink:type="simple"/></inline-formula> are assumed to be analytical.</p><p>Let us consider the following variable change<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\b9f8c792-8a5a-4354-8003-e086dbb2428b.png" xlink:type="simple"/></inline-formula>, where the operating point state vector is <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\bdc0657c-954f-4146-b06e-c6e5ff8e13bd.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\86dedb8d-862b-4bba-b2b6-9a702b0f1adc.png" xlink:type="simple"/></inline-formula> is the corresponding control input. Using the development into generalized Taylor series expansions and the kronecker tensorial product given by:</p><disp-formula id="scirp.48264-formula2593"><label>(6)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\f35fbf29-51fa-48c9-bbd7-54612302a9aa.png"/></disp-formula></sec><sec id="s3_2"><title>3.2. The Suggested Approach to the Control</title><sec id="s3_2_1"><title>3.2.1. Formulation of the Problem of Linearizing Control</title><p>Let us consider the discrete nonlinear system (1) and consider an arbitrary linear system of order n described by the following state equation [<xref ref-type="bibr" rid="scirp.48264-ref7">7</xref>] -[<xref ref-type="bibr" rid="scirp.48264-ref20">20</xref>] :</p><disp-formula id="scirp.48264-formula2594"><label>(7)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\c209314d-663f-44c7-9cb3-3092a3e74d8b.png"/></disp-formula><p>It is a question of determining, when there exists, a nonlinear feedback of the form:</p><disp-formula id="scirp.48264-formula2595"><label>(8)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\e3385c4f-27a6-4137-9f47-84a56ecf06f1.png"/></disp-formula><p>Here is a nonlinear analytical transformation described by the following equation:</p><disp-formula id="scirp.48264-formula2596"><label>(9)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\0deb5f03-6821-4d3c-9a82-03878f4af84c.png"/></disp-formula><p>Such that (5) is transformed into the linear system (7).</p></sec><sec id="s3_2_2"><title>3.2.2. The Control Determination</title><p>By using the polynomial development of the functions <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\e6caa66e-beb2-4b2b-a4b5-0f61ed832ed6.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\4483d6c5-404e-4824-809f-8410708a4db5.png" xlink:type="simple"/></inline-formula>, the relations (8) and (9) are written as:</p><disp-formula id="scirp.48264-formula2597"><label>(10)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\a64eb23e-bfc9-4fdd-af93-8e77f890e177.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\6f5224a3-936e-4df7-ba56-573bda29f8a5.png" xlink:type="simple"/></inline-formula>is the redundant power.</p><p>The control vector <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\d0350282-0c96-4b41-ac40-1eb2d2defbba.png" xlink:type="simple"/></inline-formula> and the state analytic transformation are defined by the matrices <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\12764fe9-28c9-4644-a859-8352786d67ee.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\aaea6890-4012-40af-9f93-e519892bc19d.png" xlink:type="simple"/></inline-formula>.</p><p>By replacing the functions <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\2c72566b-4b67-4d3e-8e95-6e5d6277c28b.png" xlink:type="simple"/></inline-formula> and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\cbeb5b39-fe43-49e9-9870-ccee7e7b106e.png" xlink:type="simple"/></inline-formula> with the developments (6) in the state Equation (5), we can get:</p><disp-formula id="scirp.48264-formula2598"><label>(11)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\0142700f-ed33-4fc5-867e-ea82b51b110a.png"/></disp-formula><p>After replacing the control vector <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\7c48e5f6-0ad3-49be-bc50-b5af9c52a56b.png" xlink:type="simple"/></inline-formula> with the development (10), Equation (11) becomes:</p><disp-formula id="scirp.48264-formula2599"><label>(12)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\f579edd4-be7e-483e-920e-8457cee96649.png"/></disp-formula><p>Such equation can be stated in this form:</p><disp-formula id="scirp.48264-formula2600"><label>(13)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\c0c3a112-3a43-403b-b37d-0b82c68a59dd.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\b76a5ca3-cc21-4742-a005-434c0792110d.png" xlink:type="simple"/></inline-formula></p><p>The vector defined in Equation (9) verified:</p><disp-formula id="scirp.48264-formula2601"><label>(14)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\76d24873-5617-4427-b641-f5cb56f28dad.png"/></disp-formula><p>and for <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\417fe4f7-c5ad-4740-a38d-0a41427625bb.png" xlink:type="simple"/></inline-formula></p><disp-formula id="scirp.48264-formula2602"><label>(15)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\36fe6c80-5c13-4ef8-8e53-e26df2a2e510.png"/></disp-formula><p>where</p><disp-formula id="scirp.48264-formula2603"><label>(16)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\85f3c7c3-c764-4759-a393-d97db237145a.png"/></disp-formula><p>In particular, we have</p><disp-formula id="scirp.48264-formula2604"><label>(17)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\23468211-185a-48de-a4c6-357c2ab607ca.png"/></disp-formula><p>and</p><disp-formula id="scirp.48264-formula2605"><label>(18)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\ad905d74-2874-4486-80f6-84d12a9b7095.png"/></disp-formula><p>The expression (14) truncated to the r order:</p><p>Using the polynomial development functions <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\b60b0ef2-d01d-4bae-8fe2-fb5e1b9e9cde.png" xlink:type="simple"/></inline-formula> and<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\260dd539-7de1-4584-9dbe-a1d891b42148.png" xlink:type="simple"/></inline-formula>, the relations (7) and (10) are written as:</p><disp-formula id="scirp.48264-formula2606"><label>(19)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\a10fc479-ea62-4c26-b016-caf062430299.png"/></disp-formula><p>other</p><disp-formula id="scirp.48264-formula2607"><label>(20)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\04ee4c4b-95fe-43be-b9b8-81e3764363ce.png"/></disp-formula><p>By replacing <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\53420449-be49-462e-a095-46da9d0125ae.png" xlink:type="simple"/></inline-formula> which is defined by System (7) in Equation (10), we obtain the form:</p><disp-formula id="scirp.48264-formula2608"><label>(21)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\6715ffcc-691a-48c9-a7e2-84e40d93194a.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\e4eb2078-1060-4083-a02e-0e5a3da3b835.png" xlink:type="simple"/></inline-formula> is a redundant matrix.</p><p>The identification of the relations (20) and (21) leads to the following recurring equations:</p><disp-formula id="scirp.48264-formula2609"><label>(22)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\da79c4dc-07dc-48af-996e-3d3e6face274.png"/></disp-formula><p>The choice of the matrix <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\516e0abd-4f4a-4858-81cc-d6dcd0c798c5.png" xlink:type="simple"/></inline-formula> such as <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\76d52564-c608-4cef-9a7a-9477ae92d5df.png" xlink:type="simple"/></inline-formula> implies:</p><disp-formula id="scirp.48264-formula2610"><label>(23)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\39541837-e217-402b-8ecb-fa1a3076de0c.png"/></disp-formula><p>when the function <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\fcec5e9d-8f1b-474e-ba49-74ca61180b7b.png" xlink:type="simple"/></inline-formula> is introduced into the Sylvester Equation, it comes [<xref ref-type="bibr" rid="scirp.48264-ref21">21</xref>] :</p><disp-formula id="scirp.48264-formula2611"><label>(24)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\45260fea-ad34-4889-8b73-d204fea066e6.png"/></disp-formula><p>where</p><disp-formula id="scirp.48264-formula2612"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\65234104-fcd9-4fec-a4d7-5db329dfa8dd.png"/></disp-formula><p>A necessary condition of existence of the matrix <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\53d208a4-d917-4803-9e94-0d3033c2f45d.png" xlink:type="simple"/></inline-formula> and the matrix <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\45cc8841-bd52-4d5f-9fd0-c8ac856ad75a.png" xlink:type="simple"/></inline-formula> itself is a full row. When this condi- tion is satisfied, the relation (24) leads to what may be said as satisfied:</p><disp-formula id="scirp.48264-formula2613"><label>(25)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\929dad08-69de-49ef-8f56-2d2375b0c75a.png"/></disp-formula><p>where</p><p><inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\a2c2225b-b370-4cc0-b051-fae06c0ea5eb.png" xlink:type="simple"/></inline-formula>is the pseudo-inverse of<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\333820ae-f79b-4dd7-8b29-ed733ae7996c.png" xlink:type="simple"/></inline-formula>.</p><p>Equation (25) allows for the determination of the coefficients of the matrices<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\544b5812-562a-46dc-9683-3bd5618a2ab1.png" xlink:type="simple"/></inline-formula>. The parameters <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\6f76fa3f-4e07-4ae3-9fa9-824438496d68.png" xlink:type="simple"/></inline-formula> of</p><p>the control law are selected such that the standard <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\b7dab3b7-ec6c-4887-a8e2-b34fb6e332e0.png" xlink:type="simple"/></inline-formula> is minimal. This minimization leads</p><p>to the following expression of the matrices<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\a40ec85d-8e3e-4915-94ba-923f9c748722.png" xlink:type="simple"/></inline-formula>:</p><disp-formula id="scirp.48264-formula2614"><label>(26)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\6d7c8df0-252d-45bc-b493-66bd8f4e1eee.png"/></disp-formula></sec></sec></sec><sec id="s4"><title>4. The Principe of the Algebraic Inversion of the Recurring State Equation</title><p>This principle derives its effectiveness from the fact that the asymptotic speeds of the points belonging to the closed curves (when<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\783f2efd-624d-4283-b844-7bd6ac35b9a8.png" xlink:type="simple"/></inline-formula>) constitute an integral part of the border of the searched stability region. This technique is identical to that developed in the case of continuous systems.</p><p>This method is obviously based on the execution of the iterations by reversing the sampling moments de- scribed by the parameter k of the state Equation (13) and represent the autonomous nonlinear discrete polynomi- al system [<xref ref-type="bibr" rid="scirp.48264-ref22">22</xref>] -[<xref ref-type="bibr" rid="scirp.48264-ref25">25</xref>] . Likewise, we have to consider the system described by the following equation:</p><disp-formula id="scirp.48264-formula2615"><label>(27)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\40e54546-b077-4eed-95a5-d547cbecaee9.png"/></disp-formula><p>Such a system is called reverse, it is characterized by the same samples belonging to the closed curves of the state space and which describe the discrete dynamics of the system (13) but by reversing the direction of the states. The origin which is thought to be stable for the system (27), thus, becomes unstable for the system known as reverse (13).