<?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">AM</journal-id><journal-title-group><journal-title>Applied Mathematics</journal-title></journal-title-group><issn pub-type="epub">2152-7385</issn><publisher><publisher-name>Scientific Research Publishing</publisher-name></publisher></journal-meta><article-meta><article-id pub-id-type="doi">10.4236/am.2012.36082</article-id><article-id pub-id-type="publisher-id">AM-20085</article-id><article-categories><subj-group subj-group-type="heading"><subject>Articles</subject></subj-group><subj-group subj-group-type="Discipline-v2"><subject>Physics&amp;Mathematics</subject></subj-group></article-categories><title-group><article-title>
 
 
  Basins of Attraction in the Copenhagen Problem Where the Primaries Are Magnetic Dipoles
 
</article-title></title-group><contrib-group><contrib contrib-type="author" xlink:type="simple"><name name-style="western"><surname>ilemachos</surname><given-names>J. Kalvouridis</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>Maria</surname><given-names>Ch. Gousidou-Koutita</given-names></name><xref ref-type="aff" rid="aff2"><sup>2</sup></xref><xref ref-type="corresp" rid="cor1"><sup>*</sup></xref></contrib></contrib-group><aff id="aff2"><addr-line>Department of Mathematics, Faculty of Sciences, Aristotle University of Thessaloniki, Thessaloniki, Greece</addr-line></aff><aff id="aff1"><addr-line>Department of Mechanics, Faculty of Applied Sciences, National Technical University of Athens, Athens, Greece</addr-line></aff><author-notes><corresp id="cor1">* E-mail:<email>tkalvouridis@gmail.com(IJK)</email>;<email>gousidou@math.auth.gr(MCG)</email>;</corresp></author-notes><pub-date pub-type="epub"><day>21</day><month>06</month><year>2012</year></pub-date><volume>03</volume><issue>06</issue><fpage>541</fpage><lpage>548</lpage><history><date date-type="received"><day>March</day>	<month>14,</month>	<year>2012</year></date><date date-type="rev-recd"><day>April</day>	<month>11,</month>	<year>2012</year>	</date><date date-type="accepted"><day>April</day>	<month>18,</month>	<year>2012</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>
 
 
  We deal with the Copenhagen problem where the two big bodies of equal masses are also magnetic dipoles and we study some aspects of the dynamics of a charged particle which moves in the electromagnetic field produced by the primaries. We investigate the equilibrium positions of the particle and their parametric variations, as well as the basins of attraction for various numerical methods and various values of the parameter 
  λ.
 
</p></abstract><kwd-group><kwd>Copenhagen Problem with Magnetic Dipoles; Equilibrium Locations; Basins of Attraction; Solution of Non-Linear Algebraic Systems; Newton and Quasi-Newton Methods; Comparison of Numerical Methods</kwd></kwd-group></article-meta></front><body><sec id="s1"><title>1. Introduction</title><p>The Copenhagen problem is a particular case of the famous restricted three-body problem where the two big spherical and homogeneous primaries have equal masses and rotate with constant angular velocity in circular orbits around their centre of mass, while a small massless particle moves under the resultant Newtonian action of the two primaries. The problem was exhaustively studied by Stromgren and his collaborators in the decade of 1920’s and has been revisited during the last ten years after the discovery of many exosolar planetary systems. A large part of these systems that have been identified since 1990, are two-body systems where the two primaries have almost equal masses. In this work we deal with a very interesting version of the Copenhagen problem in which we consider that the two big primaries are also magnetic dipoles and that the particle is a small charge which moves in the electromagnetic field produced by the two rotating dipoles. This new consideration besides the application to the aforementioned dynamical systems could also be applied to magnetic binary stars, the existence of which has been already confirmed. The dynamics of a charged particle in a magnetic binary system has been studied in the past ([1,2]). The material of this work is organized in four sections. In the first section we extract the equations of motion of the charged particle, in the second section we study the equilibrium positions, their stability and their parametric variation, in the third section we investigate the basins of attraction of these equilibria by applying two well known numerical methods, the Newton’s method and an improved Modified Broyden’s one. Finally, in the last section, we discuss the obtained results and we expose some of the major conclusions concerning our investigation.