<?xml version="1.0" encoding="ISO-8859-1"?><article xmlns:mml="http://www.w3.org/1998/Math/MathML" xmlns:xlink="http://www.w3.org/1999/xlink" xmlns:xsi="http://www.w3.org/2001/XMLSchema-instance">
<front>
<journal-meta>
<journal-id>1909-3667</journal-id>
<journal-title><![CDATA[Tecciencia]]></journal-title>
<abbrev-journal-title><![CDATA[Tecciencia]]></abbrev-journal-title>
<issn>1909-3667</issn>
<publisher>
<publisher-name><![CDATA[Universidad ECCI]]></publisher-name>
</publisher>
</journal-meta>
<article-meta>
<article-id>S1909-36672014000100008</article-id>
<article-id pub-id-type="doi">10.18180/tecciencia.2014.16.7</article-id>
<title-group>
<article-title xml:lang="en"><![CDATA[Identification and multivariable control in state space of a permanent magnet synchronous generator]]></article-title>
<article-title xml:lang="es"><![CDATA[Identificación y control multivariable en el estado espacio de un generador síncrono de imanes permanentes]]></article-title>
</title-group>
<contrib-group>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Albarracín Ávila]]></surname>
<given-names><![CDATA[Danna Lisseth]]></given-names>
</name>
<xref ref-type="aff" rid="A01"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Padilla Buritica]]></surname>
<given-names><![CDATA[Jorge Iván]]></given-names>
</name>
<xref ref-type="aff" rid="A02"/>
</contrib>
<contrib contrib-type="author">
<name>
<surname><![CDATA[Giraldo Suárez]]></surname>
<given-names><![CDATA[Eduardo]]></given-names>
</name>
<xref ref-type="aff" rid="A03"/>
</contrib>
</contrib-group>
<aff id="A01">
<institution><![CDATA[,Universidad Tecnológica de Pereira  ]]></institution>
<addr-line><![CDATA[Pereira ]]></addr-line>
<country>Colombia</country>
</aff>
<aff id="A02">
<institution><![CDATA[,Escuela Colombiana de carreras industriales  ]]></institution>
<addr-line><![CDATA[Bogotá ]]></addr-line>
<country>Colombia</country>
</aff>
<aff id="A03">
<institution><![CDATA[,Universidad Tecnológica de Pereira  ]]></institution>
<addr-line><![CDATA[Pereira ]]></addr-line>
<country>Colombia</country>
</aff>
<pub-date pub-type="pub">
<day>00</day>
<month>01</month>
<year>2014</year>
</pub-date>
<pub-date pub-type="epub">
<day>00</day>
<month>01</month>
<year>2014</year>
</pub-date>
<volume>9</volume>
<numero>16</numero>
<fpage>66</fpage>
<lpage>72</lpage>
<copyright-statement/>
<copyright-year/>
<self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_arttext&amp;pid=S1909-36672014000100008&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_abstract&amp;pid=S1909-36672014000100008&amp;lng=en&amp;nrm=iso"></self-uri><self-uri xlink:href="http://www.scielo.org.co/scielo.php?script=sci_pdf&amp;pid=S1909-36672014000100008&amp;lng=en&amp;nrm=iso"></self-uri><abstract abstract-type="short" xml:lang="en"><p><![CDATA[In this paper, a scheme for online identification of multivariable systems (MIMO) and a linear state feedback control is considered. The identification algorithm takes into account the input/output behavior in order to obtain a linear state spaces model that describes adequately the system in discrete time. This representation is obtained by using an online identification method such as the projection algorithm. An optimal linear quadratic regulator is applied in discrete time, where the obtained state feedback control law minimizes the quadratic cost function to calculate the optimal gain matrix. The proposed methodology for identification and multivariable control is applied an evaluated in a wind turbine with a Permanent Magnet Synchronous Generator (PMSG).]]></p></abstract>
