From Secondary School To University: Attracting Young Students Towards A Career In Nuclear

From its creation, Spanish Young Generation in Nuclear (Jóvenes Nucleares, JJNN), a non-profit organization that depends on the Spanish Nuclear Society (SNE), has as an important scope to help spread knowledge about nuclear energy, not only pointing out its advantages and its role in our society, but also trying to correct some of the ideas that are due to the biased information and to the lack of knowledge. To try to have success in that goal, some high school lectures were taught and it has been organized regularly a Basic Course on Nuclear Science and Technology

Motivating Young Students to Start a Career in Nuclear: The Basic Course of Science and Nuclear Technology, An Educational Activity of Spanish Young Generation in Nuclear (JÓVENES NUCLEARES)

The main objective of this course, conducted by Jóvenes Nucleares (Spanish Young Generation in Nuclear, JJNN), a non-profit organization that depends on the Spanish Nuclear Society (SNE) is to pass on basic knowledge about Science and Nuclear Technology to the general public, mostly students and introduce them to its most relevant points. The purposes of this course are to provide general information, to answer the most common questions about Nuclear Energy and to motivate the young students to start a career in nuclear. Therefore, it is directed mainly to high school and university students, but also to general people that wants to learn about the key issues of such an important matter in our society. Anybody could attend the course, as no specific scientific education is required. The course is done at least once a year, during the Annual Meeting of the Spanish Nuclear Society, which takes place in a different Spanish city each time. The course is done also to whichever university or institution that asks for it to JJNN, with the only limit of the presenter´s availability. The course is divided into the following chapters: Physical nuclear and radiation principles, Nuclear power plants, Nuclear safety, Nuclear fuel, Radioactive waste, Decommission of nuclear facilities, Future nuclear power plants, Other uses of nuclear technology, Nuclear energy, climate change and sustainable development. The course is divided into 15 minutes lessons on the above topics, imparted by young professionals, experts in the field that belongs either to the Spanish Young Generation in Nuclear, either to companies and institutions related with nuclear energy. At the end of the course, a 200 pages book with the contents of the course is handed to every member of the audience. This book is also distributed in other course editions at high schools and universities in order to promote the scientific dissemination of the Nuclear Technology. As an extra motivation, JJNN delivers a course certificate to the assistants. At the end of the last edition course, in Santiago de Compostela, the assistants were asked to provide a feedback about it. Some really interesting lessons were learned, that will be very useful to improve next editions of the course. As a general conclusion of the courses it can be said that many of the students that have assisted to the course have increased their motivation in the nuclear field, and hopefully it will help the young talents to choose the nuclear field to develop their careers

Understanding time-drift for different aircraft descent guidance strategies

In this paper the effect of different aircraft automated descent guidance strategies on fuel burn and the temporal predictability of the executed trajectory is investigated. The paper aims to provide an understanding of how airborne automation can be permitted by Air Traffic Control to remain in control of the descent in the presence of disturbances while providing sufficient predictability. Simulations have been performed investigating different guidance strategies. While each strategy has its advantages and disadvantages, results indicate that improved temporal predictability comes at the cost of additional fuel burn and loss of predictability in other dimensions of the trajectory.

Automatic generation of real-time deformable parametric model of the aorta for a VR-based catheterism guidance system

The purpose of this work is twofold: first, to develop a process to automatically create parametric models of the aorta that can adapt to any possible intraoperative deformation of the vessel. Second, it intends to provide the tools needed to perform this deformation in real time, by means of a non-rigid registration method. This dynamically deformable model will later be used in a VR-based surgery guidance system for aortic catheterism procedures, showing the vessel changes in real time.

Guidance for the development of accessibility evaluation tools following the Unified Software Development Process

Automated and semi-automated accessibility evaluation tools are key to streamline the process of accessibility assessment, and ultimately ensure that software products, contents, and services meet accessibility requirements. Different evaluation tools may better fit different needs and concerns, accounting for a variety of corporate and external policies, content types, invocation methods, deployment contexts, exploitation models, intended audiences and goals; and the specific overall process where they are introduced. This has led to the proliferation of many evaluation tools tailored to specific contexts. However, tool creators, who may be not familiar with the realm of accessibility and may be part of a larger project, lack any systematic guidance when facing the implementation of accessibility evaluation functionalities. Herein we present a systematic approach to the development of accessibility evaluation tools, leveraging the different artifacts and activities of a standardized development process model (the Unified Software Development Process), and providing templates of these artifacts tailored to accessibility evaluation tools. The work presented specially considers the work in progress in this area by the W3C/WAI Evaluation and Report Working Group (ERT WG)