</p></sec><sec id="s2"><title>2. The Problem</title><p>We consider a synodic coordinate system Oxyz centered at the mass centre O of the system, where the plane Oxy is the plane of the primaries’ motion, and the x-axis is the axis of syzygies of the primaries which create dipoletype magnetic fields. We assume that the axes of the magnetic moments are perpendicular to the Oxy plane and that the primaries rotate about their centre of mass in circular orbits with constant angular velocity ω (<xref ref-type="fig" rid="fig1">Figure 1</xref>). That is</p><p><img src="7-7400778\b1ec11a3-5bab-4114-b56e-4e98eb63a37c.jpg" />, i = 1, 2.</p><p>The magnetic inductions of the dipoles are,</p><p><img src="7-7400778\c4dc5bb4-8beb-45b6-a1ca-3dfddf21c6b9.jpg" />, i = 1, 2 where <img src="7-7400778\1ca36d19-0d34-4c88-9e79-da4bdc8786d1.jpg" /> are the vector potentials. From Faraday’s law we obtain</p><p><img src="7-7400778\0f3b1eb3-bdf0-4e6d-bc6c-920f74f49bd3.jpg" />, i = 1, 2.</p><p>A small particle of charge q and mass m is acted upon by a Lorentz’s force created by the two rotating primaries P<sub>1</sub> and P<sub>2</sub></p><p><img src="7-7400778\b1a662e7-0db7-4662-a64f-a53e5047092d.jpg" />,</p><p>where</p><p><img src="7-7400778\f77f42fd-60ef-4597-8c1a-f10a385150b8.jpg" />,<img src="7-7400778\6dbbb022-7d85-4510-9d78-c7a210111449.jpg" />.</p><p>Under these assumptions, the normalized differential equations that describe the planar motion of S in the synodic coordinate system Oxyz, are,</p><disp-formula id="scirp.20085-formula135708"><label>(1)</label><graphic position="anchor" xlink:href="7-7400778\44a40772-b1de-4b51-b645-79c059414654.jpg"  xlink:type="simple"/></disp-formula><p>where</p><p><img src="7-7400778\ad01d4ee-d86c-44ad-bb43-394be03d6253.jpg" /></p><p>is the potential function, A<sub>x</sub>, A<sub>y</sub> are the x and y-components of the vector potential of the resultant electromagnetic field expressed in the synodic system, with</p><p><img src="7-7400778\04dfd8d2-a647-4eb6-a719-fe0cc6509f32.jpg" />, <img src="7-7400778\44c03e72-1209-491d-9813-4cb1928c33b1.jpg" />,</p><p><img src="7-7400778\da19a6d9-5643-4d0f-8be7-42c99922c3cf.jpg" />, <img src="7-7400778\c0824834-0a0f-4f53-ab40-9b4af34db4de.jpg" /></p><p>where r<sub>1</sub> and r<sub>2</sub> are the distances of the particle from the primaries,</p><p><img src="7-7400778\94894c0a-2703-4ff4-ab7f-eaa8b7a2210b.jpg" />,</p><p><img src="7-7400778\9955fd03-a607-4ecc-878d-af08b610e5da.jpg" />,</p><p><img src="7-7400778\3f6cf8b2-a8cd-4d43-b3d1-f377b861ba53.jpg" />, <img src="7-7400778\8da625f3-fe5e-443e-9523-016c8717495d.jpg" />, <img src="7-7400778\bdb680fd-3da0-424a-90af-923405f65c85.jpg" /></p><p>or analytically,</p><p><img src="7-7400778\4a9310ec-7d6e-4306-885f-980bb404d4a3.jpg" /></p><p><img src="7-7400778\05b38f16-a92e-48b8-84ac-232e9ebf67f7.jpg" /></p><p>and</p><p><img src="7-7400778\25642cb1-dc7f-45ca-848e-5e32509a1b34.jpg" /></p><p>with</p><p><img src="7-7400778\59693ce6-3afb-4bf0-bf6b-7d761a1c5bc0.jpg" />, <img src="7-7400778\04762911-61fc-4adb-b37a-595af160f083.jpg" />, <img src="7-7400778\b725e9b8-602d-4be6-98d3-5c3cab9c4c7d.jpg" /></p><p>The dynamical system is characterized by the parameter <img src="7-7400778\489f213b-0da2-425c-9e08-062ba0cf1e05.jpg" /> which is the ratio of the two magnetic moments. Since parameter λ connects the magnitudes of these moments, its role in the formation of the resultant electromagnetic field is very important. From Equation (1) we obtain a Jacobian-type integral of motion which has the form</p><disp-formula id="scirp.20085-formula135709"><label>(2)</label><graphic position="anchor" xlink:href="7-7400778\1f62d872-3cee-46fc-a3ca-ee3db39a9a10.jpg"  xlink:type="simple"/></disp-formula><p>where C is a constant that is called the Jacobian constant or energy constant.