<abstract abstract-type="short" xml:lang="es"><p><![CDATA[En este trabajo, se considera un esquema de identificación en línea de sistemas multivariable (MIMO) y un control lineal por realimentación de estados. El algoritmo de identificación considera el comportamiento de entrada/salida con el fin de obtener un modelo de espacio de estados lineal que describe adecuadamente el sistema en tiempo discreto. Esta representación se obtiene mediante el uso de un método de identificación en línea, tales como el algoritmo de proyección. Un regulador lineal cuadrático óptimo se aplica en tiempo discreto, donde la ley de control por realimentación de estados obtenida, minimiza la función de costo cuadrática para calcular la matriz de ganancia óptima. Se aplica la metodología propuesta para la identificación y el control multivariable, en una turbina eólica con un generador síncrono de imanes permanentes (PMSG).]]></p></abstract>
<kwd-group>
<kwd lng="en"><![CDATA[Control]]></kwd>
<kwd lng="en"><![CDATA[identification]]></kwd>
<kwd lng="en"><![CDATA[optimal gain]]></kwd>
<kwd lng="en"><![CDATA[multivariable]]></kwd>
<kwd lng="en"><![CDATA[linear model]]></kwd>
<kwd lng="en"><![CDATA[feedback]]></kwd>
<kwd lng="es"><![CDATA[Control]]></kwd>
<kwd lng="es"><![CDATA[identificación]]></kwd>
<kwd lng="es"><![CDATA[ganancia óptima]]></kwd>
<kwd lng="es"><![CDATA[multivariable]]></kwd>
<kwd lng="es"><![CDATA[modelo lineal]]></kwd>
<kwd lng="es"><![CDATA[retroalimentación]]></kwd>
</kwd-group>
</article-meta>
</front><body><![CDATA[  <font size="2" face="Verdana">     <p>DOI: <a href="http://dx.doi.org/10.18180/tecciencia.2014.16.7" target="_blank">http://dx.doi.org/10.18180/tecciencia.2014.16.7</a>.</p>      <p align="center"><font size="4"><b>Identification and multivariable control in state space of a permanent magnet synchronous generator </b></font></p>      <p align="center"><font size="3"><b>Identificaci&oacute;n y control multivariable en el estado espacio de un generador s&iacute;ncrono de imanes permanentes </b></font></p>      <p align="center">Danna Lisseth Albarrac&iacute;n &Aacute;vila<sup>1</sup>, Jorge Iv&aacute;n Padilla Buritica<sup>2</sup>, Eduardo Giraldo Su&aacute;rez<sup>3</sup></p>      <p><sup>1</sup><i> Universidad Tecnol&oacute;gica de Pereira, Pereira, Colombia, </i><A href="mailto:egiraldos@utp.edu.co"> <i>egiraldos@utp.edu.co</i></A>.    <br>  <sup>2</sup><i> Escuela Colombiana de carreras industriales, Bogot&aacute;, Colombia, </i><A href="mailto:jpadillab@ecci.edu.co"> <i>jpadillab@ecci.edu.co</i></A>.    <br>  <sup>3</sup><i> Universidad Tecnol&oacute;gica de Pereira, Pereira, Colombia, </i><A href="mailto:carlos.pena@usa.edu.co"> <i>carlos.pena@usa.edu.co</i></A>.</p>      <p>How to cite: Albarracin Avila, D., et al, Identification and multivariable control in state space of a permanent magnet synchronous generator, TECCIENCIA, Vol. 9 No. 16., 66-72, 2014, DOI: <a href="http://dx.doi.org/10.18180/tecciencia.2014.16.7" target="_blank">http://dx.doi.org/10.18180/tecciencia.2014.16.7</a>.</p>      <p><i>Received: 09 April 2014     Accepted: 28 May 2014               Published: 30 July 2014 </i></p>  <hr>     ]]></body>
<body><![CDATA[<p><font size="3"><b>Abstract </b></font></p>      <p>In this paper, a scheme for online identification of multivariable systems (MIMO) and a linear state feedback control is considered. The identification algorithm takes into account the input/output behavior in order to obtain a linear state spaces model that describes adequately the system in discrete time. This representation is obtained by using an online identification method such as the projection algorithm. An optimal linear quadratic regulator is applied in discrete time, where the obtained state feedback control law minimizes the quadratic cost function to calculate the optimal gain matrix. The proposed methodology for identification and multivariable control is applied an evaluated in a wind turbine with a Permanent Magnet Synchronous Generator (PMSG).