</p></sec><sec id="s5"><title>5. Algebraic Approach to the Inversion of the State Discrete Equation</title><p>This section is dedicated to the synthesis of the analytical methods which aim at approximating the recurring state equation of the studied discrete system through a state equation which describes its evolution in the oppo- site direction in the state space.</p><p>An algebraic approach will then be considered [<xref ref-type="bibr" rid="scirp.48264-ref26">26</xref>] . Such an approach considers an initial field of asymptotic stability around an equilibrium point to carry out, thereafter, converse iterations allowing us to widen the initial field of the considered stability.</p><p>Let us suppose then:</p><disp-formula id="scirp.48264-formula2616"><label>(28)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\3d130e43-688e-4936-b244-de0da2a11afe.png"/></disp-formula><p>This assumption is rigorously justified in the case where the evolution from iteration to another is done with an optimal choice of the sampling period.</p><p>According to the analytical development given in [<xref ref-type="bibr" rid="scirp.48264-ref22">22</xref>] , we assume in the remaining part of this paper that the classes of discrete systems under consideration are truncated to the third order which can be written as follows:</p><disp-formula id="scirp.48264-formula2617"><label>(29)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\d5ce1338-eabd-4880-88d1-283e5df79683.png"/></disp-formula><p>By replacing <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\557fd2f8-aa89-418c-a370-6a79a232a3fc.png" xlink:type="simple"/></inline-formula> by its expression (29) in (28) and by neglecting the terms<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\1444eac7-687d-44dd-affe-4282c18ff068.png" xlink:type="simple"/></inline-formula>, for<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\f14e3834-4ffb-4f0a-a38b-2694be4507ec.png" xlink:type="simple"/></inline-formula>, we can easily reach, after identification, the following equality:</p><disp-formula id="scirp.48264-formula2618"><label>(30)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\0b8b3882-0b9d-42b2-9227-362f41e73a10.png"/></disp-formula><p>where</p><disp-formula id="scirp.48264-formula2619"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\605d4364-38ab-4a24-b75e-98ab0cc30fbb.png"/></disp-formula><p>The expression (30) characterizes the term <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\c51a58a9-cd82-4213-a052-debdc9856598.png" xlink:type="simple"/></inline-formula> which describes a weak variation of the deviations de- scribing the dynamics of the models studied between two successive sampling moments. The representation of the discrete state (28) is regarded as an approximation of the dynamic behavior in the reverse direction of the studied systems discrete states. Such an approximation is, in fact, an assumption which will be as much satisfied as the variation <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\2f34ec9e-1571-42d9-9329-5eff939c04a2.png" xlink:type="simple"/></inline-formula> is reduced. This imposes the choice of a weak sampling period [<xref ref-type="bibr" rid="scirp.48264-ref26">26</xref>] [<xref ref-type="bibr" rid="scirp.48264-ref27">27</xref>] .</p></sec><sec id="s6"><title>6. Synthesis and Implementation of an Algorithm of Estimating an Attraction Domain</title><p>In this section, we suggest a synthesis algorithm which allows formulating the principal steps leading to the es- timate of an asymptotic stability region of the discrete nonlinear systems [<xref ref-type="bibr" rid="scirp.48264-ref24">24</xref>] . Thus, the estimated ASR can be arbitrarily approximated by means of sequence of convergence of simple successive fields generated by Equa- tion (13). Firstly, we start with an Initial Region of Asymptotic Stability (IRAS) noted by<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\471d2583-adf0-4015-bc74-a00537991298.png" xlink:type="simple"/></inline-formula>. A new field is, then, obtained by applying the first iteration of (13).</p><p>This algorithm is presented in 4 steps:</p><p>Step 1: It tends to determine the system equilibrium points out of the original point and to analyze the local stability of each point.</p><p>Step 2: It is likely to determine an IRAS <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\844829d7-d91e-4034-a08c-0da4bdf8d3f3.png" xlink:type="simple"/></inline-formula> in the space around each asymptotically stable equilibrium point.</p><p>Step 3: It concerns the development of an iterative calculation based on Equation (13) initialized by a depar- ture stability field <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\f7fe48da-264e-45c7-b464-a6e12697ca10.png" xlink:type="simple"/></inline-formula> determined in Step 2.</p><p>Step 4: It consists in stopping the iterative calculation based on Equation (13) when a broad ASR is obtained after the convergence of the curve towards a limited form.</p><p>The application of Step 1 does not generally present any difficulty, contrary to the determination of a IRAS. In order to solve this problem, we used a technique presented in [<xref ref-type="bibr" rid="scirp.48264-ref22">22</xref>] [<xref ref-type="bibr" rid="scirp.48264-ref23">23</xref>] .