</p></sec><sec id="s3"><title>3. Equilibrium Locations and Their Parametric Variation</title><p>As it is known, in an equilibrium position on the plane of the primaries’ revolution the following conditions hold,</p><disp-formula id="scirp.20085-formula135710"><label>(3)</label><graphic position="anchor" xlink:href="7-7400778\a25a4733-0137-4e7a-825c-543be5e38a55.jpg"  xlink:type="simple"/></disp-formula><p>Therefore, the coordinates of these positions are the solutions of the system of non-linear algebraic equations,</p><disp-formula id="scirp.20085-formula135711"><label>(4)</label><graphic position="anchor" xlink:href="7-7400778\ece5eee6-76ce-412e-b87d-127ca96b4c8e.jpg"  xlink:type="simple"/></disp-formula><p>We have found that for our case where the magnetic moments are perpendicular on the plane of the primaries’ revolution, all the equilibrium positions of the particle are located on this plane. Some of these points are dynamically equivalent, which means that are characterized by the same Jacobian constant C and by the same state of stability. Τhe total number of the existing equilibrium locations depends on the value of parameter λ. More precisely:</p><p>• When <img src="7-7400778\a9e70994-5340-4c68-8f5d-dae5165814d9.jpg" /> there are three collinear equilibrium positions (L<sub>1</sub>, L<sub>2</sub>, L<sub>3</sub>).</p><p>• When 2.6 ≤ λ ≤ 10.8, there are three collinear positions (L<sub>1</sub>, L<sub>2</sub>, L<sub>3</sub>) and four triangular positions that form two pairs (L<sub>4</sub>, L<sub>5</sub>) and (L<sub>6</sub>, L<sub>7</sub>). The points of each pair are symmetric with respect of the x-axis and are dynamically equivalent since they are characterized by the same Jacobian constant C and the same state of stability.</p><p>• When λ &gt; 10.8 there are three collinear points (L<sub>1</sub>, L<sub>2</sub>, L<sub>3</sub>) and one pair of dynamically equivalent triangular points (L<sub>4</sub>, L<sub>5</sub>).</p><p><xref ref-type="fig" rid="fig2">Figure 2</xref> shows the distribution of these equilibria on the Oxy plane for various λ.</p></sec><sec id="s4"><title>4. Methods and Algorithms for Finding the Basins of Attraction</title><sec id="s4_1"><title>4.1. Basins of Attraction</title><p>As we have mentioned before, in order to locate the equilibrium positions of the particle, we have to solve numerically the non-linear algebraic system (4). This is achieved by applying an iterative scheme, provided that an initial approximation is given. This starting value represents a point on plane (x, y). The iterator stops when some predetermined accuracy is reached for an equilibrium point which can be considered as an “attractor” of the method. We call the set of the initial points that lead to the discrete equilibrium points or the dynamically equivalent points, “basins of attraction” (or “basins of convergence”, or “attracting domains”). These regions have been studied in the past in some problems of Celestial Dynamics, such as the restricted three-body problem [<xref ref-type="bibr" rid="scirp.20085-ref3">3</xref>], the ring problem of (N + 1)-bodies [4-8], and the Hill’s problem with radiation and oblateness [<xref ref-type="bibr" rid="scirp.20085-ref9">9</xref>]. The technique to find these regions is based on a double scanning process of the Oxy plane. Here, we have considered the intervals<img src="7-7400778\2b6f63d7-4a19-4f10-b291-7347172ade8a.jpg" />, <img src="7-7400778\6b38d1d9-7148-482a-8aed-4993d1870676.jpg" />for the vertical and the horizontal scanning respectively and a step equal to 0.005. We have created in this way a dense grid, the nodes of which are the initial values of the algorithm in use. In all the considered cases we have used 10<sup>−8</sup> as the accuracy criterion to terminate the iterative process. We have stored in separate files all the initial points that lead to dynamically equivalent equilibrium points. At the same time, for each initial point, we have recorded the number of the iterations required to find the equilibrium position with the aforementioned accuracy. Naturally, the number of the iterations required to locate an equilibrium position depends on the predetermined accuracy, while the number of the points that</p><p>constitute the set of the attracting domain of dynamically equivalent set of equilibrium positions depends on the step-size of the scanning process, and the method used. At this point we notice that many numerical methods solving systems of nonlinear algebraic equations have been proposed and described in the past (see for example [10,11]). In what follows we briefly describe the two algorithms used, that is, the old classic Newton’s algorithm and a modified version of Broyden’s iteration scheme.