</p>      <p><b><i>Keywords</i>: </b>Control, identification, optimal gain, multivariable, linear model, feedback.</p>  <hr>     <p><font size="3"><b>Resumen </b></font></p>      <p>En este trabajo, se considera un esquema de identificaci&oacute;n en l&iacute;nea de sistemas multivariable (MIMO) y un control lineal por realimentaci&oacute;n de estados. El algoritmo de identificaci&oacute;n considera el comportamiento de entrada/salida con el fin de obtener un modelo de espacio de estados lineal que describe adecuadamente el sistema en tiempo discreto. Esta representaci&oacute;n se obtiene mediante el uso de un m&eacute;todo de identificaci&oacute;n en l&iacute;nea, tales como el algoritmo de proyecci&oacute;n. Un regulador lineal cuadr&aacute;tico &oacute;ptimo se aplica en tiempo discreto, donde la ley de control por realimentaci&oacute;n de estados obtenida, minimiza la funci&oacute;n de costo cuadr&aacute;tica para calcular la matriz de ganancia &oacute;ptima. Se aplica la metodolog&iacute;a propuesta para la identificaci&oacute;n y el control multivariable, en una turbina e&oacute;lica con un generador s&iacute;ncrono de imanes permanentes (PMSG).</p>      <p><b><i>Palabras clave</i>: </b>Control, identificaci&oacute;n, ganancia &oacute;ptima, multivariable, modelo lineal, retroalimentaci&oacute;n.</p>  <hr>     <p><font size="3"><b>1. Introduction </b></font></p>      <p>With its abundant, inexhaustible potential, its increasingly competitive cost, and environmental advantage, wind energy is one of the best technologies available today to provide a sustainable supply to the world development. Now, the wind energy is an important sustainable energy resource and with this creates the need for increased power production from the wind in adverse conditions, when the wind turbine generator system is coupled to a power system &#91;1&#93;. Recent studies are focused on investigating the system behavior with internal disturbances and variable wind speed that affects the system &#91;2&#93;, and other investigations proposing new techniques about the system identification and the control systems in the maximum extracting of energy of the whole system &#91;3&#93;.</p>      <p>The systems that use the subspace identification methods (SIMs) have become quite popular in recent years. The SIMs objective is to estimate the state variables or the extended observability matrix directly from the input and output data &#91;4&#93;. The most influential methods are CVA (Canonical Variate Analysis &#91;5&#93;), MOESP (Multivariable Output Error State Space &#91;6&#93;) and N4SID (Numerical Subspace State-Space System Identification &#91;6&#93;). But exist other methods that used the Darma model to estimate the plant parameters in each time with past inputs/outputs values &#91;7&#93;.</p>      <p>Linear system identified with SIMs, are suitable for the application of state space controllers. The investigations around the discrete linear quadratic regulator (DLQR) control are oriented to the convergence of control strategies for discrete-time linear systems in state space based on dynamic programming (DP) and the classical DLQR. The performance of the DP algorithms is evaluated for changes in control targets that are mapped in <i>Q</i> and <i>R</i> weighting matrices &#91;8&#93;.</p>      ]]></body>
