WO2008046942A1 - Closed-loop identification of wind turbines - Google Patents

Closed-loop identification of wind turbines Download PDF

Info

Publication number
WO2008046942A1
WO2008046942A1 PCT/ES2007/000584 ES2007000584W WO2008046942A1 WO 2008046942 A1 WO2008046942 A1 WO 2008046942A1 ES 2007000584 W ES2007000584 W ES 2007000584W WO 2008046942 A1 WO2008046942 A1 WO 2008046942A1
Authority
WO
WIPO (PCT)
Prior art keywords
identification
models
wind turbine
closed loop
input
Prior art date
Application number
PCT/ES2007/000584
Other languages
Spanish (es)
French (fr)
Inventor
Javier SANZ RODRÍGUEZ
Mikel Lasa Morán
Miguel Iribas Latour
Ioan-Doré LANDAU
Original Assignee
Fundación Cener-Ciemat
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Fundación Cener-Ciemat filed Critical Fundación Cener-Ciemat
Publication of WO2008046942A1 publication Critical patent/WO2008046942A1/en

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B17/00Systems involving the use of models or simulators of said systems
    • G05B17/02Systems involving the use of models or simulators of said systems electric
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/04Automatic control; Regulation
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/04Automatic control; Regulation
    • F03D7/042Automatic control; Regulation by means of an electrical or electronic controller
    • F03D7/043Automatic control; Regulation by means of an electrical or electronic controller characterised by the type of control logic
    • F03D7/045Automatic control; Regulation by means of an electrical or electronic controller characterised by the type of control logic with model-based controls
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03DWIND MOTORS
    • F03D7/00Controlling wind motors 
    • F03D7/02Controlling wind motors  the wind motors having rotation axis substantially parallel to the air flow entering the rotor
    • F03D7/04Automatic control; Regulation
    • F03D7/042Automatic control; Regulation by means of an electrical or electronic controller
    • F03D7/043Automatic control; Regulation by means of an electrical or electronic controller characterised by the type of control logic
    • F03D7/046Automatic control; Regulation by means of an electrical or electronic controller characterised by the type of control logic with learning or adaptive control, e.g. self-tuning, fuzzy logic or neural network
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B13/00Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion
    • G05B13/02Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric
    • G05B13/04Adaptive control systems, i.e. systems automatically adjusting themselves to have a performance which is optimum according to some preassigned criterion electric involving the use of models or simulators
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05BCONTROL OR REGULATING SYSTEMS IN GENERAL; FUNCTIONAL ELEMENTS OF SUCH SYSTEMS; MONITORING OR TESTING ARRANGEMENTS FOR SUCH SYSTEMS OR ELEMENTS
    • G05B23/00Testing or monitoring of control systems or parts thereof
    • G05B23/02Electric testing or monitoring
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05BINDEXING SCHEME RELATING TO WIND, SPRING, WEIGHT, INERTIA OR LIKE MOTORS, TO MACHINES OR ENGINES FOR LIQUIDS COVERED BY SUBCLASSES F03B, F03D AND F03G
    • F05B2260/00Function
    • F05B2260/84Modelling or simulation
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02EREDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00Energy generation through renewable energy sources
    • Y02E10/70Wind energy
    • Y02E10/72Wind turbines with rotation axis in wind direction