</p><p>The detailed analysis of the algorithm allows us to deduce some remarks and conclusions similar to the case of the reverse trajectory method considered for the continuous systems. Actually, the topological and graphic character on which this algorithm is based shows some difficulties for the high order systems. Nevertheless, it remains effective for reduced order systems<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\26136c81-f11a-47a0-9f5e-530be562f5b4.png" xlink:type="simple"/></inline-formula>.</p><p>• Concerning the second order systems, the method converges towards a sufficiently large asymptotic stability region in a minimal time. This result comprises a very important performance in the context of synthesizing control laws that will be established on line [<xref ref-type="bibr" rid="scirp.48264-ref28">28</xref>] .</p><p>• For the systems of order higher than two, the method remains also applicable only to widen the initial asymp- totic stability region. A sufficient number of <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\f0e96a92-d98b-4787-bee4-e964d94b4470.png" xlink:type="simple"/></inline-formula> reverse iterations allows obtaining a border <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\40b2e7e7-ef9b-4781-9298-b9ec4747e931.png" xlink:type="simple"/></inline-formula> which lim- its a larger domain of asymptotic stability<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\3837c0b5-8d3a-49c5-9b9a-b9a2736bfcea.png" xlink:type="simple"/></inline-formula>.</p><p>Theorem [<xref ref-type="bibr" rid="scirp.48264-ref25">25</xref>] :</p><p>The discrete time state variables of Equation (13) are exponentially stable in the ball<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\114dc358-3a7f-40bf-b276-e230e6c3b219.png" xlink:type="simple"/></inline-formula>, where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\6b65aa3a-f245-4ee2-a48c-11db448c426c.png" xlink:type="simple"/></inline-formula> is the positive solution of the polynomial equation:</p><disp-formula id="scirp.48264-formula2620"><label>(31)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\3985964c-621f-4eef-b510-d10aecc20992.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\cf7e55d0-ccd4-4456-9779-0f8e6fb7ebaa.png" xlink:type="simple"/></inline-formula> are positive numbers verifying:</p><disp-formula id="scirp.48264-formula2621"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\fe0da74d-c5ba-4d61-b7d7-3c5de825b84e.png"/></disp-formula></sec><sec id="s7"><title>7. Simulation Results</title><p>The problem of transitory stability of the generator-systems becomes increasingly important because of the re- markable increase in the network dimensions of production and the transport of electrical energy [<xref ref-type="bibr" rid="scirp.48264-ref29">29</xref>] [<xref ref-type="bibr" rid="scirp.48264-ref30">30</xref>] .</p><p>It is perceived that the stability of the production systems of electrical energy is never global but local around an operating state considered as an equilibrium state.</p><p>This typical problem brought about by the disturbances in the production systems stability is the main factor that encouraged us to consider the exact asymptotic stability region of the considered systems [<xref ref-type="bibr" rid="scirp.48264-ref31">31</xref>] [<xref ref-type="bibr" rid="scirp.48264-ref32">32</xref>] .</p><p>The very study is about the application of the method of the suggested approaches to the linearizing control of a synchronous generator.</p><p>The synchronous generator can be described by a model of order three characterized by the state vector [<xref ref-type="bibr" rid="scirp.48264-ref33">33</xref>] :</p><disp-formula id="scirp.48264-formula2622"><label>(32)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\4fbb01c6-8f66-4bfd-886b-ee8bd723cbdd.png"/></disp-formula><p>As for input, it has the excitation tension<inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\86bdac43-66dd-44bf-9356-d122753b2f9e.png" xlink:type="simple"/></inline-formula>.</p><p>The following Equations represent this model [<xref ref-type="bibr" rid="scirp.48264-ref34">34</xref>] :</p><disp-formula id="scirp.48264-formula2623"><label>(33)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\d0a21775-219f-47de-a180-cd95844dbd03.png"/></disp-formula><p>where <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\ed0a2fd9-fe74-4076-9a5d-44db4fa1a28d.png" xlink:type="simple"/></inline-formula> is an additional component which is expected to improve the performance of the small-scale model of the generator, and <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\4e6a88a8-8e64-4c49-8126-1304d102a945.png" xlink:type="simple"/></inline-formula> for <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\d052b6f7-f6d1-40cf-8a80-5a845e21ec64.png" xlink:type="simple"/></inline-formula> are the constants given by:</p><disp-formula id="scirp.48264-formula2624"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\a26cd0cc-f38f-4772-a7fe-ee92295ab4fe.png"/></disp-formula><p>The development of the Equations around an operating point <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\948896c5-aa0a-48d0-a717-4b82481c55c8.png" xlink:type="simple"/></inline-formula> leads to the following polynomial non-linear model [<xref ref-type="bibr" rid="scirp.48264-ref35">35</xref>] :</p><disp-formula id="scirp.48264-formula2625"><label>(34)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\f94ce513-7710-4d6a-a5c6-a18d4b44ccb5.png"/></disp-formula><p>where</p><disp-formula id="scirp.48264-formula2626"><label>(35)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\5f202c73-4e7c-422e-aa46-3fcfcb60dc56.png"/></disp-formula><p>The