<body><![CDATA[<p>This paper is focused on the mathematical model of a wind generator where the behavior of its variables will be examined. So, a nonlinear multivariable system identification scheme is proposed, based on a linear state space representation to improve the performance of the wind turbine. Lastly, the system's closed loop response is evaluated with the optimal adaptive controllers and the parameters stated by using the identification schemes.</p>      <p><font size="3"><b>2. Model description</b></font></p>      <p>The model of a wind turbine with Permanent Magnet Synchronous Generator (PMSG) is constructed from a number of sub models of the turbine, drive train, synchronous generator and rotor side converter. A general structure of the model is shown in <a href="#f1">Figure 1</a> &#91;9,13&#93;.</p>       <p align="center"><a name="f1"><img src="img/revistas/tecci/v9n16/v9n16a08f1.jpg"></a>.</p>       <p><i>2.1 Turbine Model</i></p>      <p>The main purpose of the wind turbine is to obtain energy from the wind and transform it into electrical energy &#91;9&#93;. The power extracted from the wind is described by (1)</p>      <p align="center"><a name="ec1"><img src="img/revistas/tecci/v9n16/v9n16a08ec1.jpg"></a>.</p>      <p>Where, <i>&rho;</i> is the air density, <i>Ra</i> is the radius of the area covered by the wind, <i>v</i> is the wind speed and <i>Cp</i> is the performance coefficient in function of the tip speed.</p>      <p>The torque developed from the wind and the <i>Cp</i> approximation is presented in (2) and (3).</p>      <p align="center"><a name="ec2"><img src="img/revistas/tecci/v9n16/v9n16a08ec2.jpg"></a></p>      ]]></body>
<body><![CDATA[<p align="center"><a name="ec3"><img src="img/revistas/tecci/v9n16/v9n16a08ec3.jpg"></a></p>      <p>A second order approximation, of the coefficient <i>Cp</i>, is calculated employing the least square technique.</p>      <p align="center"><a name="ec4"><img src="img/revistas/tecci/v9n16/v9n16a08ec4.jpg"></a></p>       <p>The tip speed is (5)</p>      <p align="center"><a name="ec5"><img src="img/revistas/tecci/v9n16/v9n16a08ec5.jpg"></a></p>      <p>The speed in the generator side is (6), where <i>G </i>is the multiplier coefficient of the gear box.</p>      <p align="center"><a name="ec6"><img src="img/revistas/tecci/v9n16/v9n16a08ec6.jpg"></a></p>      <p>The torque in the generator side is:</p>      <p align="center"><a name="ec7"><img src="img/revistas/tecci/v9n16/v9n16a08ec7.jpg"></a></p>      <p>Replacing <a href="#ec5">equations (5</a>) and (<a href="#ec4">4</a>) in (<a href="#ec2">2</a>), the torque in the generator side is represented by the approximation (8)</p>      ]]></body>
<body><![CDATA[<p align="center"><a name="ec8"><img src="img/revistas/tecci/v9n16/v9n16a08ec8.jpg"></a>.</p>      <p><font size="3"><b>3. Drive train system </b></font></p>      <p> Las figuras y tablas deben aparecer lo m&aacute;s cerca posible del lugar de su primera cita, por ejemplo, La <a href="#f1">figura. 1</a>, en el texto. Las figuras se numerar&aacute;n con n&uacute;meros ar&aacute;bigos, con la leyenda centrada debajo de la figura, en negrita.    <br>  The drive train of PMSG consists of five parts, namely, rotor, low speed shaft, gearbox, high-speed shaft and generator. When the study focuses on the interaction between wind farms and AC grids, the drive train can be treated as one-lumped mass model for the sake of time efficiency and acceptable precision. So, the drive train takes the form of the latter one in the paper in which the parameters have been referred to the generator side &#91;10&#93;.</p>      <p align="center"><a name="ec9"><img src="img/revistas/tecci/v9n16/v9n16a08ec9.jpg"></a></p>      <p><i>&omega;</i><sub><i>H</i></sub> the angular velocity, <i>T</i><sub><i>e</i></sub> electrical torque, <i>T</i><sub><i>m</i></sub> mechanical torque,<i> Bm </i>is the rotating damping, <i>J</i><sub><i>H</i></sub> is the inertia constant and <i>&theta;</i> the angular position angle.</p>       <p><font size="3"><b>4. Pmsg modeling </b></font></p>      <p> The PMSG has been considered as a system which makes possible to produce electricity from the mechanical energy obtained from the wind.