Definitions

  • the present invention is related to the functional control of wind turbines, proposing a closed loop identification system for said application.
  • a wind turbine is a very complex mechanism, which includes a large number of mechanical elements, actuators, aerodynamic elements, etc.
  • a wind turbine is an extremely complex mechanism to analyze independently, which makes it extremely complex to correctly adjust the entire number of parameters that, together with the dynamics equations, describe the behavior of the wind turbine.
  • This method basically has two limitations or contraindications.
  • the first of the limitations is that it is not advisable to make this type of identification in open loop when the integrity of the machine can be compromised by operating in said mode.
  • the second of the limitations comes from the fact of not having access to the power source that governs the behavior of the machine. In the case of a wind turbine, we are therefore faced with two limitations that open loop identification techniques present.
  • Open loop identification is a technique known and widely used in the field of control and other scientific or financial areas.
  • the concept of identification in the field of control refers to a method for experimentally obtaining input-output models of a mechanism or machine.
  • the concept of open loop refers in turn to the fact that the system is developed without the control of the application mechanism or machine being active, which makes the system operate freely.
  • This open loop identification technique is developed experimentally, based on a specific configuration in relation to the system for which the application is intended.
  • the conventional controller design process is developed using linear models obtained from non-linear simulators.
  • the protocols and linearization algorithms are diverse, but they have in common that they are numerical methods and that they are based exclusively on the theoretical equations that describe the behavior of a wind turbine.
  • This protocol consists in applying a differential impulse to the different inputs to the non-linear models. These can be wind speed, pitch angle and generator torque, etc. After these small disturbances, the wind turbine is allowed to evolve freely.
  • the derivatives of all the states defined by the non-linear simulator are estimated and from these values that are obtained, linear models of the machine to be controlled are determined, with which the controllers are designed and then implemented in real machines .
  • closed loop refers to the fact that the control loops that automatically govern the behavior of a mechanism, are active during the normal operation of the machine.
  • a system of identification of closed-loop wind turbines is proposed, by means of which linear models that accurately represent the dynamic behavior of the application wind turbine can be obtained, such models being used for various purposes, such as controller design, use as part of a control algorithm, parameter identification, component analysis, etc.
  • the system is based on the development of a process that is carried out through software, through which a series of steps are performed, obtaining and storing data, which are subsequently analyzed and treated in order to obtain models of input and output that can be subsequently used for any of the functions indicated above.
  • Wind-related Wind speed, at any height from the ground or at any distance from the wind turbine, whether measured or inferred.
  • Generator torque real or demanded, torque in the generator air gap
  • generator power real or demanded
  • active power real or demanded
  • reactive power real or demanded
  • currents and voltages of each of the lines of the three-phase system real or demanded, voltages and currents dyq, real or demanded, of the generator control system, etc.
  • Pitch angle real or demanded
  • pitch speed real or demanded
  • pitch acceleration real or demanded
  • powers voltages and currents
  • Yaw angle real or demanded
  • yaw speed real or demanded
  • yaw acceleration real or demanded
  • powers voltages and currents, real or demanded of the yaw motor.
  • Pressures flows, positions, speeds and accelerations of the actuator, in case of being hydraulic, etc.
  • Speed of the generator speed of the rotor on the high side, speed of the rotor on the low side, real and demanded active power to the generator, real and demanded reactive power to the generator, actual and demanded currents and voltages of each of the lines of the three-phase system, actual and demanded voltages and currents dyq of the generator control system, deformations, positions, speeds, accelerations, linear and angular, forces and moments in the bushing, along the power train, along each of the blades, along the tower, along the nacelle, etc.
  • the process includes an experimentation protocol, data collection, identification routines, and obtaining linear models for the desired application.
  • the experimentation protocol is developed during the normal operation of the wind turbine, with the control of the same asset.
  • This control consists in the introduction of a reference signal as the desired value for the variable to be controlled.
  • the signal to be controlled, the output is fed back to compare it with the reference signal.
  • This difference called error, feeds the controller that will be responsible for applying a signal that will cause the output signal to approximate its reference value by means of the actuator, thus trying to reject external and uncontrollable disturbances to the system such as bursts of wind etc.
  • the closed loop experimentation protocol for the identification of wind turbines is carried out by introducing a signal that can be added to the reference signal of the control loop or can be added to the value that the controller have calculated. Data collection and storage should be done by software, and then analyzed using identification routines.
  • the identification routines must consist of a copy of the controller and an adjustable model of the closed loop input / output model, of any combination of the input and output variables mentioned above.
  • the corresponding output of the real wind turbine is compared with the closed loop output predicted by the identification algorithm.
  • the error is processed by another algorithm, which will vary the values of the parameters in the appropriate way, in order to minimize the difference between the actual measurement of the wind turbine output variable and the output variable predicted by the identification algorithm.
  • the model Once the model is obtained, it can be validated by statistical, frequency and temporal methods. If these validation conditions are met, the models are given as correct and can then be used for all the exposed activities.
  • Figure 1 shows a block diagram of the development process of the system of the invention.
  • Figure 2 is a diagram of the application of the excitation signal in the system experimentation protocol, according to an embodiment.
  • Figure 3 is a diagram of the application of the excitation signal in the experimentation protocol, according to another embodiment.
  • the object of the invention relates to a closed loop wind turbine identification system, which aims to obtain linear models that accurately represent the dynamic behavior of the application wind turbine, to design the algorithms that govern the behavior of the wind turbine in the actual operation of it.
  • the system consists of the realization of a process of generation, storage and analysis of data, by means of a sequence like the one represented in figure 1, which includes an experimentation protocol (1), a data collection (2), routines of identification (3), the obtaining (4) of linear input-output models, and the application (5) of the linear models identified for the design and implementation of wind turbine controllers.
  • experimentation protocol (1) is developed as follows:
  • Said excitation signal (9) must have a high frequency content, particularly between 0 and 1000 Hz, as well as a determined and limited length depending on the application wind turbine ( ⁇ ), which excitation signal (9) can be applied at the input of the reference signal (7), as shown in figure 2, or in an intermediate part with respect to one or more of the actuators that govern the behavior of the wind turbine (6), as shown in figure 3.
  • the experiment can be repeated as many times as desired, and the procedure can be applied to all control loops that are active in the wind turbine or simulator (6), with the possibility of measuring all the appropriate variables for Get the models you want.
  • the identification routines (3) of the process are developed by submitting the data obtained to conventional parameter identification algorithms, so that these identification routines (3) are intended to find the relationship between temporary collections of data, the results being in these identification routines (3), linear empirical models are obtained.
  • the result of applying the experimentation protocol (1), as well as the data collection (2) and their subsequent treatment with the identification routines (3), are linear models that They describe the behavior of the system, so that once (4) these models are obtained, they can be applied (5) for activities such as: component design, start-up of wind turbines, certification, adaptive control, predictive control, maintenance of control, control tuning, dynamic operation monitoring, etc.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • General Physics & Mathematics (AREA)
  • Combustion & Propulsion (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Software Systems (AREA)
  • Evolutionary Computation (AREA)
  • Artificial Intelligence (AREA)
  • Health & Medical Sciences (AREA)
  • Computer Vision & Pattern Recognition (AREA)
  • Medical Informatics (AREA)
  • Mathematical Physics (AREA)
  • Fuzzy Systems (AREA)
  • Wind Motors (AREA)
  • Control Of Eletrric Generators (AREA)

Abstract

The invention relates to the closed-loop identification of wind turbines, involving a process including an experimentation protocol (1), data collection (2), identification routines (3), acquisition (4) of linear input/output models and application (5) of said linear models to the functions to be controlled. The experimentation protocol (1) is performed with the wind turbine in normal operation, by introducing a reference signal with the algorithm of the function to be controlled and returning the output from said function to the input while an excitation signal is being applied with the control algorithm.