Design and kinematic analysis of 3PSS-1S wrist for needle insertion guidance

In this work it is presented a complete kinematic analysis of the 3PSS-1S parallel mechanism for its implementation as a spherical wrist for a needle insertion guidance robot. The spherical 3PSS-1S mechanism is a low weight and reduced dimension parallel mechanism that allows spherical movements providing the requirements needed for the serial–parallel robotic arm for needle insertion guidance. The solution of its direct kinematic is computed with a numerical method based on the Newton–Raphson formulation and a constraint function of the mechanism. The input–output velocity equation is obtained with the use of screw theory. Three types of singular postures are identified during simulations and verified in the real prototype. The 3PSS-1S can perform pure rotations of ±45°±45°, ±40°±40°, ±60°±60° along the View the MathML sourcex, View the MathML sourcey, View the MathML sourcez axes respectively.

iCarer Project: Intelligent Care Guidance and Learning Services Platform for Informal Carers of the Elderly

The increasing ageing population is demanding new care approaches to maintain the quality of life of elderly people. Informal carers are becoming crucial agents in the care and support of elderly people, which can lead to those carers suffering from additional stress due to competing priorities with employment or due to lack of knowledge about elderly people?s care needs. Thus, support and stress relief in carers should be a key issue in the home-care process of these older adults. Considering this context, this work presents the iCarer project aimed at developing a personalized and adaptive platform to offer informal carers support by means of monitoring their activities of daily care and psychological state, as well as providing an orientation to help them improve the care provided. Additionally, iCarer will provide e-Learning services and an informal carers learning network. As a result, carers will be able to expand their knowledge, supported by the experience provided by expert counsellors and fellow carers. Additionally, the coordination between formal and informal carers will be improved, offering the informal carers flexibility to organize and combine their assistance and social activities.

Diseño de un instrumento de evaluación de la gestión de recursos humanos. Aplicación en pymes industriales

El punto de partida para que una empresa mejore su competitividad es la evaluación de su gestión; para ello, es necesario contar con instrumentos que de manera objetiva, evalúen la gestión y proporcionen una guía para la mejora continua de los procesos. Este trabajo de investigación presenta el diseño y aplicación de un instrumento para evaluar la gestión de recursos humanos en las pymes industriales. Es un instrumento adaptado a la cultura, mercado, características y especificidades propias de las pymes del sector industrial del Estado Bolívar, Venezuela. Los items de evaluación fueron divididos en cuatro bloques de acuerdo al ciclo Planificar, Hacer, Verificar, Actuar y su validación estadística fue realizada mediante la técnica de análisis multivariante. Una vez validada, se aplicó la herramienta a trescientos setenta y cinco individuos del área de Recursos Humanos en ciento veinticinco Pymes industriales. Los resultados indican que los aspectos de tipo funcional son los que conducen la gestión en lugar de las razones estratégicas de la empresa, y en general, no existe plan de carrera ni sistema de evaluación de desempeño. La caracterización aportada por este estudio permite a las empresas evaluadas conocer cuales son los factores a mejorar en su gestión.The starting point for a company to improve its competitiveness is the evaluation of their management; for this it is necessary to have instruments that objectively evaluate and provide management guidance for continuous process improvement. This research paper presents the design and implementation of a tool to assess the human resource management in industrial SMEs. It is an instrument adapted to the culture, market characteristics and needs of SMEs in the Bolivar State, Venezuela. The evaluation items were divided into four blocks according to the Plan, Do, Check, Act cycle and its statistical validation was performed using the technique of multivariate analysis. Once validated, the tool was applied to hundred seventy five individuals of Human Resources belonging to hundred twenty five industrial SMEs. The results indicate that aspects of functional type are the leading management rather than strategic reasons, and in general, there is no career plan and system performance evaluation. The characterization provided by this study evaluated allows companies to know what factors to improve their management.

Optimization of the Integrated Guidance and Control for a Dual Aerodynamic Control Missile

