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Control no lineal de un aerodeslizador no holonómico con acciones de control limitadas
Nonlinear control of an underactuated nonholonomic hovercraft with limited control inputs
Dictino Chaos
Autor para correspondencia
dchaos@dia.uned.es

Autor para correspondencia.
, David Moreno-Salinas, Rocío Muñoz, Joaquín Aranda
Departamento de Informática y Automática, Escuela Técnica Superior de Ingeniería Informática, UNED, calle Juan del Rosal 16, 28040, Madrid
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        "resumen" => "<p id="spar0005" class="elsevierStyleSimplePara elsevierViewall">Este art&#237;culo aborda el problema de seguimiento de trayectoria de un aerodeslizador subactuado&#46; Esta clase de sistemas es dif&#237;cil de controlar debido a que su movimiento est&#225; sujeto a una restricci&#243;n no holon&#243;mica de segundo orden&#46; La resoluci&#243;n de este complejo problema requiere la descomposici&#243;n de la din&#225;mica del sistema en dos subsistemas &#40;posici&#243;n y orientaci&#243;n&#41; para los que se dise&#241;a una ley de control basada en dos controladores no lineales en cascada&#46; El lazo externo de control calcula los valores de la fuerzas en el sistema inercial Fx y Fy que deber&#237;an aplicarse al aerodeslizador para seguir la trayectoria deseada&#46; A partir de estas fuerzas se determina la referencia para la orientaci&#243;n&#44; <span class="elsevierStyleItalic">&#968;</span><span class="elsevierStyleInf">c</span>&#44; entrada del lazo interno&#46; Por su parte&#44; el lazo interno intenta controlar la orientaci&#243;n para de esta forma seguir las referencia <span class="elsevierStyleItalic">&#968;</span><span class="elsevierStyleInf">c</span> del lazo externo&#46; Ambos controladores se han dise&#241;ado teniendo en cuenta la saturaci&#243;n de los actuadores&#46; En particular&#44; el principal resultado de este art&#237;culo muestra que en los casos donde la trayectoria est&#225; adecuadamente definida&#44; es posible ajustar los par&#225;metros del controlador para evitar la saturaci&#243;n de los actuadores&#46; Este trabajo demuestra de forma te&#243;rica la estabilidad asint&#243;tica global del error de seguimiento bajo la acci&#243;n del controlador propuesto&#46; Adem&#225;s&#44; mediante simulaciones&#44; se analiza el comportamiento del sistema y el significado pr&#225;ctico de los resultados te&#243;ricos&#46;</p>"
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        "resumen" => "<p id="spar0010" class="elsevierStyleSimplePara elsevierViewall">This paper deals with the interesting problem of trajectory tracking of an underactuated hovercraf&#46; This system is difficult to control because it exhibits second order nonholonomic restrictions on its movement&#46; In order to solve the control problem the dynamics of the system is discomposed in two subsystems &#40;one for position and another for orientation&#41; and a nonlinear control law based on two nonlinear cascaded controllers is designed&#46; On one hand the outer&#44; loop computes the forces that are necessary to track the spatial trajectory <span class="elsevierStyleItalic">F</span><span class="elsevierStyleInf"><span class="elsevierStyleItalic">x</span></span> and <span class="elsevierStyleItalic">F</span><span class="elsevierStyleInf"><span class="elsevierStyleItalic">y</span></span> in the inertial frame&#46; Based on this forces&#44; the reference for the orientation <span class="elsevierStyleItalic">&#968;</span><span class="elsevierStyleInf">c</span> is computed and it is feedback to the inner loop&#46; On the other hand&#44; the inner loop tries to converge the orientation to the reference <span class="elsevierStyleItalic">&#968;</span><span class="elsevierStyleInf"><span class="elsevierStyleItalic">c</span></span> given by the outer loop&#46; Both controllers are designed taking into account saturation of the actuators&#46; In fact the main result of this paper shows that if the reference trajectory is given properly it is possible to avoid saturation of the actuators&#46; With adequate selection&#44; global asymptotic stability of the tracking error under the proposed control law is theoretically demonstrated&#46; In addition simulations are made in order to analyze the performance of the control law and the practical meaning of the theoretical results&#46;</p>"
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