Wake up Radio Architecture for Wireless Sensor Networks Using an Ultra Low Power FPGA

In this paper an implementation of a Wake up Radio(WuR) with addressing capabilities based on an ultra low power FPGA for ultra low energy Wireless Sensor Networks (WSNs) is proposed. The main goal is to evaluate the utilization of very low power configurable devices to take advantage of their speed, flexibility and low power consumption instead of the traditional approaches based on ASICs or microcontrollers, for communication frame decoding and communication data control.

Sistemas de control de roturas en presas y caracterización de sistemas hidráulicos

Este proyecto nace de la necesidad de automatizar el estudio de sistemas hidráulicos y de control de roturas en presas. Para realizar el estudio de sistemas hidráulicos se usarán un número indeterminado de sensores de nivel, presión y caudal. El número de sensores que se pueden utilizar viene determinado por el material disponible. Estos sensores se conectarán a unas tarjetas de National Instruments modelo NI 9208 y éstas a su vez a un chasis modelo CompactDAQ NI-9174 con cuatro ranuras. Conectando este chasis al ordenador podremos obtener los datos provenientes de los sensores. También se podrá controlar una válvula para determinar la cantidad de agua que fluye en nuestro experimento. Está válvula está conectada a una tarjeta NI-9264 que se conectará al chasis en su última posición Para detectar y estudiar posibles roturas en presas se dispone de un motor y un láser con los cuales se puede barrer la superficie de una presa y obtener una imagen en tres dimensiones de la misma procesando los datos provenientes del laser. Para recoger los datos de los sensores y controlar una válvula se ha desarrollado una aplicación utilizando LabVIEW, un programa creado por National Instruments. Para poder controlar el motor y el láser se parte de una aplicación que ya estaba realizada en LabVIEW. El objetivo ha sido detectar y corregir una serie de errores en la misma. Dentro del proyecto, además de la explicación detallada de la aplicación para los sensores y la válvula, y las pruebas realizadas para detectar y corregir los errores de la aplicación del láser y el motor, existe: una breve introducción a la programación en LabVIEW, la descripción de los pasos realizados para el conexionado de los sensores con las tarjetas, los manuales de usuario de las aplicaciones y la descripción de los equipos utilizados. This project stars from the need to automate the study of hydraulic systems and control dam breaks. For the study of hydraulic systems it will be used an unspecified number of level, pressure and flow sensors. The number of sensors that can be used is determined by the available material. These sensors are connected to a NI 9208 National Instruments target and these cards to a NI-9174 CompactDAQ chassis with four slots. Connecting the chassis to a computer we will obtain data from the sensors. We also can control a valve to determine the amount of water flowing in our experiment. This valve is connected to a NI-9264 card and this card to the last position of the chassis. To detect and study dams breakage it used a motor and a laser. With these two devices we can scan the surface of a dam and obtain a three-dimensional image processing data from the laser. To collect data from the sensors and control the valve it has developed an application using LabVIEW, a program created by National Instruments. To control the motor and the laser it is used an application that was already created using LabVIEW. The aim of this part has been detect and correct a number of errors in this application. Within the project, in addition to the detailed explanation of the application for sensors and valve, and tests to detect and correct errors in the application of lasers and the motor, there is: a brief introduction to programming in LabVIEW, the description of the steps taken for connecting the sensors with cards, user manuals and application description of the equipment used.

LED backlight designs with the flow-line method

An LED backlight has been designed using the flow-line design method. This method allows a very efficient control of the light extraction. The light is confined inside the guide by total internal reflection, being extracted only by specially calculated surfaces: the ejectors. Backlight designs presented here have a total optical efficiency of up to 80% (including Fresnel and absorption losses) with an FWHM below 30 degrees. The experimental results of the first prototype are shown.

Flow and wakes in large wind farms in complex terrain and offshore

Power losses due to wind turbine wakes are of the order of 10 and 20% of total power output in large wind farms. The focus of this research carried out within the EC funded UPWIND project is wind speed and turbulence modelling for large wind farms/wind turbines in complex terrain and offshore in order to optimise wind farm layouts to reduce wake losses and loads.

Wake-up architecture for Wireless sensor nodes based on ultra low power FPGA

In this work a novel wake-up architecture for wireless sensor nodes based on ultra low power FPGA is presented. A simple wake up messaging mechanism for data gathering applications is proposed. The main goal of this work is to evaluate the utilization of low power configurable devices to take advantage of their speed, flexibility and low power consumption compared with traditional approaches, based on ASICs or microcontrollers, for frame decoding and data control. A test bed based on infrared communications has been built to validate the messaging mechanism and the processing architecture.