studied generator is characterized by the parameters expressed in the following reduced values (per unit “p.u”) [<xref ref-type="bibr" rid="scirp.48264-ref34">34</xref>] :</p><disp-formula id="scirp.48264-formula2627"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\13abd512-a6e8-498c-b687-539dfa57b334.png"/></disp-formula><p>The discretization of the continuous model of the synchronous generator leads to a polynomial model of the following form:</p><disp-formula id="scirp.48264-formula2628"><label>(36)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\7ac3c2b7-aafd-4cff-ac9b-1d0531391323.png"/></disp-formula><p>with:</p><disp-formula id="scirp.48264-formula2629"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\edbdf285-dc0a-4f12-a509-c45593061f1c.png"/></disp-formula><disp-formula id="scirp.48264-formula2630"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\edbdf285-dc0a-4f12-a509-c45593061f1c.png"/></disp-formula><disp-formula id="scirp.48264-formula2631"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\edbdf285-dc0a-4f12-a509-c45593061f1c.png"/></disp-formula><disp-formula id="scirp.48264-formula2632"><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\edbdf285-dc0a-4f12-a509-c45593061f1c.png"/></disp-formula><p>The application of the control approach to the obtained discrete model lets us determine a polynomial control law:</p><disp-formula id="scirp.48264-formula2633"><label>(37)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\2684d3b2-cf04-4c60-85ae-a257e03394c4.png"/></disp-formula><p>And a non-linear transformation</p><disp-formula id="scirp.48264-formula2634"><label>(38)</label><inline-graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\6ec8889e-58ba-4725-8e33-192a22744b6d.png"/></disp-formula><p>The line matrix <inline-formula><inline-graphic xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\4162abf0-492a-4a85-914e-daad53a8083e.png" xlink:type="simple"/></inline-formula> is, in fact, selected in a way that the dynamics of the arbitrary linear system is defined by poles equal to 0.6, 0.7, 0.7 which yield:</p><fig-group id="fig1"><caption><title>Figure 1</title><p> Evolution of the state<img src="htmlimages\7-2340123x\439764cb-5295-40b4-b1be-e5fb5e73196d.png" width="36.25" height="37.5" /></p></caption><fig id ="fig1_1"><label>The line matrices and are given by:</label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\e6aa5ccf-c6b7-408c-a120-253891365225.png"/></fig><fig id ="fig1_2"><label></label><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\75491c8d-9a9d-46ce-a3a6-5304c33e8cd1.png"/></fig></fig-group><fig id="fig2"><label>Figure 2</label><caption><p> Evolution of the state<img src="htmlimages\7-2340123x\57a07865-4268-4e5d-8626-7ed4f8c19e9e.png" width="37.5" height="37.5" /></p></caption><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\9bb7df55-409e-4808-9e6a-cb9e4f450605.png"/></fig><fig id="fig3"><label>Figure 3</label><caption><p> Evolution of the state<img src="htmlimages\7-2340123x\54646391-aac4-4760-bd4c-421c1dfac8da.png" width="37.5" height="37.5" /></p></caption><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\dafcc6bb-6ee8-40d7-a5a8-bbf7b0660d44.png"/></fig><fig id="fig4"><label>Figure 4</label><caption><p> Evolution of control<img src="htmlimages\7-2340123x\33156fb7-231a-4104-886a-5a57adb82ba4.png" width="28.75" height="36.25" /></p></caption><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\b80bd4cf-25fc-4f4d-b4d6-22e9bf776fb5.png"/></fig><fig id="fig5"><label>Figure 5</label><caption><p> Aymptotic stability region of two Axes</p></caption><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\97de65bc-b127-40ea-8ee6-3e91c51a013f.png"/></fig><fig id="fig6"><label>Figure 6</label><caption><p> Asymptotic stability region of the synchronous generator</p></caption><graphic xmlns:xlink="http://www.w3.org/1999/xlink" xlink:href="http://file.scirp.org/Html/htmlimages\7-2340123x\14eaaa49-aca8-436f-b46e-70acbaba6433.png"/></fig><p>Indeed, we may notice that the variables quickly return to the origin and that the recorded excesses remain within the tolerated limits. The same conclusion can be drawn to the control signal which permits to ensure this powerful regulation.</p><p>The discrete Reverse Trajectory Method (RTM) is theoretically exploitable for any locally stable nonlinear system. Moreover, it proves its effectiveness through the advantage of being numerically implementable for high order systems. What is more, one may also note that the performance of this method largely depends on the determination of an asymptotic initial region which will be used as an initial field for integration in opposite di- rection. We apply RTM so as to determine an Asymptotic Stability Region (ASR). The results of this step are given in <xref ref-type="fig" rid="fig5">Figure 5</xref> and <xref ref-type="fig" rid="fig6">Figure 6</xref>.</p><p>We notice, in <xref ref-type="fig" rid="fig5">Figure 5</xref> and <xref ref-type="fig" rid="fig6">Figure 6</xref>, the method remains applicable to the systems of order higher than two.</p></sec></body><back><ref-list><title>References</title><ref id="scirp.48264-ref1"><label>1</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>CAMILLI</surname><given-names> F. </given-names></name>,<name name-style="western"><surname> LORETI</surname><given-names> P. </given-names></name>,<etal>et al</etal>. (<year>2006</year>)<article-title>A ZUBOV’S METHOD FOR STOCHASTIC DIFFERENTIAL EQUATIONS</article-title><source> NONLINEAR DIFFERENTIAL EQUATIONS AND APPLICATIONS</source><volume> 13</volume>,<fpage> 205</fpage>-<lpage>222</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1007/S00030-005-0036-1</pub-id></mixed-citation></ref><ref id="scirp.48264-ref2"><label>2</label><mixed-citation publication-type="other" xlink:type="simple">LYAPUNOV, A.M. (1892) THE GENERAL PROBLEM OF THE STABILITY OF MOTION. KHARKOV MATHEMATICAL SOCIETY, KHARKOV.