</p>      <p>The dynamic model of the PMSG is derived from the two-phase synchronous reference frame, which the <i>q-</i>axis is 90&deg; ahead of the <i>d-</i>axis with respect to the direction of rotation &#91;1&#93;. By the application of the Park transform and presenting the model as a generator with negative currents; the system is expressed in the coordinates of the rotor which makes the design of the driver simpler because their signals are treated as direct current and that reduces the model to two axes.</p>      <p>The system is modeled with the set of <a href="#ec10">equations (10)</a> to (<a href="#ec13">13</a>) where <i>idq</i> and <i>udq</i> represent currents and voltages of the stator in the axis <i>q</i> and <i>d </i>respectively &#91;9&#93;.</p>      ]]></body>
<body><![CDATA[<p align="center"><a name="ec10"><img src="img/revistas/tecci/v9n16/v9n16a08ec10.jpg"></a></p>      <p align="center"><a name="ec11"><img src="img/revistas/tecci/v9n16/v9n16a08ec11.jpg"></a></p>      <p align="center"><a name="ec12"><img src="img/revistas/tecci/v9n16/v9n16a08ec12.jpg"></a></p>      <p align="center"><a name="ec13"><img src="img/revistas/tecci/v9n16/v9n16a08ec13.jpg"></a></p>         <p><i>n</i><sub><i>p</i></sub> is the number of pole pairs, <i>R</i> is the stator resistance, <i>L</i><sub><i>s</i></sub> is the inductance of the stator, <i>&phi;m</i> the magnetization flow in the rotor.</p>      <p>The system in state space is represented in (14) to (15) to feed a <i>RL</i> load, <i>L</i> is the inductance of the load, <i>R</i><sub><i>L</i></sub> the variable resistance of the load, <i>J</i><sub><i>H</i></sub> inertia coefficient at the side of the generator. The state vector is <i>x</i>=&#91;<i>x</i><sub>1</sub>,<i>x</i><sub>2</sub>,<i>x</i><sub>3</sub>&#93;<sup>T</sup>=&#91;<i>i</i><sub>d</sub>,<i>i</i><sub>q</sub>,&omega;&#93;, the inputs of the system<i>u</i>=&#91;u<sub>1</sub>,u<sub>2</sub>&#93;<sup>T</sup>=&#91;<i>R</i><sub><i>L</i></sub>,<i>&nu;</i>&#93;<sup><i>T</i></sup> and the rotor speed &omega; is the output.</p>      <p align="center"><a name="ec14"><img src="img/revistas/tecci/v9n16/v9n16a08ec14.jpg"></a></p>      <p align="center"><a name="ec15"><img src="img/revistas/tecci/v9n16/v9n16a08ec15.jpg"></a></p>      <p align="center"><a name="ec16"><img src="img/revistas/tecci/v9n16/v9n16a08ec16.jpg"></a></p>      <p align="center"><a name="ec17"><img src="img/revistas/tecci/v9n16/v9n16a08ec17.jpg"></a></p>      ]]></body>
<body><![CDATA[<p>&eta; is the drive train performance coefficient.</p>      <p><font size="3"><b>5. Subspace identification method </b></font></p>      <p><i>5.1. Representation of Multivariable Systems</i></p>      <p> The representation of a multi-variable discrete system with <i>m</i> outputs and <i>r</i> inputs with <i>q</i> as delay operator can be stated in &#91;7&#93;:</p>      <p align="center"><a name="ec18"><img src="img/revistas/tecci/v9n16/v9n16a08ec18.jpg"></a></p>      <p>where <i>A</i> is given by:</p>      <p align="center"><a name="ec19"><img src="img/revistas/tecci/v9n16/v9n16a08ec19.jpg"></a></p>      <p>and <i>B</i> is given by:</p>      <p align="center"><a name="ec20"><img src="img/revistas/tecci/v9n16/v9n16a08ec20.jpg"></a></p>,     <p>wint<sub>1</sub> &ge;n<sub>2</sub>h and where <i>A</i><sub><i>i</i></sub>&isin;<img src="img/revistas/tecci/v9n16/v9n16a08img1.jpg">,<i>B</i><sub>i</sub>&isin;<img src="img/revistas/tecci/v9n16/v9n16a08img2.jpg">,the inputs <i>u</i>&isin;<img src="img/revistas/tecci/v9n16/v9n16a08img3.jpg">and the outputs <i>y</i>&isin;<img src="img/revistas/tecci/v9n16/v9n16a08img4.jpg"> as</p>       ]]></body>