Description

IDENTIFICACIÓN DE AEROGENERADORES EN LAZO CERRADO IDENTIFICATION OF AEROGENERATORS IN CLOSED LOOP
Sector de la técnicaTechnical sector
La presente invención está relacionada con el control funcional de los aerogeneradores, proponiendo un sistema de identificación en lazo cerrado para dicha aplicación.The present invention is related to the functional control of wind turbines, proposing a closed loop identification system for said application.
Estado de la técnicaState of the art
Numerosos y diversos estudios teóricos existen a propósito de la fisica que envuelve un aerogenerador.Numerous and diverse theoretical studies exist regarding the physics that involves a wind turbine.
Estos estudios han hecho que se desarrollen modelos no lineales teóricos del comportamiento de los aerogeneradores con diferentes grados de acierto.These studies have led to the development of theoretical nonlinear models of wind turbine behavior with different degrees of success.
El desarrollo de estos modelos no lineales y su implementación en simuladores, unido a la complejidad creciente de los aerogeneradores ha hecho necesario el crecimiento en complejidad del control de los mismos. Para poder diseñar controladores, se requiere disponer de modelos lineales que describan de la mejor forma posible el comportamiento del aerogenerador, para diferentes condiciones de viento.The development of these non-linear models and their implementation in simulators, together with the increasing complexity of wind turbines has made the growth in complexity of their control necessary. To be able to design controllers, it is necessary to have linear models that describe in the best possible way the behavior of the wind turbine, for different wind conditions.
El desarrollo de simuladores basados en complejos modelos no lineales, junto con las necesidades de los diseñadores de control, han llevado a que se utilicen los simuladores no lineales con el fin de obtener modelos lineales, mediante diferentes técnicas de linealización, obteniendo resultados cuya idoneidad es en algunos casos discutible.The development of simulators based on complex non-linear models, together with the needs of control designers, have led to the use of non-linear simulators in order to obtain linear models, using different linearization techniques, obtaining results whose suitability is In some cases moot.
Un hecho cierto en todos los ámbitos de la ciencia, y la descripción de ésta, es la necesidad de contar con datos experimentales que de alguna forma permitan dar valores numéricos a las diferentes constantes que intervienen en un modelo. Este es un problema complejo y en muchos ámbitos no resuelto en su totalidad.A true fact in all areas of the science, and its description, is the need to have experimental data that somehow allow numerical values to be given to the different constants involved in a model. This is a complex problem and in many areas not fully resolved.
Un aerogenerador es un mecanismo muy complejo, que incluye gran número de elementos mecánicos, actuadores, elementos aerodinámicos, etc. Además, un aerogenerador es un mecanismo sumamente complejo de analizar de forma independiente, lo que hace tremendamente complejo conseguir ajustar de forma correcta toda la cantidad de parámetros que junto con las ecuaciones de la dinámica, describen el comportamiento del aerogenerador.A wind turbine is a very complex mechanism, which includes a large number of mechanical elements, actuators, aerodynamic elements, etc. In addition, a wind turbine is an extremely complex mechanism to analyze independently, which makes it extremely complex to correctly adjust the entire number of parameters that, together with the dynamics equations, describe the behavior of the wind turbine.
Estos problemas relativos a la cuantificación de ciertos parámetros del modelo no lineal, junto con las técnicas numéricas de linealización poco correctas, llevan en ocasiones a la obtención de modelos lineales poco acertados, o poco ajustados a la realidad. Dichos modelos son dificilmente evaluables hasta que el control que se diseña no se prueba en la máquina real, y se analiza si el comportamiento simulado se asemeja al real. Se ha comprobado con cierta frecuencia que un diseño de control basado en modelos lineales obtenidos a partir de dichos simuladores no lineales, no funciona en el sistema real, lo que obliga a la realización de ajustes manuales y poco precisos en el control diseñado.These problems related to the quantification of certain parameters of the non-linear model, together with the poorly correct numerical linearization techniques, sometimes lead to the obtaining of linear models that are not very successful, or that are not adjusted to reality. These models are difficult to assess until the control that is designed is not tested on the real machine, and it is analyzed whether the simulated behavior resembles the real one. It has been proven with some frequency that a control design based on linear models obtained from said non-linear simulators does not work in the real system, which requires manual and little precise adjustments to the designed control.
Esto pone de manifiesto que los modelos obtenidos de dicha forma no son del todo correctos y que es aconsejable una experimentación sobre el sistema real (o sobre su modelo no lineal teórico) para la obtención de modelos adecuados.This shows that the models obtained in this way are not entirely correct and that experimentation on the real system (or on its theoretical nonlinear model) is advisable for obtaining of suitable models.
La forma más habitual para obtener valores de ciertas propiedades fisicas de una máquina real a identificar, es operar experimentalmente con la máquina de una forma concreta. La experimentación para la identificación en el ámbito del control se lleva a cabo sobre el sistema real, operando tradicionalmente en lazo abierto. Esto es, aplicando una señal excitante al sistema y leyendo las variables de salida. Este proceso es posible hacerlo cuando se tiene acceso a la fuente de energía que gobierna el comportamiento del mecanismo.The most common way to obtain values of certain physical properties of a real machine to identify, is to operate experimentally with the machine in a concrete way. Experimentation for identification in the field of control is carried out on the real system, traditionally operating in open loop. That is, applying an exciting signal to the system and reading the output variables. This process is possible when you have access to the source of energy that governs the behavior of the mechanism.
Este método tiene fundamentalmente dos limitaciones o contraindicaciones. La primera de las limitaciones es que no es recomendable hacer este tipo de identificación en lazo abierto cuando la integridad de la máquina se puede ver comprometida por operar en dicho modo. La segunda de las limitaciones viene por el hecho de no tener acceso a la fuente de energía que gobierna el comportamiento de la máquina. En el caso de un aerogenerador, nos encontramos por lo tanto ante dos limitaciones que las técnicas de identificación en lazo abierto presentan.This method basically has two limitations or contraindications. The first of the limitations is that it is not advisable to make this type of identification in open loop when the integrity of the machine can be compromised by operating in said mode. The second of the limitations comes from the fact of not having access to the power source that governs the behavior of the machine. In the case of a wind turbine, we are therefore faced with two limitations that open loop identification techniques present.
Por todos estos motivos expuestos anteriormente se ve imprescindible utilizar técnicas de identificación en lazo cerrado en el ámbito del control de aerogeneradores .For all these reasons, it is essential to use closed loop identification techniques in the field of wind turbine control.
La identificación en lazo abierto es una técnica conocida y utilizada ampliamente en el ámbito del control y otras áreas científicas o financieras. El concepto de la identificación en el ámbito del control, se refiere a un método para obtener de forma experimental modelos de entrada-salida de un mecanismo o máquina. El concepto de lazo abierto se refiere por su parte a que el sistema se desarrolla sin que esté activo el control del mecanismo o máquina de aplicación, lo cual hace que el sistema opere libremente.Open loop identification is a technique known and widely used in the field of control and other scientific or financial areas. The concept of identification in the field of control refers to a method for experimentally obtaining input-output models of a mechanism or machine. The concept of open loop refers in turn to the fact that the system is developed without the control of the application mechanism or machine being active, which makes the system operate freely.
Dicha técnica de identificación en lazo abierto, se desarrolla de forma experimental, partiendo de una configuración concreta en relación con el sistema para el que va destinada la aplicación.This open loop identification technique is developed experimentally, based on a specific configuration in relation to the system for which the application is intended.