</p></sec><sec id="s4_2"><title>4.2. The Numerical Methods Used</title><sec id="s4_2_1"><title>4.2.1. Newton’s Algorithm</title><p>For our particular problem this very popular and simple algorithm takes the form,</p><disp-formula id="scirp.20085-formula135712"><label>(5)</label><graphic position="anchor" xlink:href="7-7400778\4bbcbb3c-6d4f-496a-9abb-3cb9bf534570.jpg"  xlink:type="simple"/></disp-formula><p><img src="7-7400778\eeef0ab0-0e2f-42bd-95c6-c1082c23bb5a.jpg" />, <img src="7-7400778\6526d6c9-1edc-4115-9f22-128a0f83075f.jpg" />are the values of x and y at the n-th approximation of the iteration process. Relations (5) can also be written in the form,</p><p><img src="7-7400778\c75f52ee-4412-405d-a2f6-c25b275d89a1.jpg" /></p><p>where <img src="7-7400778\4eab44fb-aae0-47f3-adf8-03ab3d51c7d8.jpg" /> is the Jacobian matrix</p><p><img src="7-7400778\46157ea7-9676-4dce-b149-11ef47b821a6.jpg" />.</p></sec><sec id="s4_2_2"><title>4.2.2. Modified Broyden’s Method</title><p>Broyden’s method is based on the secant’s one (it is a generalization of it) and belongs to a class of methods called quasi-Newton. We suppose that <img src="7-7400778\ca636c7e-b028-4381-be61-fa5f5fa81d75.jpg" /> is an initial solution <img src="7-7400778\210affbe-2066-46ea-a9eb-71f9a0e391e0.jpg" /> of the non-linear system</p><p><img src="7-7400778\2437d131-5bee-438f-9eaa-d0c1d5d08e4d.jpg" /></p><p>and we compute the Jacobian matrix</p><p><img src="7-7400778\1c817f5c-cf5c-40b9-913f-dfccd4bf5a92.jpg" /></p><p>and its inverse</p><p><img src="7-7400778\0358966b-5cc9-4b45-a659-08bdf796d09b.jpg" /></p><p>We calculate the next approximation<img src="7-7400778\c5fd1aae-270c-44d2-b2f6-9cb9ee8958a9.jpg" /> in the same manner as in Newton’s method and then we determine <img src="7-7400778\a4da17f7-8c3f-4d6a-8f0c-d53a97db124e.jpg" />, for n = 2, 3, ∙∙∙solving the system<img src="7-7400778\b69665e3-2879-40bb-9cc4-5444260aca01.jpg" />, at each step, until the criterion of convergence is satisfied. In this method <img src="7-7400778\306af0d1-8223-43ac-b605-d5474604f661.jpg" /> has replaced the Jacobian matrix <img src="7-7400778\34f2dd9a-c112-45a3-b85e-a2a368d6bf58.jpg" />that appears in Newton-Raphson’s method.</p><p>This is the main difference between the two methods. Broyden’s method has convergence that is called “superlinear”; this implies that <img src="7-7400778\88f9ecb9-b35e-47bf-a830-71bcba9a70fa.jpg" />On the contrary, Newton’s method has a “quadratic” convergence. For our problem,</p><p><img src="7-7400778\8c4204ef-1225-47b7-81b7-38a6b2063dcf.jpg" /></p><p>and</p><disp-formula id="scirp.20085-formula135713"><label>(6)</label><graphic position="anchor" xlink:href="7-7400778\acf01c01-0a30-49cf-9567-c18e0aa3b247.jpg"  xlink:type="simple"/></disp-formula><p>for Broyden’s method, where <img src="7-7400778\5812a9dd-9fe8-4d32-8911-71e617260dc1.jpg" /> is given by the formula:</p><disp-formula id="scirp.20085-formula135714"><label>(7)</label><graphic position="anchor" xlink:href="7-7400778\40c00527-bffd-4326-887a-0cd9d5285424.jpg"  xlink:type="simple"/></disp-formula><p>where<img src="7-7400778\f9c75e6f-dfab-46fe-90cf-a892ae3d37dd.jpg" />. This method has been applied by Gousidou and Kalvouridis [5-8].</p><p>An improvement of Broyden’s method is based on the Sherman-Morrison’s matrix inversion formula. This formula computes the inverse matrix <img src="7-7400778\d5f658bd-8a90-4b4c-b065-c410cbd626c8.jpg" /> directly from<img src="7-7400778\fbd679b2-c1a9-4467-8fc8-39e1086c6bba.jpg" />, eliminating in this way, the need for a matrix inversion in each iterative step. So, we have not to inverse the matrix<img src="7-7400778\a4928fc4-dd19-4c5c-8396-2218b6ed70dc.jpg" />, which appears in Newton’s method</p><disp-formula id="scirp.20085-formula135715"><label>(8)</label><graphic position="anchor" xlink:href="7-7400778\312c3536-081b-47b0-b67f-4a30cebe47d0.jpg"  