CFD modelling of the interaction between the Surface Boundary Layer and rotor wake. Comparison of results obtained with different turbulence models and mesh strategies

A simplified CFD wake model based on the actuator disk concept is used to simulate the wind turbine, represented by a disk upon which a distribution of forces, defined as axial momentum sources, are applied on the incoming non-uniform flow. The rotor is supposed to be uniformly loaded, with the exerted forces function of the incident wind speed, the thrust coefficient and the rotor diameter. The model is tested under different parameterizations of turbulence models and validated through experimental measurements downwind of a wind turbine in terms of wind speed deficit and turbulence intensity.

Validation of a CFD wake model based on the actuator disk technique and the thrust coefficient. Preliminary results

A simplified CFD wake model based on the actuator-disk concept is used to simulate the wind turbine, represented by an actuator disk upon which a distribution of forces, defined as axial momentum sources, are applied on the incoming flow. The rotor is supposed to be uniformly loaded, with the exerted forces as a function of the incident wind speed, the thrust coefficient and the rotor diameter. The model is validated through experimental measurements downwind of a wind turbine in terms of wind speed deficit. Validation on turbulence intensity will also be made in the near future.

Prediction of wake effects on wind farm power production using a RANS approach. Part II. Offshore: Case studies from the UPWIND project

The estimation of power losses due to wind turbine wakes is crucial to understanding overall wind farm economics. This is especially true for large offshore wind farms, as it represents the primary source of losses in available power, given the regular arrangement of rotors, their generally largerdiameter and the lower ambient turbulence level, all of which conspire to dramatically affect wake expansion and, consequently, the power deficit. Simulation of wake effects in offshore wind farms (in reasonable computational time) is currently feasible using CFD tools. An elliptic CFD model basedon the actuator disk method and various RANS turbulence closure schemes is tested and validated using power ratios extracted from Horns Rev and Nysted wind farms, collected as part of the EU-funded UPWIND project. The primary focus of the present work is on turbulence modeling, as turbulent mixing is the main mechanism for flow recovery inside wind farms. A higher-order approach, based on the anisotropic RSM model, is tested to better take into account the imbalance in the length scales inside and outside of the wake, not well reproduced by current two-equation closure schemes.

Far wake structure in rarefied plasma flows past charged bodies

The asymptotic structure of the far-wake behind a charged body in a rarefied plasma flow is investigated under the assumption of small ion-to-electron temperature ratio and of flow speed hypersonic with respect to the ions but not with respect to the electrons. It is found that waves are excited even if the flow is subacoustic (flow velocity less than the ion-acoustic speed). For both superacoustic and subacoustic velocities a steep wave front develops separating the weakly perturbed, quasineutral plasma ahead, from the region behind where ion waves appear. Near the axis a trailing front develops;the region between this and the axis is quasineutral for superacoustic speeds. The decay laws in all of these regions, the self-similar structure of the fronts and the general character of the waves are determined.The damping of the waves and special flow detail for bodies large and small compared with the Debye length are discussed. A nonlinear analysis of the leading wave front in superacoustic flow is carried out. A hyperacoustic equivalence principle is presented.

Advances in global instability computations: from incompressible to hypersonic flow