En el caso de los aerogeneradores, el proceso convencional de diseño de controladores se desarrolla mediante modelos lineales obtenidos a partir de simuladores no lineales. Los protocolos y algoritmos de linealización son diversos, pero tienen en común que son métodos numéricos y que están basados en exclusiva en las ecuaciones teóricas que describen el comportamiento de un aerogenerador . Dicho protocolo consiste en aplicar un impulso diferencial a las distintas entradas a los modelos no lineales. Éstas pueden ser velocidad de viento, ángulo de pitch y par del generador, etc. Tras estas pequeñas perturbaciones, se deja evolucionar libremente al aerogenerador. Asi se estiman las derivadas de todos los estados definidos por el simulador no lineal y a partir de estos valores que se obtienen, se determinan modelos lineales de la máquina a controlar, con los que se diseñan los controladores y que luego son implementados en las máquinas reales.In the case of wind turbines, the conventional controller design process is developed using linear models obtained from non-linear simulators. The protocols and linearization algorithms are diverse, but they have in common that they are numerical methods and that they are based exclusively on the theoretical equations that describe the behavior of a wind turbine. This protocol consists in applying a differential impulse to the different inputs to the non-linear models. These can be wind speed, pitch angle and generator torque, etc. After these small disturbances, the wind turbine is allowed to evolve freely. Thus, the derivatives of all the states defined by the non-linear simulator are estimated and from these values that are obtained, linear models of the machine to be controlled are determined, with which the controllers are designed and then implemented in real machines .
Debido a la variabilidad de los factores que influyen en el comportamiento de los aerogeneradores, los controladores que se obtienen de la forma indicada, basados en modelos obtenidos tras la linealización de simuladores no lineales, en ocasiones no funcionan como era de esperar sobre la máquina real. Esto puede ser critico, ya que el diseño de los componentes de un aerogenerador se hace en función de los controladores diseñados frente a los modelos lineales.Due to the variability of the factors that They influence the behavior of wind turbines, the controllers that are obtained in the indicated way, based on models obtained after the linearization of non-linear simulators, sometimes they do not work as expected on the real machine. This can be critical, since the design of the components of a wind turbine is based on the controllers designed against the linear models.
Es conocido, por otro lado, el concepto de lazo cerrado, que hace referencia al hecho de que los lazos de control que gobiernan de forma automática el comportamiento de un mecanismo, están activos durante el funcionamiento normal de la máquina.It is known, on the other hand, the concept of closed loop, which refers to the fact that the control loops that automatically govern the behavior of a mechanism, are active during the normal operation of the machine.
El concepto de identificación en lazo cerrado, fue no obstante rechazado en sus comienzos por los investigadores, al considerar que no era aplicable por motivos técnicos. Sin embargo estudios realizados recientemente evidencian que esta tecnología es posible, haciendo una correcta formulación del problema y de los algoritmos usados en el proceso.The concept of closed-loop identification, however, was initially rejected by the researchers, considering that it was not applicable for technical reasons. However, recent studies show that this technology is possible, making a correct formulation of the problem and the algorithms used in the process.
Objeto de la invenciónObject of the invention
De acuerdo con la invención se propone un sistema de identificación de los aerogeneradores en lazo cerrado, mediante el cual se logra la obtención de modelos lineales que representan de forma precisa el comportamiento dinámico del aerogenerador de aplicación, pudiendo utilizarse dichos modelos para diversos fines, como diseño de controladores, utilización como parte de un algoritmo de control, identificación de parámetros, análisis de componentes, etc. El sistema se basa en el desarrollo de un proceso que se lleva a cabo a través de un software, mediante el cual se efectúan una serie de pasos, obteniendo y almacenándose datos, los cuales son posteriormente analizados y tratados con el fin de obtener modelos de entrada y salida que puedan ser posteriormente utilizados para cualquiera de las funciones indicadas anteriormente .In accordance with the invention, a system of identification of closed-loop wind turbines is proposed, by means of which linear models that accurately represent the dynamic behavior of the application wind turbine can be obtained, such models being used for various purposes, such as controller design, use as part of a control algorithm, parameter identification, component analysis, etc. The system is based on the development of a process that is carried out through software, through which a series of steps are performed, obtaining and storing data, which are subsequently analyzed and treated in order to obtain models of input and output that can be subsequently used for any of the functions indicated above.
Como se ha comentado, el objetivo de este protocolo de experimentación es obtener modelos de entrada/salida para el aerogenerador . Cuando a lo largo del texto se haga referencia a entrada, debe suponerse que puede ser cualquiera de las siguientes variables de entrada:As mentioned, the objective of this experimentation protocol is to obtain input / output models for the wind turbine. When reference is made throughout the text, it should be assumed that it can be any of the following input variables:
Relacionadas con el viento: Velocidad del viento, a cualquier altura desde el suelo o a cualquier distancia del aerogenerador, ya sean medidas o inferidas.Wind-related: Wind speed, at any height from the ground or at any distance from the wind turbine, whether measured or inferred.
Relacionadas con el generador: Par del generador, real o demandado, par en el entrehierro del generador, potencia del generador, real o demandada, potencia activa, real o demandada, potencia reactiva, real o demandada, corrientes y tensiones de cada una de las lineas del sistema trifásico, reales o demandadas, tensiones y corrientes d y q, reales o demandadas, del sistema de control del generador, etc.Related to the generator: Generator torque, real or demanded, torque in the generator air gap, generator power, real or demanded, active power, real or demanded, reactive power, real or demanded, currents and voltages of each of the lines of the three-phase system, real or demanded, voltages and currents dyq, real or demanded, of the generator control system, etc.
Relacionadas con el actuador de pitch: Ángulo de pitch, real o demandado, velocidad de pitch, real o demandada, aceleración de pitch, real o demandada, potencias, tensiones y corrientes, _ •ηRelated to the pitch actuator: Pitch angle, real or demanded, pitch speed, real or demanded, pitch acceleration, real or demanded, powers, voltages and currents, _ • η
reales o demandadas del motor de pitch. Presiones, flujos, posiciones, velocidades y aceleraciones del actuador, en caso de ser hidráulico, etc.actual or demanded of the pitch motor. Pressures, flows, positions, speeds and accelerations of the actuator, in case of being hydraulic, etc.
- Relacionadas con el actuador del yaw: Ángulo de yaw, real o demandado, velocidad de yaw, real o demandada, aceleración de yaw, real o demandada, potencias, tensiones y corrientes, reales o demandadas del motor de yaw. Presiones, flujos, posiciones, velocidades y aceleraciones del actuador, en caso de ser hidráulico, etc- Related to the yaw actuator: Yaw angle, real or demanded, yaw speed, real or demanded, yaw acceleration, real or demanded, powers, voltages and currents, real or demanded of the yaw motor. Pressures, flows, positions, speeds and accelerations of the actuator, in case of being hydraulic, etc.
Relacionadas con la geometria de la pala: Variación en geometria de la sección de la pala y de la longitud de la pala, posición, velocidad, aceleración de elementos o partes de elementos, utilizadas para el control aerodinámico, móviles en las palas del aerogenerador, asi como tensiones, corrientes, presiones, flujos, etc., de los actuadores que modificasen las propiedades geométricas de las palasRelated to the geometry of the blade: Variation in geometry of the section of the blade and the length of the blade, position, speed, acceleration of elements or parts of elements, used for aerodynamic control, mobile in the blades of the wind turbine, as well as voltages, currents, pressures, flows, etc., of the actuators that modified the geometric properties of the blades
Por otro lado, cuando el texto hace referencia a salidas dentro del proceso de identificación, se estará refiriendo a cualquiera de las siguientes variables, sensables o inferidas, de un aerogenerador:On the other hand, when the text refers to outputs within the identification process, it will be referring to any of the following variables, sensible or inferred, of a wind turbine:
Velocidad del generador, velocidad del rotor en el lado de alta, velocidad del rotor en lado de baja, potencia activa real y demandada al generador, potencia reactiva real y demandada al generador, corrientes y tensiones reales y demandadas de cada una de las lineas del sistema trifásico, tensiones y corrientes reales y demandadas d y q del sistema de control del generador, deformaciones, posiciones, velocidades, aceleraciones, lineales y angulares, fuerzas y momentos en el buje, a lo largo del tren de potencia, a lo largo de cada una de las palas, a lo largo de la torre, a lo largo de la nacelle, etc.Speed of the generator, speed of the rotor on the high side, speed of the rotor on the low side, real and demanded active power to the generator, real and demanded reactive power to the generator, actual and demanded currents and voltages of each of the lines of the three-phase system, actual and demanded voltages and currents dyq of the generator control system, deformations, positions, speeds, accelerations, linear and angular, forces and moments in the bushing, along the power train, along each of the blades, along the tower, along the nacelle, etc.