<body><![CDATA[<p align="center"><a name="ec21"><img src="img/revistas/tecci/v9n16/v9n16a08ec21.jpg"></a></p>      <p>If<i>A</i><sub>o</sub> with I the identity matrix, y takes the form:</p>      <p align="center"><a name="ec22"><img src="img/revistas/tecci/v9n16/v9n16a08ec22.jpg"></a></p>      <p>where <i>A</i><sub><i>i</i></sub> and <i>B</i><sub><i>i</i></sub> are of the form:</p>      <p align="center"><a name="ec23"><img src="img/revistas/tecci/v9n16/v9n16a08ec23.jpg"></a></p>        <p><a href="#ec22">Equations (22)</a> and (<a href="#ec23">23</a>) can be expressed the output <i>y<sub><i>i</i></sub> in</i> terms of past inputs/outputs as:</p>      <p align="center"><a name="ec24"><img src="img/revistas/tecci/v9n16/v9n16a08ec24.jpg"></a></p>      <p>It appears from the above equation that the DARMA model of the <a href="#ec18">equation (18)</a> can be expressed as &#91;11&#93;:</p>      <p align="center"><a name="ec25"><img src="img/revistas/tecci/v9n16/v9n16a08ec25.jpg"></a></p>      <p>where <i>&theta;T  <sup>i</sup></i>s transposed of <i>&theta;</i>, and <i>&theta; </i>has dimension <i>(mn1+rn2) x m</i> that holds the parameters of <i>A</i><sub>i</sub> and <i>B</i><sub>i</sub>  of the form:</p>      ]]></body>
<body><![CDATA[<p align="center"><a name="ec26"><img src="img/revistas/tecci/v9n16/v9n16a08ec26.jpg"></a></p>      <p>and &Oslash;(<i>K</i>&minus;1)  is a vector of dimension <i>(mn<sub>1</sub>+rn<sub>2</sub>) x 1</i> that holds the values of past input/output</p>      <p align="center"><a name="ec27"><img src="img/revistas/tecci/v9n16/v9n16a08ec27.jpg"></a></p>      <p>An state space representation can be obtained from (22) and (27) by selecting &Oslash;(<i>K</i>&minus;1)as the state space vector, as follows:</p>      <p align="center"><a name="ec28"><img src="img/revistas/tecci/v9n16/v9n16a08ec28.jpg"></a></p>      <p>being</p>      <p align="center"><a name="ec29"><img src="img/revistas/tecci/v9n16/v9n16a08ec29.jpg"></a></p>      <p>and</p>      <p align="center"><a name="ec30"><img src="img/revistas/tecci/v9n16/v9n16a08ec30.jpg"></a></p>      <p>and</p>      ]]></body>
<body><![CDATA[<p align="center"><a name="ec31"><img src="img/revistas/tecci/v9n16/v9n16a08ec31.jpg"></a></p>      <p>The PMSG has been considered as a system which makes possible to produce electricity from the mechanical energy obtained from the wind. The PMSG has been considered as a system which makes possible to produce electricity from the mechanical energy obtained from the wind. The PMSG has been considered as a system which makes possible to produce electricity from the mechanical energy obtained from the wind. The PMSG has been considered as a system which makes possible to produce electricity from the mechanical energy obtained from the wind.</p>      <p><i>5.2. Online Estimation Schemes</i></p>      <p>The estimated parameters <img src="img/revistas/tecci/v9n16/v9n16a08te1.jpg">&#770;<sup><i>T</i></sup>(<i>K</i>) are calculated in terms of the previous matrix of the estimated parameters  <img src="img/revistas/tecci/v9n16/v9n16a08te1.jpg">&#770;<sup><i>T</i></sup>(<i>K</i>&minus;1) as follows</p>      <p align="center"><a name="ec32"><img src="img/revistas/tecci/v9n16/v9n16a08ec32.jpg"></a></p>       <p>where <img src="img/revistas/tecci/v9n16/v9n16a08te1.jpg">&#770;<sup><i>T</i></sup>(<i>K</i>) is the matrix of parameters estimated in time <i>k</i>, <i>M</i>(<i>K</i>&minus;1) denotes the algorithm gain (possibly a matrix), &Oslash;(<i>K</i>&minus;1) is a regression vector composed of past inputs/outputs, and <i>e</i> (<i>K</i>&minus;1) is the error of the form</p>      <p align="center"><a name="ec33"><img src="img/revistas/tecci/v9n16/v9n16a08ec33.jpg"></a></p>      <p>where <i>&#375;</i> (<i>K</i>) = <img src="img/revistas/tecci/v9n16/v9n16a08te1.jpg">&#770;<sup><i>T</i></sup>(<i>K</i>&minus;1 ) &Oslash; (<i>K</i>&minus;1) is given by</p>      <p align="center"><a name="ec34"><img src="img/revistas/tecci/v9n16/v9n16a08ec34.jpg"></a></p>       <p><i>5.3. Projection Algorithm</i></p>      ]]></body>