Esta tesis constituye un gran avance en el conocimiento del estudio y análisis de inestabilidades hidrodinámicas desde un punto de vista físico y teórico, como consecuencia de haber desarrollado innovadoras técnicas para la resolución computacional eficiente y precisa de la parte principal del espectro correspondiente a los problemas de autovalores (EVP) multidimensionales que gobiernan la inestabilidad de flujos con dos o tres direcciones espaciales inhomogéneas, denominados problemas de estabilidad global lineal. En el contexto del trabajo de desarrollo de herramientas computacionales presentado en la tesis, la discretización mediante métodos de diferencias finitas estables de alto orden de los EVP bidimensionales y tridimensionales que se derivan de las ecuaciones de Navier-Stokes linealizadas sobre flujos con dos o tres direcciones espaciales inhomogéneas, ha permitido una aceleración de cuatro órdenes de magnitud en su resolución. Esta mejora de eficiencia numérica se ha conseguido gracias al hecho de que usando estos esquemas de diferencias finitas, técnicas eficientes de resolución de problemas lineales son utilizables, explotando el alto nivel de dispersión o alto número de elementos nulos en las matrices involucradas en los problemas tratados. Como más notable consecuencia cabe destacar que la resolución de EVPs multidimensionales de inestabilidad global, que hasta la fecha necesitaban de superordenadores, se ha podido realizar en ordenadores de sobremesa. Además de la solución de problemas de estabilidad global lineal, el mencionado desarrollo numérico facilitó la extensión de las ecuaciones de estabilidad parabolizadas (PSE) lineales y no lineales para analizar la inestabilidad de flujos que dependen fuertemente en dos direcciones espaciales y suavemente en la tercera con las ecuaciones de estabilidad parabolizadas tridimensionales (PSE-3D). Precisamente la capacidad de extensión del novedoso algoritmo PSE-3D para el estudio de interacciones no lineales de los modos de estabilidad, desarrollado íntegramente en esta tesis, permite la predicción de transición en flujos complejos de gran interés industrial y por lo tanto extiende el concepto clásico de PSE, el cuál ha sido empleado exitosamente durante las pasadas tres décadas en el mismo contexto para problemas de capa límite bidimensional. Típicos ejemplos de flujos incompresibles se han analizado en este trabajo sin la necesidad de recurrir a restrictivas presuposiciones usadas en el pasado. Se han estudiado problemas vorticales como es el caso de un vórtice aislado o sistemas de vórtices simulando la estela de alas, en los que la homogeneidad axial no se impone y así se puede considerar la difusión viscosa del flujo. Además, se ha estudiado el chorro giratorio turbulento, cuya inestabilidad se utiliza para mejorar las características de funcionamiento de combustores. En la tesis se abarcan adicionalmente problemas de flujos compresibles. Se presenta el estudio de inestabilidad de flujos de borde de ataque a diferentes velocidades de vuelo. También se analiza la estela formada por un elemento rugoso aislado en capa límite supersónica e hipersónica, mostrando excelentes comparaciones con resultados obtenidos mediante simulación numérica directa. Finalmente, nuevas inestabilidades se han identificado en el flujo hipersónico a Mach 7 alrededor de un cono elíptico que modela el vehículo de pruebas en vuelo HIFiRE-5. Los resultados comparan favorablemente con experimentos en vuelo, lo que subraya aún más el potencial de las metodologías de análisis de estabilidad desarrolladas en esta tesis. ABSTRACT The present thesis constitutes a step forward in advancing the frontiers of knowledge of fluid flow instability from a physical point of view, as a consequence of having been successful in developing groundbreaking methodologies for the efficient and accurate computation of the leading part of the spectrum pertinent to multi-dimensional eigenvalue problems (EVP) governing instability of flows with two or three inhomogeneous spatial directions. In the context of the numerical work presented in this thesis, the discretization of the spatial operator resulting from linearization of the Navier-Stokes equations around flows with two or three inhomogeneous spatial directions by variable-high-order stable finite-difference methods has permitted a speedup of four orders of magnitude in the solution of the corresponding two- and three-dimensional EVPs. This improvement of numerical performance has been achieved thanks to the high-sparsity level offered by the high-order finite-difference schemes employed for the discretization of the operators. This permitted use of efficient sparse linear algebra techniques without sacrificing accuracy and, consequently, solutions being obtained on typical workstations, as opposed to the previously employed supercomputers. Besides solution of the two- and three-dimensional EVPs of global linear instability, this development paved the way for the extension of the (linear and nonlinear) Parabolized Stability Equations (PSE) to analyze instability of flows which depend in a strongly-coupled inhomogeneous manner on two spatial directions and weakly on the third. Precisely the extensibility of the novel PSE-3D algorithm developed in the framework of the present thesis to study nonlinear flow instability permits transition prediction in flows of industrial interest, thus extending the classic PSE concept which has been successfully employed in the same context to boundary-layer type of flows over the last three decades. Typical examples of incompressible flows, the instability of which was analyzed in the present thesis without the need to resort to the restrictive assumptions used in the past, range from isolated vortices, and systems thereof, in which axial homogeneity is relaxed to consider viscous diffusion, as well as turbulent swirling jets, the instability of which is exploited in order to improve flame-holding properties of combustors. The instability of compressible subsonic and supersonic leading edge flows has been solved, and the wake of an isolated roughness element in a supersonic and hypersonic boundary-layer has also been analyzed with respect to its instability: excellent agreement with direct numerical simulation results has been obtained in all cases. Finally, instability analysis of Mach number 7 ow around an elliptic cone modeling the HIFiRE-5 flight test vehicle has unraveled flow instabilities near the minor-axis centerline, results comparing favorably with flight test predictions.

Home automation controller for a water-flow window

Facing the EU energy efficiency and legal scenarios related to buildings (2010/31 EU directive), new sustainable advanced concepts for envelopes are required. These innovative designs must be able to offer an elevated level of energy efficiency based on a high performance architecture. According to this, smart glazings, and particularly active water-flow glazings, represent a promising alternative to other solar control glazings, since they can reduce the building energy demand avoiding well known drawbacks as high cost, glare problems and high response time that affect to other smart glazings. This kind of glazing, as any other active one, needs to be operated by a control system. In order to operate a water-flow based window, a new controller based on an inexpensive microcontroller board has been developed

Molecular Dynamics Simulations of Couette flow

The first steps towards developing a continuum-molecular coupled simulations techniques are presented, for the purpose of computing macroscopic systems of confined fluids. The idea is to compute the interface wall-fluid by Molecular Dynamics simulations, where Lennard-Jones potential (and others) have been employed for the molecular interactions, so the usual non slip boundary condition is not specified. Instead, a shear rate can be imposed at the wall, which allows to obtain the properties of the wall material by means of an iterative method. The remaining fluid region will be computed by a spectral hp method. We present MD simulations of a Couette flow, and the results of the developed boundary conditions from the wall fluid interaction.