</mixed-citation></ref><ref id="scirp.48264-ref3"><label>3</label><mixed-citation publication-type="other" xlink:type="simple">ZUBOV, V.I. (1964) METHODS OF A. M. LYAPUNOV AND THEIR APPLICATION. NOORDHO.</mixed-citation></ref><ref id="scirp.48264-ref4"><label>4</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>CHESI</surname><given-names> G.</given-names></name>,<name name-style="western"><surname> GARULLI</surname><given-names> A.</given-names></name>,<name name-style="western"><surname> TESI</surname><given-names> A. </given-names></name>,<name name-style="western"><surname> VICINO</surname><given-names> A. </given-names></name>,<etal>et al</etal>. (<year>2005</year>)<article-title>LMI-BASED COMPUTATION OF OPTIMAL QUADRATIC LYAPUNOV FUNCTIONS FOR ODD POLYNOMIAL SYSTEMS</article-title><source> INTERNATIONAL JOURNAL OF ROBUST AND NONLINEAR CONTROL</source><volume> 15</volume>,<fpage> 35</fpage>-<lpage>49</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1002/RNC.967</pub-id></mixed-citation></ref><ref id="scirp.48264-ref5"><label>5</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>CHESI</surname><given-names> G.</given-names></name>,<name name-style="western"><surname> GARULLI</surname><given-names> A.</given-names></name>,<name name-style="western"><surname> TESI</surname><given-names> A. </given-names></name>,<name name-style="western"><surname> VICINO</surname><given-names> A. </given-names></name>,<etal>et al</etal>. (<year>2004</year>)<article-title>ROBUST ANALYSIS OF LFR SYSTEMS THROUGH HOMOGENEOUS POLYNOMIAL LYAPUNOV FUNCTIONS</article-title><source> IEEE TRANSACTIONS ON AUTOMATIC CONTROL</source><volume> 49</volume>,<fpage> 1211</fpage>-<lpage>1216</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1109/TAC.2004.831152</pub-id></mixed-citation></ref><ref id="scirp.48264-ref6"><label>6</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>HU</surname><given-names> T. </given-names></name>,<name name-style="western"><surname> LIN</surname><given-names> Z. </given-names></name>,<etal>et al</etal>. (<year>2003</year>)<article-title>COMPOSITE QUADRATIC LYAPUNOV FUNCTIONS FOR CONSTRAINED CONTROL SYSTEMS</article-title><source> IEEE TRANSACTIONS ON AUTOMATIC CONTROL</source><volume> 48</volume>,<fpage> 440</fpage>-<lpage>450</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1109/TAC.2003.809149</pub-id></mixed-citation></ref><ref id="scirp.48264-ref7"><label>7</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>BENHADJ BRAIEK</surname><given-names> N. </given-names></name>,<etal>et al</etal>. (<year>1996</year>)<article-title>DETERMINATION OF A STABILITY RADIUS FOR DISCRETE NONLINEAR SYSTEMS</article-title><source> JOURNAL OF SYSTEMS ANALYSIS MODELLING AND SIMULATION</source><volume> 22</volume>,<fpage> 315</fpage>-<lpage>322</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.48264-ref8"><label>8</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>CAO</surname><given-names> Y. </given-names></name>,<name name-style="western"><surname> LIN</surname><given-names> Z. </given-names></name>,<etal>et al</etal>. (<year>2003</year>)<article-title>STABILITY ANALYSIS OF DISCRETE-TIME SYSTEMS WITH ACTUATOR SATURATION BY A SATURATION-DEPENDENT LYAPUNOV FUNCTION</article-title><source> AUTOMATICA</source><volume> 39</volume>,<fpage> 1235</fpage>-<lpage>1241</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/S0005-1098(03)00072-4</pub-id></mixed-citation></ref><ref id="scirp.48264-ref9"><label>9</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>COUTINHO</surname><given-names> D.F.</given-names></name>,<name name-style="western"><surname> FU</surname><given-names> M. </given-names></name>,<name name-style="western"><surname> TROFINO</surname><given-names> A. </given-names></name>,<etal>et al</etal>. (<year>2004</year>)<article-title>ROBUST ANALYSIS AND CONTROL FOR A CLASS OF UNCERTAIN NONLINEAR DISCRETE-TIME SYSTEMS</article-title><source> SYSTEMS AND CONTROL LETTERS</source><volume> 53</volume>,<fpage> 377</fpage>-<lpage>393</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/J.SYSCONLE.2004.05.015</pub-id></mixed-citation></ref><ref id="scirp.48264-ref10"><label>10</label><mixed-citation publication-type="other" xlink:type="simple">DIBLIK, J. (2004) ANTI-LYAPUNOV METHOD FOR SYSTEMS OF DISCRETE EQUATIONS. NONLINEAR ANALYSIS: THEORY, METHODS AND APPLICATIONS, 57, 1043-1057.</mixed-citation></ref><ref id="scirp.48264-ref11"><label>11</label><mixed-citation publication-type="other" xlink:type="simple">CHARFEDDINE, S. AND JERBI, H. (2013) A SURVERY OF NON LINEAR GAIN SCHEDULING DESIGN CONTROL OF CONTINUOUS AND DISCRETE TIME SYSTEMS. INTERNATIONAL JOURNAL MODELLING, IDENTIFICATION AND CONTROL, 19, 203-216.HTTP://DX.DOI.ORG/10.1504/IJMIC.2013.055427</mixed-citation></ref><ref id="scirp.48264-ref12"><label>12</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>CHARFEDDINE</surname><given-names> S.</given-names></name>,<name name-style="western"><surname> JERBI</surname><given-names> H. </given-names></name>,<name name-style="western"><surname> SBITA</surname><given-names> L. </given-names></name>,<etal>et al</etal>. (<year>2013</year>)<article-title>CHARFEDDINE, S., JERBI, H. AND SBITA, L.  