Todas las variables citadas como variables de entrada, pueden ser también consideradas como variables de salida.All variables cited as input variables can also be considered as output variables.
El proceso comprende un protocolo de experimentación, una recolección de datos, unas rutinas de identificación, y la obtención de modelos lineales para la aplicación que se desee.The process includes an experimentation protocol, data collection, identification routines, and obtaining linear models for the desired application.
El protocolo de experimentación se desarrolla durante el funcionamiento normal del aerogenerador, con el control del mismo activo. Este control consiste en la introducción de una señal de referencia como valor deseado para la variable que se quiere controlar. La señal que se quiere controlar, la salida, se realimenta para compararla con la señal de referencia. Esta diferencia, llamada error, alimenta al controlador que será el responsable de aplicar una señal que hará que mediante el actuador, la señal de salida se aproxime a su valor de referencia, intentando asi rechazar perturbaciones externas e incontrolables al sistema como puedan ser ráfagas de viento etc.The experimentation protocol is developed during the normal operation of the wind turbine, with the control of the same asset. This control consists in the introduction of a reference signal as the desired value for the variable to be controlled. The signal to be controlled, the output, is fed back to compare it with the reference signal. This difference, called error, feeds the controller that will be responsible for applying a signal that will cause the output signal to approximate its reference value by means of the actuator, thus trying to reject external and uncontrollable disturbances to the system such as bursts of wind etc.
Por su parte el protocolo de experimentación en lazo cerrado para la identificación de aerogeneradores, se lleva a cabo mediante la introducción de una señal que puede ser sumada bien a la señal de referencia del lazo de control o bien puede ser sumada al valor que el controlador haya calculado. La recolección y almacenamiento de datos, se debe hacer por software, para luego ser analizados mediante las rutinas de identificación.For its part, the closed loop experimentation protocol for the identification of wind turbines is carried out by introducing a signal that can be added to the reference signal of the control loop or can be added to the value that the controller have calculated. Data collection and storage should be done by software, and then analyzed using identification routines.
Las rutinas de identificación deben constar de una copia del controlador y un modelo ajustable del modelo salida/entrada en lazo cerrado, de cualquier combinación de las variables de entrada y salida citadas anteriormente. La salida correspondiente del aerogenerador real es comparada con la salida del lazo cerrado predicha por el algoritmo de identificación. El error es procesado mediante otro algoritmo, que variará los valores de los parámetros en la forma adecuada, con el fin de minimizar la diferencia entre la medida real de la variable de salida del aerogenerador y la variable de salida predicha por el algoritmo de identificación.The identification routines must consist of a copy of the controller and an adjustable model of the closed loop input / output model, of any combination of the input and output variables mentioned above. The corresponding output of the real wind turbine is compared with the closed loop output predicted by the identification algorithm. The error is processed by another algorithm, which will vary the values of the parameters in the appropriate way, in order to minimize the difference between the actual measurement of the wind turbine output variable and the output variable predicted by the identification algorithm.
Una vez el modelo es obtenido, éste puede ser validado por métodos estadísticos, frecuenciales y temporales. Si estas condiciones de validación se cumplen, los modelos son dados por correctos y se pueden entonces emplear para todas las actividades expuestas.Once the model is obtained, it can be validated by statistical, frequency and temporal methods. If these validation conditions are met, the models are given as correct and can then be used for all the exposed activities.
Se obtiene asi un sistema con el que se logran las ventajas siguientes:A system is thus obtained with which the following advantages are achieved:
1. Obtención de modelos fiables. La experiencia en el trabajo con modelos lineales obtenidos mediante técnicas de linealización a partir de simuladores no lineales, demuestra que éstos proporcionan en ocasiones modelos poco fiables; de modo que se pueden encontrar modelos de una misma máquina que presentan propiedades muy diferentes e incluso contradictorias. Esto hace que el diseño de controladores frente a dichos modelos plantee dudas razonables sobre la validez de los mismos. Por el contrario los modelos que se obtienen en lazo cerrado son más próximos a la realidad y por lo tanto más fiables, obteniéndose mejores resultados a partir de ellos .1. Obtaining reliable models. Experience in working with linear models obtained through linearization techniques from non-linear simulators, demonstrates that these sometimes provide unreliable models; so that you can find models of the same machine that have very different properties and even contradictory. This makes the design of controllers against these models raise reasonable doubts about their validity. On the contrary, the models obtained in closed loop are closer to reality and therefore more reliable, obtaining better results from them.
2. Reducción de errores numéricos en los modelos. Una de las posibles consecuencias de las técnicas usadas actualmente para la estimación de los modelos, es la obtención de modelos mal condicionados. Esto da lugar a limitaciones en el trato de los mismos y en su correcta transformación de un sistema de representación de modelos lineales (espacios de estado) , a otros métodos de representación de modelos lineales de entrada-salida (funciones de transferencia) . Por el contrario el sistema propuesto elimina el problema de la obtención de modelos mal condicionados.2. Reduction of numerical errors in the models. One of the possible consequences of the techniques currently used for estimating models is the obtaining of poorly conditioned models. This results in limitations in their treatment and in their correct transformation of a system of representation of linear models (state spaces), to other methods of representation of linear input-output models (transfer functions). On the contrary, the proposed system eliminates the problem of obtaining poorly conditioned models.
3. Modelos teórico-prácticos.3. Theoretical-practical models.
El hecho de utilizarse una técnica experimental, permite la utilización del sistema tanto en el ámbito de la simulación, como en el ámbito de la experimentación en máquinas reales.The fact of using an experimental technique allows the use of the system both in the field of simulation, and in the field of experimentation on real machines.
4. Modelos "ad-hoc" para cada máquina y emplazamiento . El hecho de poder obtener un modelo para cada máquina, hace que se pueda diseñar un controlador apropiado para cada una de ellas, en relación con sus propias especificidades debidas a la construcción, montaje, emplazamiento, etc. 5. Obtención de modelos temporales de una misma máquina .4. "Ad-hoc" models for each machine and location. The fact of being able to obtain a model for each machine, makes it possible to design an appropriate controller for each of them, in relation to its own specificities due to construction, assembly, location, etc. 5. Obtaining temporary models of the same machine.
El hecho de que se pueda experimentar sobre máquinas reales, hace que se puedan obtener modelos que describan su comportamiento cuando se considere oportuno, de forma que se puede estudiar la degradación entre el modelo teórico y la máquina real con el paso del tiempo.The fact that one can experiment on real machines, makes it possible to obtain models that describe their behavior when deemed appropriate, so that degradation between the theoretical model and the real machine can be studied over time.
6. Mantenimiento aplicado a los algoritmos de control .6. Maintenance applied to control algorithms.
Dado que se pueden obtener modelos reales de la máquina en cualquier instante de tiempo, se pueden hacer las modificaciones que se consideren oportunas dentro de los algoritmos de control, que tengan en cuenta los cambios que sufre la máquina con el paso del tiempo y que se detectan con el modelo identificador .Since real machine models can be obtained at any time, the modifications deemed appropriate within the control algorithms can be made, taking into account the changes that the machine undergoes over time and They detect with the identifier model.
7. Utilización de los modelos identificados dentro de las rutinas de control.7. Use of the models identified within the control routines.
Existen distintas técnicas y estrategias de control que usan de forma explícita el modelo de la planta y el modelo de las perturbaciones que se pueden obtener mediante la identificación, por lo que al estar disponibles los modelos identificados mencionados, estas técnicas son susceptibles de ser usadas.There are different control techniques and strategies that explicitly use the plant model and the model of the disturbances that can be obtained through identification, so that when the identified models mentioned are available, these techniques are likely to be used.