Control estadístico de la calibración de MDP volumétricos para la transferencia de custodia de hidrocarburos líquidos

Este proyecto tiene por objeto desarrollar una sistemática de control metrológico para vigilar la exactitud de los medidores volumétricos de desplazamiento positivo que operan en las compañías logísticas de hidrocarburos para la transferencia de custodia que están en el cargadero y se ensayan in situ para obtener su meter factor. El punto de partida son las hojas primarias de las calibraciones generadas frente a sus patrones y el prover que nos facilitan las compañías. Dado el elevado número de ensayos y debido a que estos medidores no tienen gráficos de control estables, el enfoque del tratamiento ha sido un etiquetado para realizar un control de inestabilidad y calidad de los ensayos y así, determinar equipos anómalos. Para la búsqueda de equipos atípicos se ha desarrollado el filtro de Tukey para el estudio de la estadística descriptiva de los valores del meter factor. Entre los dos métodos se han obtenido una clasificación de equipos vigilables, recalibrables y sustituibles para facilitar a las compañías logísticas. ABSTRACT The aim of this project is to develop a systematic metrological control to monitor the accuracy of the positive displacement flow meters operating in oil logistics companies for custody transfer which are in the loading track facilities and it are tested in-situ to obtain the meter factor. Due to the high number of assays that meters don´t have stable graphics of control, the approach of data processing has been a labeled to perform an instability and quality control of assays for establish anomalous meters. To find outliers meters is developed the filter of Turkey to study the descriptive statistics of meter factor values. Between both analytical methods is obtained a classification of controllable, recalibrables and replaceable meters to provide to the logistic company.

Diseño electrónico de la tarjeta de interfaz y control para un equipo de seguimiento en elevación en un subsistema de contramedidas electrónicas

Como apoyo al Subsistema ECM tradicional de los sistemas de Guerra Electrónica, surge el Equipo de Seguimiento en Elevación cuyo fin es la búsqueda de la amenaza en elevación. Ante la necesidad de un mayor número de líneas entre los bloques internos de este Equipo de Seguimiento, se hace necesario el diseño de una Tarjeta de Interfaz y Control. La tarjeta se ocupará de realizar el control de datos y flujo de señales de módulos RF que componen el Equipo, haciendo de interfaz entre las Tarjetas Procesadoras y Digitalizadoras, así como entre la Tarjeta de Proceso y el Bloque de Recepción. Una vez que se haya realizado el análisis de la necesidad de controlar estas señales, estudiado las especificaciones y los requisitos funcionales del Sistema, se procederá a implementar el diseño hardware y desarrollo firmware de la Tarjeta de Interfaz y Control de un Equipo de Seguimiento en Elevación para un Subsistema ECM, que constituye el objetivo de este PFC. ABSTRACT. In order to find a threat on elevation, and as a support on the basic ECM subsystems of E-war systems, the Elevation Tracking Equipment appears. To the need of a bigger number of lines between inside blocks of this Tracking Equipment, the design of an Interface and Control Board is needed. This board will deal with the data control and with the flow of RF modules signals that set up the Equipment, and will also work as an interface between the Processing and Digitalizing Board, as well as between the Process Board and the Reception Block. Once the signal control necessity analysis has been made, and once the specifications and functional System requirements have been studied, the hardware design and the firmware development will be ran as a target of PFC.

Resilient Wireless Sensor Networks Using Topology Control: A Review

Wireless sensor networks (WSNs) may be deployed in failure-prone environments, and WSNs nodes easily fail due to unreliable wireless connections, malicious attacks and resource-constrained features. Nevertheless, if WSNs can tolerate at most losing k − 1 nodes while the rest of nodes remain connected, the network is called k − connected. k is one of the most important indicators for WSNs’ self-healing capability. Following a WSN design flow, this paper surveys resilience issues from the topology control and multi-path routing point of view. This paper provides a discussion on transmission and failure models, which have an important impact on research results. Afterwards, this paper reviews theoretical results and representative topology control approaches to guarantee WSNs to be k − connected at three different network deployment stages: pre-deployment, post-deployment and re-deployment. Multi-path routing protocols are discussed, and many NP-complete or NP-hard problems regarding topology control are identified. The challenging open issues are discussed at the end. This paper can serve as a guideline to design resilient WSNs.