NONLINEAR DICSRETE-TIME GAIN SCHEDULING CONTROL FOR AFFINE NON LINEAR POLYNOMIAL SYSTEMS</article-title><source> INTERNATIONAL REVIEW ON MODELLING AND SIMULATIONS</source><volume> 6</volume>,<fpage> 1031</fpage>-<lpage>1041</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.48264-ref13"><label>13</label><mixed-citation publication-type="other" xlink:type="simple">CHARFEDDINE, S. AND JERBI, H. (2012) SYNTHESIS OF A POLYNOMIAL DISCRETE TIME CONTROL APPROACH FOR NONLINEAR SYSTEMS. 17TH INTERNATIONAL CONFERENCE ON METHODS &amp; MODELS IN AUTOMATION &amp; ROBOTICS, POLAND, 391-396.</mixed-citation></ref><ref id="scirp.48264-ref14"><label>14</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>TABABE</surname><given-names> K. </given-names></name>,<etal>et al</etal>. (<year>1985</year>)<article-title>GLOBAL ANALYSIS OF CONTINUOUS ANALOGS OF THE LEVENBERG-MARQUARDT AND NEW-RAPHSON METHODS FOR SOLVING NONLINEAR EQUATION</article-title><source> ANNUAL INSTITUTION STATISTIC MATHEMATIC B</source><volume> 37</volume>,<fpage> 189</fpage>-<lpage>203</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.48264-ref15"><label>15</label><mixed-citation publication-type="other" xlink:type="simple">TABABE, K. (1979) CONTINUOUS NEWTON-RAPHSON METHOD FOR SOLVING AN UNDERDETERMINED SYSTEM OF NONLINEAR EQUATIONS. JOURNAL NONLINEAR ANALYSIS, THEORY METHODS APPLICATION, 3, 495-503.HTTP://DX.DOI.ORG/10.1016/0362-546X(79)90064-6</mixed-citation></ref><ref id="scirp.48264-ref16"><label>16</label><mixed-citation publication-type="other" xlink:type="simple">ISURUGY, Y. AND SHINA, M. (1995) DISCRETISATION OF CONTINUOUS TIME CONTROL LAWS FOR NONLINEAR SYSTEMS WITH COMPUTATIONAL DELAY. PROCEEDINGS OF THE 3RD EUROPEAN CONTROL CONFERENCE, ROME, 1995.</mixed-citation></ref><ref id="scirp.48264-ref17"><label>17</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>CAO</surname><given-names> Y. </given-names></name>,<name name-style="western"><surname> LIN</surname><given-names> Z. </given-names></name>,<etal>et al</etal>. (<year>2003</year>)<article-title>STABILITY ANALYSIS OF DISCRETE-TIME SYSTEMS WITH ACTUATOR SATURATION BY A SATURATION-DEPENDENT LYAPUNOV FUNCTION</article-title><source> AUTOMATICA</source><volume> 39</volume>,<fpage> 1235</fpage>-<lpage>1241</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/S0005-1098(03)00072-4</pub-id></mixed-citation></ref><ref id="scirp.48264-ref18"><label>18</label><mixed-citation publication-type="other" xlink:type="simple">JERBI, H. AND BENHADJ BRAIEK, N. (1999) ON THE DESIGN OF LINEARIZING CONTROLLER FOR NONLINEAR DISCRETE SYSTEMS. IEEE SMC’99 INTERNATIONAL CONFERENCE PROCEEDINGS, TOKYO, 12-15 OCTOBER 1999, 33-37.</mixed-citation></ref><ref id="scirp.48264-ref19"><label>19</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>MCNICHOLS</surname><given-names> K.H. </given-names></name>,<name name-style="western"><surname> FADLI</surname><given-names> M.S. </given-names></name>,<etal>et al</etal>. (<year>2003</year>)<article-title>SELECTING OPERATING POINTS FOR DISCRETE TIME GAIN SCHEDULING</article-title><source> COMPUTERS AND ELECTRICAL ENGINEERING</source><volume> 29</volume>,<fpage> 289</fpage>-<lpage>301</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/S0045-7906(01)00031-3</pub-id></mixed-citation></ref><ref id="scirp.48264-ref20"><label>20</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>MCCONLEY</surname><given-names> M.W.</given-names></name>,<name name-style="western"><surname> APPLEBY</surname><given-names> B.D.</given-names></name>,<name name-style="western"><surname> DAHLEH</surname><given-names> M.A. </given-names></name>,<name name-style="western"><surname> FERON</surname><given-names> E. </given-names></name>,<etal>et al</etal>. (<year>2000</year>)<article-title>A COMPUTATIONALLY EFFICIENT LYAPUNOV-BASED SCHEDULING PROCEDURE FOR CONTROL OF NONLINEAR SYSTEMS WITH STABILITY GUARANTEES</article-title><source> IEEE TRANSACTIONS ON AUTOMATIC CONTROL</source><volume> 45</volume>,<fpage> 33</fpage>-<lpage>49</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1109/9.827354</pub-id></mixed-citation></ref><ref id="scirp.48264-ref21"><label>21</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>ROTELLA</surname><given-names> F. </given-names></name>,<name name-style="western"><surname> BORNE</surname><given-names> P. </given-names></name>,<etal>et al</etal>. (<year>1989</year>)<article-title>EXPLICIT SOLUTION OF SYLVESTER AND LYAPUNOV EQUATION</article-title><source> MATHEMATIC AND COMPUTERS IN SIMULATION</source><volume> 31</volume>,<fpage> 271</fpage>-<lpage>281</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/0378-4754(89)90163-8</pub-id></mixed-citation></ref><ref id="scirp.48264-ref22"><label>22</label><mixed-citation publication-type="other" xlink:type="simple">BACHA, A., JERBI, H. AND BENHADJ BRAIEK, N. (2007) ON THE SYNTHESIS OF A COMBINED DISCRETE REVERSING TRAJECTORY METHOD FOR THE ASYMPTOTIC STABILITY REGION ESTIMATION OF NONLINEAR POLYNOMIAL SYSTEMS. PROCEEDINGS OF 13TH IEEE IFAC, INTERNATIONAL CONFERENCE ON METHODS, MODELS IN AUTOMATION AND ROBOTICS, IEEE CONFERENCE NUMBER 12469, SZCZECIN, 27-30 AUGUST 2007, 243-248.</mixed-citation></ref><ref id="scirp.48264-ref23"><label>23</label><mixed-citation publication-type="other" xlink:type="simple">BACHA, A., JERBI, H. AND BENHADJ BRAIEK, N. (2008) TECHNIQUE OF STABILITY DOMAIN DETERMINATION OF NONLINEAR DISCREET POLYNOMIAL SYSTEM. PROCEEDINGS OF THE 17TH WORLD CONGRESS THE INTERNATIONAL FEDERATION OF AUTOMATIC CONTROL, SEOUL, JUNE 2008, 8690-8694.