Descripción de las figurasDescription of the figures
La figura 1 muestra un diagrama en bloques del proceso de desarrollo del sistema de la invención.Figure 1 shows a block diagram of the development process of the system of the invention.
La figura 2 es un esquema de la aplicación de la señal de excitación en el protocolo de experimentación del sistema, según un modo de realización. La figura 3 es un esquema de la aplicación de la señal de excitación en el protocolo de experimentación, según otro modo de realización.Figure 2 is a diagram of the application of the excitation signal in the system experimentation protocol, according to an embodiment. Figure 3 is a diagram of the application of the excitation signal in the experimentation protocol, according to another embodiment.
Descripción detallada de la invenciónDetailed description of the invention
El objeto de la invención se refiere a un sistema de identificación de aerogeneradores en lazo cerrado, el cual tiene como objetivo la obtención de modelos lineales que representen de forma precisa el comportamiento dinámico del aerogenerador de aplicación, para diseñar los algoritmos que rijan el comportamiento del aerogenerador en el funcionamiento real del mismo.The object of the invention relates to a closed loop wind turbine identification system, which aims to obtain linear models that accurately represent the dynamic behavior of the application wind turbine, to design the algorithms that govern the behavior of the wind turbine in the actual operation of it.
El sistema consiste en la realización de un proceso de generación, almacenamiento y análisis de datos, mediante una secuencia como la representada en la figura 1, que incluye un protocolo de experimentación (1) , una recogida de datos (2) , unas rutinas de identificación (3), la obtención (4) de modelos lineales de entrada-salida, y la aplicación (5) de los modelos lineales identificados para el diseño e implementación de controladores para aerogeneradores.The system consists of the realization of a process of generation, storage and analysis of data, by means of a sequence like the one represented in figure 1, which includes an experimentation protocol (1), a data collection (2), routines of identification (3), the obtaining (4) of linear input-output models, and the application (5) of the linear models identified for the design and implementation of wind turbine controllers.
De acuerdo con el sistema propuesto, el protocolo de experimentación (1) se desarrolla de la manera siguiente:In accordance with the proposed system, the experimentation protocol (1) is developed as follows:
Durante el funcionamiento normal del aerogenerador (6), según la representación de las figuras 2 y 3, el control de éste permanece siempre activo, aplicándose una señal de referencia (7) en relación con la señal que se quiere controlar, con realimentación (8) de la salida de dicha señal hacia la entrada, de manera que en un momento de operación del aerogenerador (6) se introduce una señal de excitación (9) en el algoritmo de control (10) que gobierna el sistema.During normal operation of the wind turbine (6), according to the representation of figures 2 and 3, its control is always active, applying a reference signal (7) in relation to the signal to be controlled, with feedback (8 ) of the output of said signal to the input, so that at an operation time of the wind turbine (6) an excitation signal (9) is introduced into the control algorithm (10) that governs the system.
Dicha señal de excitación (9) debe tener un alto contenido frecuencial, particularmente entre 0 y 1000 Hz, así como una longitud determinada y limitada dependiendo del aerogenerador (β) de aplicación, pudiendo ser aplicada esa señal de excitación (9) en la entrada de la señal de referencia (7), como representa la figura 2, o en una parte intermedia respecto de uno o varios de los actuadores que gobiernan el comportamiento del aerogenerador (6) , como representa la figura 3.Said excitation signal (9) must have a high frequency content, particularly between 0 and 1000 Hz, as well as a determined and limited length depending on the application wind turbine (β), which excitation signal (9) can be applied at the input of the reference signal (7), as shown in figure 2, or in an intermediate part with respect to one or more of the actuators that govern the behavior of the wind turbine (6), as shown in figure 3.
Es decir que, en relación con un aerogenerador (6), se puede marcar, por ejemplo, una velocidad de giro de las palas de dicho aerogenerador (6), con lo que éste trata de alcanzar dicha velocidad de giro de las palas adaptándose a cada velocidad del viento, para lo cual la señal de salida de la velocidad de las palas se introduce de nuevo en la máquina después de compararla con la señal de entrada, con lo cual se le está indicando al aerogenerador (6) una aceleración mayor o menor en la velocidad de giro, evitando que el funcionamiento del aerogenerador (6) se salga de los rangos lógicos de funcionamiento.That is to say, in relation to a wind turbine (6), it is possible to mark, for example, a speed of rotation of the blades of said wind turbine (6), whereby it tries to reach said speed of rotation of the blades adapting to each wind speed, for which the output signal of the speed of the blades is introduced back into the machine after comparing it with the input signal, which is indicating to the wind turbine (6) a greater acceleration or lower in the speed of rotation, preventing the operation of the wind turbine (6) from leaving the logical operating ranges.
Por otra parte, la introducción de una señal de excitación (9), que se acopla a la señal de referencia (7) de entrada, permite, mediante el estudio de la salida y del efecto de las perturbaciones, diseñar los algoritmos que rijan el funcionamiento del aerogenerador (6) en una situación real. El protocolo de experimentación (1) mencionado se puede realizar igualmente, en las mismas condiciones, sobre un simulador en lugar del aerogenerador real (6), consiguiéndose un idéntico resultado.On the other hand, the introduction of an excitation signal (9), which is coupled to the input reference signal (7), allows, by studying the output and the effect of the disturbances, to design the algorithms that govern the wind turbine operation (6) in a real situation. The mentioned experimentation protocol (1) can also be carried out, under the same conditions, on a simulator instead of the real wind turbine (6), achieving an identical result.
Mediante la recolección de datos (2) el experimento se puede repetir tantas veces como se desee, pudiendo aplicarse el procedimiento a todos los lazos de control que estén activos en el aerogenerador o simulador (6), con posibilidad de medir todas las variables oportunas para obtener los modelos que se deseen.By collecting data (2) the experiment can be repeated as many times as desired, and the procedure can be applied to all control loops that are active in the wind turbine or simulator (6), with the possibility of measuring all the appropriate variables for Get the models you want.
Durante la experimentación se guardan los datos correspondientes a todos los sensores que tenga el aerogenerador o simulador (6), asi como las secuencias de todas las señales involucradas en el lazo de control del aerogenerador, asi como • la señal de excitación, tanto si es introducida como una suma a la referencia, como si es introducida como suma a la acción calculada por el controlador.During the experiment, the data corresponding to all the sensors that the wind turbine or simulator (6) has, as well as the sequences of all the signals involved in the wind turbine control loop, as well as the excitation signal, whether it is saved entered as a sum to the reference, as if it is introduced as a sum to the action calculated by the controller.
Las rutinas de identificación (3) del proceso se desarrollan sometiendo los datos obtenidos a algoritmos de identificación de parámetros convencionales, de modo que estas rutinas de identificación (3) tienen por objeto encontrar la relación existente entre colecciones temporales de datos, siendo los resultados que se obtienen en dichas rutinas de identificación (3), modelos empíricos lineales.The identification routines (3) of the process are developed by submitting the data obtained to conventional parameter identification algorithms, so that these identification routines (3) are intended to find the relationship between temporary collections of data, the results being in these identification routines (3), linear empirical models are obtained.
El resultado de aplicar el protocolo de experimentación (1) , asi como la recolección de los datos (2) y el posterior tratamiento de éstos con las rutinas de identificación (3), son modelos lineales que describen el comportamiento del sistema, de manera que una vez que se obtienen (4) estos modelos, se pueden aplicar (5) para actividades como: diseño de componentes, puesta en marcha de aerogeneradores, certificación, control adaptativo, control predictivo, mantenimiento de control, sintonización de control, monitorización de funcionamiento dinámico, etc. The result of applying the experimentation protocol (1), as well as the data collection (2) and their subsequent treatment with the identification routines (3), are linear models that They describe the behavior of the system, so that once (4) these models are obtained, they can be applied (5) for activities such as: component design, start-up of wind turbines, certification, adaptive control, predictive control, maintenance of control, control tuning, dynamic operation monitoring, etc.