xlink:type="simple"/></disp-formula><p>and not need to solve a system</p><p><img src="7-7400778\f15429cc-ee5a-4acb-b70f-d8f1f218c63a.jpg" /></p><p>with</p><p><img src="7-7400778\5bb36b84-28b9-4092-ad13-d502fe9af699.jpg" />in each iteration, as it is needed in Broyden’s method. Its convergence is also “superlinear”, but with less number of operations than the original Broyden’s method, since the operations that are needed are those for the multiplication of a matrix by a vector, as it is resulted from the formula:</p><disp-formula id="scirp.20085-formula135716"><label>(9)</label><graphic position="anchor" xlink:href="7-7400778\c4e7a078-8722-4f03-920c-516eb5558207.jpg"  xlink:type="simple"/></disp-formula><p>where</p><p><img src="7-7400778\0a59a67e-d945-4625-af29-755b20b37ddf.jpg" /></p><p>and</p><p><img src="7-7400778\181b7d29-cced-4064-b033-33b786e7fa9b.jpg" />, for<img src="7-7400778\04e6853d-2194-49a7-8f47-f6d8a186eb79.jpg" />, (10)</p><p>(Faires and Burden [<xref ref-type="bibr" rid="scirp.20085-ref12">12</xref>]).</p></sec></sec></sec><sec id="s5"><title>5. Discussion of the Results</title><sec id="s5_1"><title>5.1. General Remarks and Comments</title><p>Newton-Raphson’s method gives a greater number of converging points per equilibrium point, in comparison to Broyden’s method which gives a few number of converging points. This is shown in the bar charts of <xref ref-type="fig" rid="fig3">Figure 3</xref> for the three considered cases with λ = 2, 10 and 12.</p><p>The general structure of the obtained basins of attracttions generally consists of some very dense parts that mainly evolve around the respective equilibrium point and of dispersed points that lie on the boundaries of the dense regions of this equilibrium or other ones. Figures 4-7 illustrate the results obtained from our investigation. The two methods provide results showing similarities and differences that mostly arise from the philosophy and the geometric origin of the individual method.</p><p>Fundamental similarities:</p><p>• In all diagrams, the shapes of the central parts of the corresponding attracting regions that evolve in the neighborhood of the dynamically equivalent equilibrium points are similar.</p><p>• The boundaries of these central parts are not clearly defined. They look as if they are being unraveled or unweaved. If one chooses launching points near these boundaries, very slight differences can give rise to very different outcomes.</p><p>Substantial differences:</p><p>• The central parts of the dense regions of NewtonRaphson’s method are “compact” and homogeneous, that is, all their points lead to the equilibrium positions of a particular set and therefore show the deterministic aspect of these areas for the particular numerical method. On the contrary, the corresponding regions obtained by means of modified Broyden’s method are less extended and less cohesive than the previous ones.</p><p>• The initial approximations of plane (x, y) which do not lead to a target in the Newton-Raphson method, are very few. On the contrary, in the modified Broyden’s method, a great number of non-convergent initial approximations exists. Most of them are located at a relatively great distance from the primaries and are distributed in some extended areas of the diagram.</p><p>Newton-Raphson’s method “strikes” the target very fast, after a very few iterations. On the contrary, Broyden’s method needs many more iterations to achieve</p><p>convergence. This is depicted in the bar charts of <xref ref-type="fig" rid="fig3">Figure 3</xref> as well as in the <xref ref-type="table" rid="table1">Table 1</xref> where we give the results obtained for the three considered cases with λ = 2, 10 and 12.</p></sec><sec id="s5_2"><title>5.2. Sub-Regions of High or Low Speed of Convergence</title><p>We have extended our investigation by studying the way with which the attracting domain of an equilibrium point or set is resolved into smaller regions, according to the number of the iterations needed to reach the equilibrium</p><p>positions of this particular set. As we have already stressed in the previous section, the number of the required iterations in order to achieve the location of an equilibrium position depends on the predetermined accuracy. In order to provide clear and instructive pictures, we have classified the points of the attracting regions of each equilibrium set and for both methods used in this work, in four class intervals 1 - 10 (very fast convergence), 11 - 20 (fast convergence), 21 - 40 (moderate convergence) and &gt;40 (slow or very slow convergence) for the number of iterations and accuracy of 10<sup>−8</sup>.