</mixed-citation></ref><ref id="scirp.48264-ref24"><label>24</label><mixed-citation publication-type="other" xlink:type="simple">BACHA, A., JERBI, H. AND BENHADJ BRAIEK, N. (2008) BACKWARD ITERATION APPROACHES FOR THE STABILITY DOMAIN OF ESTIMATION OF DISCRETE NONLINEAR POLYNOMIAL SYSTEMS. INTERNATIONAL JOURNAL OF MODELLING, IDENTIFICATION AND CONTROL, 5, 313-319. HTTP://DX.DOI.ORG/10.1504/IJMIC.2008.023516</mixed-citation></ref><ref id="scirp.48264-ref25"><label>25</label><mixed-citation publication-type="other" xlink:type="simple">BENHADJ BRAIEK, N., JERBI, H. AND BACHA, A. (2008) TECHNIQUE OF STABILITY DOMAIN DETERMINATION FOR NONLINEAR DISCRETE POLYNOMIAL SYSTEMS. PROCEEDINGS OF IFAC08, SEOUL.</mixed-citation></ref><ref id="scirp.48264-ref26"><label>26</label><mixed-citation publication-type="other" xlink:type="simple">BACHA, A., JERBI, H. AND BENHADJ BRAIEK, N. (2007) A COMPARATIVE STABILITY STUDY BETWEEN TWO NEW BACKWARD ITERATION APPROACHES OF DISCRETE NONLINEAR POLYNOMIAL SYSTEMS. 4TH INTERNATIONAL MULTI-CONFERENCES ON SYSTEMS, SIGNALS AND DEVICES I.</mixed-citation></ref><ref id="scirp.48264-ref27"><label>27</label><mixed-citation publication-type="other" xlink:type="simple">BACHA, A., JERBI, H. AND BENHADJ BRAIEK, N. (2006) AN APPROACH OF ASYMPTOTIC STABILITY DOMAIN ESTIMATION OF DISCRETE POLYNOMIAL SYSTEMS. MATHEMATICAL MODELLING, IDENTIFICATION AND SIMILATION, CESA 2006 WORLD CONGRESS I.</mixed-citation></ref><ref id="scirp.48264-ref28"><label>28</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>JOUILI</surname><given-names> K.</given-names></name>,<name name-style="western"><surname> JERBI</surname><given-names> H. </given-names></name>,<name name-style="western"><surname> BENHDAJ BRAIEK</surname><given-names> N. </given-names></name>,<etal>et al</etal>. (<year>2010</year>)<article-title>AN ADVANCED FUZZY LOGIC GAIN SCHEDULING TRAJECTORY CONTROL FOR NONLINEAR SYSTEMS</article-title><source> JOURNAL OF PROCESS CONTROL</source><volume> 20</volume>,<fpage> 426</fpage>-<lpage>440</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/J.JPROCONT.2010.01.001</pub-id></mixed-citation></ref><ref id="scirp.48264-ref29"><label>29</label><mixed-citation publication-type="other" xlink:type="simple">KUJUNDZIC, S.M. (2004) METHODS AND MODELS FOR STABILITY, CONTROLLABILITY AND RELIABILITY ANALYSIS OF SYSTEMS MOTION. M. FIZMATLIT.</mixed-citation></ref><ref id="scirp.48264-ref30"><label>30</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>QI</surname><given-names> R.</given-names></name>,<name name-style="western"><surname> COOK</surname><given-names> D.</given-names></name>,<name name-style="western"><surname> KLIEMANN</surname><given-names> W. </given-names></name>,<name name-style="western"><surname> VITTAL</surname><given-names> V. </given-names></name>,<etal>et al</etal>. (<year>2000</year>)<article-title>VISUALIZATION OF STABLE MANIFOLDS AND MULTIDIMENSIONAL SURFACES IN THE ANALYSIS OF POWER SYSTEM DYNAMICS</article-title><source> JOURNAL OF NONLINEAR SCIENCES</source><volume> 10</volume>,<fpage> 175</fpage>-<lpage>195</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1007/S003329910008</pub-id></mixed-citation></ref><ref id="scirp.48264-ref31"><label>31</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>UEMURA</surname><given-names> K.</given-names></name>,<name name-style="western"><surname> MATUSKI</surname><given-names> J.</given-names></name>,<name name-style="western"><surname> YAMADA</surname><given-names> J. </given-names></name>,<name name-style="western"><surname> TSUJI</surname><given-names> T. </given-names></name>,<etal>et al</etal>. (<year>1972</year>)<article-title>UEMURA, K., MATUSKI, J., YAMADA, J. AND TSUJI, T.  APPROXIMATION OF AN ENERGY FUNCTION IN TRANSIENT STABILITY ANALYSIS OF POWER SYSTEMS</article-title><source> ELECTRICAL ENGINEER JAPAN</source><volume> 92</volume>,<fpage> 96</fpage>-<lpage>100</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.48264-ref32"><label>32</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>WILLIEMS</surname><given-names> J.L. </given-names></name>,<name name-style="western"><surname> WILLIEMS</surname><given-names> J.C. </given-names></name>,<etal>et al</etal>. (<year>1971</year>)<article-title>WILLIEMS, J.L. AND WILLIEMS, J.C.  THE APPLICATION OF LYAPUNOV METHODS TO THE COMPUTATION OF TRANSIENT STABILITY REGIONS FOR MULTIMACHINE POWER SYSTEMS</article-title><source> IEEE TRANSACTIONS ON POWER APPARATUS AND SYSTEMS</source><volume> 4</volume>,<fpage> 332</fpage>-<lpage>341</lpage>.<pub-id pub-id-type="doi"></pub-id></mixed-citation></ref><ref id="scirp.48264-ref33"><label>33</label><mixed-citation publication-type="other" xlink:type="simple">ANDERSON, P.M. AND FOUAD, A.A. POWER SYSTEM CONTROL AND STABILITY. THE IOWA STATE UNIVERSITY PRESS.</mixed-citation></ref><ref id="scirp.48264-ref34"><label>34</label><mixed-citation publication-type="journal" xlink:type="simple"><name name-style="western"><surname>MIELCZARSKI</surname><given-names> W. </given-names></name>,<name name-style="western"><surname> ZAJACZKOWSKI</surname><given-names> A.M. </given-names></name>,<etal>et al</etal>. (<year>1971</year>)<article-title>NONLINEAR FIELD VOLTAGE CONTROL OF SYNCHRONOUS GENERATOR USING FEEDBACK</article-title><source> AUTOMATICA</source><volume> 30</volume>,<fpage> 1625</fpage>-<lpage>1630</lpage>.<pub-id pub-id-type="doi">HTTP://DX.DOI.ORG/10.1016/0005-1098(94)90102-3</pub-id></mixed-citation></ref><ref id="scirp.48264-ref35"><label>35</label><mixed-citation publication-type="other" xlink:type="simple">JERBI, H. AND BENHADJ BRAIEK, N. (1995) MODÉLISATION PAR LINÉARISATION ET COMMANDE D’UN GÉNÉRATEUR SYNCHRONE. CONGRÈS MAGHRÉBIN DE GÉNIE ELECTRIQUE.</mixed-citation></ref></ref-list></back></article>