Claims

REIVINDICACIONES
1.- Identificación de aerogeneradores en lazo cerrado, para la obtención de modelos lineales que representen de forma precisa el comportamiento dinámico del aerogenerador de aplicación, caracterizado porque se desarrolla un proceso que comprende un protocolo de experimentación (1), una recolección de datos (2), rutinas de identificación (3), la obtención (4) de modelos lineales entrada-salida y la aplicación (5) de dichos modelos lineales para el diseño y síntesis de los controladores, en donde el protocolo de experimentación (1) incluye el suministro de una señal de referencia (7) en el algoritmo (10) de la función a controlar, con el aerogenerador (6) de aplicación en funcionamiento normal, realimentándose (8) la señal de salida de dicha función hacia la entrada, al mismo tiempo que se aplica una señal de excitación (9) en el algoritmo de control (10) del sistema.1.- Identification of wind turbines in a closed loop, to obtain linear models that accurately represent the dynamic behavior of the application wind turbine, characterized in that a process is developed that includes an experimentation protocol (1), a data collection ( 2), identification routines (3), obtaining (4) of linear input-output models and the application (5) of said linear models for the design and synthesis of controllers, where the experimentation protocol (1) includes the supply of a reference signal (7) in the algorithm (10) of the function to be controlled, with the application wind turbine (6) in normal operation, the output signal of said function being fed back (8) to the input, same time that an excitation signal (9) is applied in the control algorithm (10) of the system.
2.- Identificación de aerogeneradores en lazo cerrado, de acuerdo con la primera reivindicación, caracterizado porque la señal de excitación (9) se aplica en la misma entrada de suministro de la señal de referencia (7) .2.- Identification of wind turbines in closed loop, according to the first claim, characterized in that the excitation signal (9) is applied at the same input input of the reference signal (7).
3.- Identificación de aerogeneradores en lazo cerrado, de acuerdo con la primera reivindicación, caracterizado porque la señal de excitación (9) se aplica en una parte intermedia sobre los actuadores que gobiernan el funcionamiento del aerogenerador (6) de aplicación.3.- Identification of wind turbines in closed loop, according to the first claim, characterized in that the excitation signal (9) is applied in an intermediate part on the actuators that govern the operation of the application wind turbine (6).
4.- Identificación de aerogeneradores en lazo cerrado, de acuerdo con las reivindicaciones primera a tercera, caracterizado porque el protocolo de experimentación se puede realizar en las mismas condiciones sobre un aerogenerador (6) real, o sobre un 'simulador.4.- Identification of wind turbines in closed loop, according to claims first to third, characterized in that the experimentation protocol can be performed under the same conditions on a real wind turbine (6), or on a ' simulator.
5.- Identificación de aerogeneradores en lazo cerrado, de acuerdo con la primera reivindicación, caracterizado porque los modelos de entrada en relación con los que se aplica el sistema se refieren a variables relacionadas con el viento, con el generador, con el actuador de pitch, con el actuador de yaw, o con la geometria de las palas del aerogenerador.5.- Identification of wind turbines in closed loop, according to the first claim, characterized in that the input models in relation to which the system is applied refer to variables related to wind, with the generator, with the pitch actuator , with the yaw actuator, or with the geometry of the wind turbine blades.
6.- Identificación de aerogeneradores en lazo cerrado, de acuerdo con la primera reivindicación, caracterizado porque los modelos de salida en relación con los que se aplica el sistema se refieren a variables relacionadas con el generador, con el rotor, con las lineas del sistema trifásico, con el sistema de control, o con la geometria de cualquiera de las partes estructurales del aerogenerador. 6.- Identification of wind turbines in closed loop, according to the first claim, characterized in that the output models in relation to which the system is applied refer to variables related to the generator, with the rotor, with the system lines three-phase, with the control system, or with the geometry of any of the structural parts of the wind turbine.
PCT/ES2007/000584 2006-10-17 2007-10-17 Closed-loop identification of wind turbines WO2008046942A1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
ES200602630A ES2299375B1 (en) 2006-10-17 2006-10-17 SYSTEM FOR ESTIMATING THE BEHAVIOR OF AN AEROGENERATOR THAT OPERATES IN CLOSED LOOP.
ESP200602630 2006-10-17

Publications (1)

Publication Number Publication Date
WO2008046942A1 true WO2008046942A1 (en) 2008-04-24