<body><![CDATA[<p>The projection algorithm raises an optimization problem where <img src="img/revistas/tecci/v9n16/v9n16a08te1.jpg">&#770;(<i>K</i>) is being minimised with the <img src="img/revistas/tecci/v9n16/v9n16a08te1.jpg">(<i>K</i>&minus;1) and <i>y</i>(<i>K</i>)  given, such that</p>      <p align="center"><a name="ec35"><img src="img/revistas/tecci/v9n16/v9n16a08ec35.jpg"></a></p>      <p>subject to</p>      <p align="center"><a name="ec36"><img src="img/revistas/tecci/v9n16/v9n16a08ec36.jpg"></a></p>      <p>The projection algorithm is given by</p>      <p align="center"><a name="ec37"><img src="img/revistas/tecci/v9n16/v9n16a08ec37.jpg"></a></p> <ol><i>Least Squares Algorithm</i>    </ol>     <p>The least squares algorithm is given by</p>      <p align="center"><a name="ec38"><img src="img/revistas/tecci/v9n16/v9n16a08ec38.jpg"></a></p>      <p><i>5.4. Discrete Linear Quadratic Regulator</i></p>      ]]></body>
<body><![CDATA[<p>The formulation of the DLQR problem in the discrete-time case is analogous to the continuous-time LQR problem. Consider the time-invariant linear system described in (28) where the vector &Oslash;(<i>K</i>&minus;1) represents the variables to be regulated &#91;11&#93;. The DLQR problem is to determine a control sequence {<i>u</i><sup>*</sup>(<i>K</i>)},<i>K</i>&ge;0, which minimizes the cost function</p>      <p align="center"><a name="ec39"><img src="img/revistas/tecci/v9n16/v9n16a08ec39.jpg"></a></p>      <p>where the weighting matrices <i>Q</i> and <i>R </i>are real symmetric and positive definite.</p>      <p>Assume that (<i>E</i>,<i>F</i>,<i>Q</i><sup>1/2</sup><i>M</i><sub>e</sub>) is reachable and observable. Then the solution to the DLQR problem is given by the linear state feedback control law</p>      <p align="center"><a name="ec40"><img src="img/revistas/tecci/v9n16/v9n16a08ec40.jpg"></a></p>      <p>where <i>P</i><sup><i>*</i></sup><sub><i>c</i></sub> is the unique, symmetric, and positive-definite solution of the (<i>discrete-time</i>) <i>algebraic Riccati equation</i>, given by</p>      <p align="center"><a name="ec41"><img src="img/revistas/tecci/v9n16/v9n16a08ec41.jpg"></a></p>      <p>As in the continuous-time case, it can be shown that the solution <i>P</i><sup><i>*</i></sup><sub><i>c</i></sub> can be determined from the eigenvectors of the <i>Hamiltonian matrix</i>, which in this case is</p>      <p align="center"><a name="ec42"><img src="img/revistas/tecci/v9n16/v9n16a08ec42.jpg"></a></p>      <p>The linear state feedback control law can be extended for reference tracking performance as follows</p>      ]]></body>
<body><![CDATA[<p align="center"><a name="ec43"><img src="img/revistas/tecci/v9n16/v9n16a08ec43.jpg"></a></p>      <p>being <i>r</i> (<i>K</i>) a reference vector and <i>K</i><sub><i>g</i></sub> a steady state matrix gain or reference gain defined by</p>      <p align="center"><a name="ec44"><img src="img/revistas/tecci/v9n16/v9n16a08ec44.jpg"></a></p>      <p>being (<i>M</i><sub>e</sub>(<i>I</i> &minus; <i>E</i>+ <i>FK</i>)<sup>#</sup> the pseudoinverse of (<i>M</i><sub>e</sub>(I&minus;<i>E</i>+<i>FK</i>)<sup>&minus;1</sup><i>F</i>).</p>      <p><font size="3"><b>6. Results</b></font></p>      <p> The proposed model of PMSG is constructed with MATLAB/Simulink using the parameters of <a href="#t1">Tables 1</a>, <a href="#t2">2</a> and <a href="#t3">3</a>.</p>      <p align="center"><a name="t1"><img src="img/revistas/tecci/v9n16/v9n16a08t1.jpg"></a></p>      <p align="center"><a name="t2"><img src="img/revistas/tecci/v9n16/v9n16a08t2.jpg"></a></p>      <p align="center"><a name="t3"><img src="img/revistas/tecci/v9n16/v9n16a08t3.jpg"></a></p>      <p>This section presents the simulated responses of the system with a variable wind speed from 5m/s to 12 m/s and a time varying load.     ]]></body>