</p><p>The general observations that concern all sets of points and both methods can be summarized as follows:</p><p>• The subset of the “launching” points of (x, y) plane corresponding to the class interval 1 - 10 iterations for any equilibrium position of any equilibrium set, consists of a small region which occupies the central part</p><p>of the attracting domain around each equilibrium position of this particular set and of some dispersed points, which appear near these areas or between the dense regions of other equilibria or sets. Regarding Modified Broyden’s method this class appears as a sparse cluster of points that are scattered among the points of the second class.</p><p>• The subset of the points corresponding to the class interval 11 - 20 iterations of each set consists of regions or points which complement the central regions of the first class interval and of a large number of isolated points in the attracting area of this particular equilibrium point or set. These points are spread in a widely extended area on (x, y) plane.</p><p>• The points corresponding to the class interval 21 - 40 iterations of each set evolve in a similar way as in the previous class.</p><table-wrap-group id="1"><label><xref ref-type="table" rid="table1">Table 1</xref></label><caption><title> Number of converging points per class interval.(a) λ = 2; (b) λ = 10; (c) λ = 12</title></caption></table-wrap-group><p>• Regarding class interval &gt; 40 iterations, it merely consists of dispersed points lying either on the boundaries of the dense regions of the previously mentioned class interval, or between the dense regions of the other equilibrium points or sets. Naturally, a decreasing density is observed as the number of iterations increases. &#160;</p></sec></sec><sec id="s6"><title>6. Conclusion</title><p>We have investigated the attracting areas for the equilibria of a charged particle in a magnetic binary system using both Newton’s and Modified Broyden’s methods. In this system the number of equilibria depends on the values of parameter λ and the attracting domain of each dynamically equivalent set of equilibria consists of a dense sub-domain in the close neighbourhood of each equilibrium point of this set and of dispersed points distributed at the boundaries of the former domain of the same or other equilibrium sets. These boundaries are not clear and in some cases present a fractal structure. The application of the two methods reveals similarities and differences that exist between them. The dense part of an attracting region calculated with Newton’s method is more “compact” than the respective one calculated with Modified Broyden’s method. Another difference concerns the dispersed points. When these points are calculated with Newton’s method they are distributed in an extended area of the diagram and mainly on the boundaries of the “compact” regions. In Modified Broyden’s method these points are very few and in many cases form small point clusters beyond or near the central domain. We also observe that Newton’s method “strikes” the final target very fast. For the vast majority of the initial approximations, the method needs only 1 - 10 iterations. On the contrary, Modified Broyden’s method needs often many more iterations to achieve convergence. Figures 3-7 and <xref ref-type="table" rid="table1">Table 1</xref> justify our remarks. The presented material confirms that Newton’s method is more efficient than Modified Broyden’s one (for this type problem) as regards all the indices examined, such as the speed of convergence and the total number of launching points of the xy-plane that lead to the desired final destination.</p></sec><sec id="s7"><title>REFERENCES</title></sec></body><back><ref-list><title>References</title><ref id="scirp.20085-ref1"><label>1</label><mixed-citation publication-type="other" xlink:type="simple">T. J. 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