Family

ID=39313637

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/ES2007/000584 WO2008046942A1 (en) 2006-10-17 2007-10-17 Closed-loop identification of wind turbines

Country Status (2)

Country Link
ES (1) ES2299375B1 (en)
WO (1) WO2008046942A1 (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2353089A1 (en) * 2008-11-28 2011-02-25 Fundacion Cener-Ciemat System for the closed loop estimation of linear models entrance output of a wind turbine. (Machine-translation by Google Translate, not legally binding)
EP2292928A2 (en) 2009-09-03 2011-03-09 Gamesa Innovation & Technology, S.L. Wind turbine control methods and systems
EP2336558A2 (en) 2009-12-16 2011-06-22 Gamesa Innovation & Technology, S.L. Method of operating a variable speed wind turbine
CN104612904A (en) * 2014-12-08 2015-05-13 上海电气集团股份有限公司 Maximum wind energy capturing method for double-feed type wind generating set
EP3073109A1 (en) * 2015-03-23 2016-09-28 ALSTOM Renewable Technologies Obtaining dynamic properties of a part of wind turbine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN110244557B (en) * 2019-04-30 2022-03-15 国网浙江省电力有限公司电力科学研究院 Closed-loop modeling method of industrial process multi-order inertia closed-loop system

Non-Patent Citations (4)

* Cited by examiner, † Cited by third party
Title
DE BRUYNE F. ET AL.: "One closed-loop identification with a tailor-made parametrization", PROCEEDINGS OF THE AMERICA CONTROL CONFERENCE, PHILADELPHIA, PENNSYLVANIA, vol. 5, June 1998 (1998-06-01), pages 3177 - 3181 *
FORSSELL U.: "Closed-loop Identification Methods, Theory, and Applications", LINKÖPING STUDIES IN SCIENCE AND TECHNOLOGY. DISSERATIONS. NO. 566. DEPARTMENT OF ELECTRICAL ENGINEERING LINKÖPING UNIVERSITY, SE-581 83 LINKÖPING, SWEDEN, pages 5 - 11, 17 - 19, 24 - 26, 41 - 42, 49 - 68, Retrieved from the Internet <URL:http://www.control.isy.liu.se/research/authors/phd/566/main.pdf> *
VAN BAARS G. AND BONGERS P.: "Closed Loop System Identification of an Industrial Wind Turbine System: Experiment Design and First Validation Results", PROCEEDINGS OF THE 33RD CONFERENCE ON DECISION AND CONTROL, LAKE BUENA VISTA. FLORIDA *
VODA A. AND LANDAU I.D.: "Real-time evaluation of an iterative scheme for closed loop identification and control design", PROCEEDINGS OF THE AMERICAN CONTROL CONFERENCE, BALTIMORE, MARYLAND, vol. 3, July 1994 (1994-07-01), pages 3007 - 3011, XP010303968 *

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ES2353089A1 (en) * 2008-11-28 2011-02-25 Fundacion Cener-Ciemat System for the closed loop estimation of linear models entrance output of a wind turbine. (Machine-translation by Google Translate, not legally binding)
EP2292928A2 (en) 2009-09-03 2011-03-09 Gamesa Innovation & Technology, S.L. Wind turbine control methods and systems
EP2336558A2 (en) 2009-12-16 2011-06-22 Gamesa Innovation & Technology, S.L. Method of operating a variable speed wind turbine
US20110215577A1 (en) * 2009-12-16 2011-09-08 Gamesa Innovation & Technology, S.L. Wind turbine control methods for improving the production of energy recovering energy losses
US9018780B2 (en) 2009-12-16 2015-04-28 Gamesa Innovation & Technology, S.L. Control system and method to improve the electrical energy production of a variable speed wind turbine by alternative regulation
CN104612904A (en) * 2014-12-08 2015-05-13 上海电气集团股份有限公司 Maximum wind energy capturing method for double-feed type wind generating set
EP3073109A1 (en) * 2015-03-23 2016-09-28 ALSTOM Renewable Technologies Obtaining dynamic properties of a part of wind turbine

Also Published As

Publication number Publication date
ES2299375B1 (en) 2009-03-01
ES2299375A1 (en) 2008-05-16

Similar Documents

Publication Publication Date Title
Campagnolo et al. Wind tunnel testing of wake control strategies
WO2008046942A1 (en) Closed-loop identification of wind turbines
Bottasso et al. Wind tunnel testing of scaled wind turbine models: Beyond aerodynamics
Gebraad et al. A data-driven model for wind plant power optimization by yaw control
Menon et al. Dynamic aeroelastic behavior of wind turbine rotors in rapid pitch-control actions
Hure et al. Optimal wind turbine yaw control supported with very short-term wind predictions
CN105888971A (en) Active load reducing control system and method for large wind turbine blade
Heinz et al. Investigation of the load reduction potential of two trailing edge flap controls using CFD
Dai et al. Load and dynamic characteristic analysis of wind turbine flexible blades
KR101778912B1 (en) Correction apparatus for yaw alignment error of wind turbine
Bottasso et al. Wind tunnel testing of wind turbines and farms
Michel et al. Model-free control of the dynamic lift of a wind turbine blade section: experimental results
Cutler et al. Optimization of turbine tilt in a wind farm
Fleming et al. From wake steering to flow control
Stol et al. Disturbance accommodating control of a variable-speed turbine using a symbolic dynamics structural model
ES2353089B2 (en) SYSTEM FOR ESTIMATION IN CLOSED LOOP OF LINEAR MODELS INPUT OUT OF AN AIRCRAFT.
Campagnolo et al. Further calibration and validation of FLORIS with wind tunnel data
Su et al. A novel hybrid free-wake model for wind turbine performance and wake evolution
Svetozarevic et al. A robust fault detection and isolation filter for a horizontal axis variable speed wind turbine
Cordes et al. The Adaptive Camber Concept—A passive approach for gust load alleviation on wind turbines
Wang et al. Computation of hoisting forces on wind turbine blades using computation fluid dynamics
Petrović et al. Identification of wind turbine mathematical model suitable for advanced controller design
Wang et al. Numerical verification of the dynamic aerodynamic similarity criterion for wind tunnel experiments of floating offshore wind turbines
Rodrigues et al. Experimental validation of a wind turbine
Schepers et al. Final report of Task 29, Phase IV: Detailed Aerodynamics of Wind Turbines

Legal Events

Date Code Title Description
121 Ep: the epo has been informed by wipo that ep was designated in this application

Ref document number: 07822991

Country of ref document: EP

Kind code of ref document: A1

NENP Non-entry into the national phase

Ref country code: DE

122 Ep: pct application non-entry in european phase

Ref document number: 07822991

Country of ref document: EP

Kind code of ref document: A1