<body><![CDATA[<br>  The open loop response of the wind turbine is shown in <a href="#f2">Figure 2</a>.</p>      <p align="center"><a name="f2"><img src="img/revistas/tecci/v9n16/v9n16a08f2.jpg"></a></p>      <p>By applying the online identification scheme, a discrete linear model of the PMSG is obtained. Estimated model is represented in state space as shown in (45)</p>      <p align="center"><a name="ec45"><img src="img/revistas/tecci/v9n16/v9n16a08ec45.jpg"></a></p>      <p>with</p>      <p align="center"><a name="ec46"><img src="img/revistas/tecci/v9n16/v9n16a08ec46.jpg"></a></p>      <p>and</p>      <p align="center"><a name="ec47"><img src="img/revistas/tecci/v9n16/v9n16a08ec47.jpg"></a></p>      <p>being</p>      <p align="center"><a name="ec48"><img src="img/revistas/tecci/v9n16/v9n16a08ec48.jpg"></a></p>        ]]></body>
<body><![CDATA[<p><a href="#f3">Figure 3</a> shown the system's regulation with the <i>DLQR control</i>: <i>K </i>as feedback gain but without <i>K</i><sub>g</sub> as reference gain, the values are the same that is previously used. Output signal has a steady state time around the 0.3s after changing the reference value, an overshoot around the 6 rad/s and an oscillatory response before reaching the steady state.</p>      <p align="center"><a name="f3"><img src="img/revistas/tecci/v9n16/v9n16a08f3.jpg"></a></p>      <p>The system's response using the <i>DLQR control</i> is shown in <a href="#f4">Figure 4</a> with <i>K</i> as feedback gain and <i>K</i><sub><i>g</i></sub> as reference gain, in <a href="#ec46">equations (46)</a> and (<a href="#ec47">47</a>), respectively. In <a href="#f4">Figure 4</a>, the system has a steady state time around the 0.5 s, an overshoot around the 0.3rad/s and the output signals follows the references.</p>      <p align="center"><a name="f4"><img src="img/revistas/tecci/v9n16/v9n16a08f4.jpg"></a></p>      <p><font size="3"><b>7. Conclusions</b></font></p>      <p> The identification methods of state variables with least squares and projection algorithms, where the observer of states is included, allows a better estimation the linear model in state space of a multivariable discrete system. With a adequate estimation of the system, control strategies can be used where the controller adapts to changes response to any disturbance reference, at each instant time.</p>      <p>The work developed shows that a satisfactory performance of control algorithms depends of the performance of identification algorithms. The steady state time and overshoot of output signal, can be changed depending of the performance of the control algorithms or non-following reference output signal (steady-state error).</p>      <p><font size="3"><b>Acknowledgment</b></font></p>      <p> This paper was developed under the research project "Identificaci&oacute;n de sistemas multivariables aplicada a generadores e&oacute;licos" funded by the Universidad Tecnol&oacute;gica de Pereira with code "6-14-1", and the MSc. thesis "Control &oacute;ptimo de un sistema multi-variable aplicado a un generador e&oacute;lico conectado a un sistema de potencia" approved by the "Convocatoria para financiar proyectos de grado de estudiantes de pregrado y posgrado a&ntilde;o 2103" funded by the Universidad Tecnol&oacute;gica de Pereira with code "E6-14-6".</p>  <hr>     <p><font size="3"><b>References</b></font></p>      ]]></body>
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