Las futuras misiones para misiles aire-aire operando dentro de la atmósfera requieren la interceptación de blancos a mayores velocidades y más maniobrables, incluyendo los esperados vehículos aéreos de combate no tripulados. La intercepción tiene que lograrse desde cualquier ángulo de lanzamiento. Una de las principales discusiones en la tecnología de misiles en la actualidad es cómo satisfacer estos nuevos requisitos incrementando la capacidad de maniobra del misil y en paralelo, a través de mejoras en los métodos de guiado y control modernos. Esta Tesis aborda estos dos objetivos simultáneamente, al proponer un diseño integrando el guiado y el control de vuelo (autopiloto) y aplicarlo a misiles con control aerodinámico simultáneo en canard y cola. Un primer avance de los resultados obtenidos ha sido publicado recientemente en el Journal of Aerospace Engineering, en Abril de 2015, [Ibarrondo y Sanz-Aranguez, 2015]. El valor del diseño integrado obtenido es que permite al misil cumplir con los requisitos operacionales mencionados empleando únicamente control aerodinámico. El diseño propuesto se compara favorablemente con esquemas más tradicionales, consiguiendo menores distancias de paso al blanco y necesitando de menores esfuerzos de control incluso en presencia de ruidos. En esta Tesis se demostrará cómo la introducción del doble mando, donde tanto el canard como las aletas de cola son móviles, puede mejorar las actuaciones de un misil existente. Comparado con un misil con control en cola, el doble control requiere sólo introducir dos servos adicionales para accionar los canards también en guiñada y cabeceo. La sección de cola será responsable de controlar el misil en balanceo mediante deflexiones diferenciales de los controles. En el caso del doble mando, la complicación añadida es que los vórtices desprendidos de los canards se propagan corriente abajo y pueden incidir sobre las superficies de cola, alterando sus características de control. Como un primer aporte, se ha desarrollado un modelo analítico completo para la aerodinámica no lineal de un misil con doble control, incluyendo la caracterización de este efecto de acoplamiento aerodinámico. Hay dos modos de funcionamiento en picado y guiñada para un misil de doble mando: ”desviación” y ”opuesto”. En modo ”desviación”, los controles actúan en la misma dirección, generando un cambio inmediato en la sustentación y produciendo un movimiento de translación en el misil. La respuesta es rápida, pero en el modo ”desviación” los misiles con doble control pueden tener dificultades para alcanzar grandes ángulos de ataque y altas aceleraciones laterales. Cuando los controles actúan en direcciones opuestas, el misil rota y el ángulo de ataque del fuselaje se incrementa para generar mayores aceleraciones en estado estacionario, aunque el tiempo de respuesta es mayor. Con el modelo aerodinámico completo, es posible obtener una parametrización dependiente de los estados de la dinámica de corto periodo del misil. Debido al efecto de acoplamiento entre los controles, la respuesta en bucle abierto no depende linealmente de los controles. El autopiloto se optimiza para obtener la maniobra requerida por la ley de guiado sin exceder ninguno de los límites aerodinámicos o mecánicos del misil. Una segunda contribución de la tesis es el desarrollo de un autopiloto con múltiples entradas de control y que integra la aerodinámica no lineal, controlando los tres canales de picado, guiñada y cabeceo de forma simultánea. Las ganancias del autopiloto dependen de los estados del misil y se calculan a cada paso de integración mediante la resolución de una ecuación de Riccati de orden 21x21. Las ganancias obtenidas son sub-óptimas, debido a que una solución completa de la ecuación de Hamilton-Jacobi-Bellman no puede obtenerse de manera práctica, y se asumen ciertas simplificaciones. Se incorpora asimismo un mecanismo que permite acelerar la respuesta en caso necesario. Como parte del autopiloto, se define una estrategia para repartir el esfuerzo de control entre el canard y la cola. Esto se consigue mediante un controlador aumentado situado antes del bucle de optimización, que minimiza el esfuerzo total de control para maniobrar. Esta ley de alimentación directa mantiene al misil cerca de sus condiciones de equilibrio, garantizando una respuesta transitoria adecuada. El controlador no lineal elimina la respuesta de fase no-mínima característica de la cola. En esta Tesis se consideran dos diseños para el guiado y control, el control en Doble-Lazo y el control Integrado. En la aproximación de Doble-Lazo, el autopiloto se sitúa dentro de un bucle interior y se diseña independientemente del guiado, que conforma el bucle más exterior del control. Esta estructura asume que existe separación espectral entre los dos, esto es, que los tiempos de respuesta del autopiloto son mucho mayores que los tiempos característicos del guiado. En el estudio se combina el autopiloto desarrollado con una ley de guiado óptimo. Los resultados obtenidos demuestran que se consiguen aumentos muy importantes en las actuaciones frente a misiles con control canard o control en cola, y que la interceptación, cuando se lanza cerca del curso de colisión, se consigue desde cualquier ángulo alrededor del blanco. Para el misil de doble mando, la estrategia óptima resulta en utilizar el modo de control opuesto en la aproximación al blanco y utilizar el modo de desviación justo antes del impacto. Sin embargo la lógica de doble bucle no consigue el impacto cuando hay desviaciones importantes con respecto al curso de colisión. Una de las razones es que parte de la demanda de guiado se pierde, ya que el misil solo es capaz de modificar su aceleración lateral, y no tiene control sobre su aceleración axial, a no ser que incorpore un motor de empuje regulable. La hipótesis de separación mencionada, y que constituye la base del Doble-Bucle, puede no ser aplicable cuando la dinámica del misil es muy alta en las proximidades del blanco. Si se combinan el guiado y el autopiloto en un único bucle, la información de los estados del misil está disponible para el cálculo de la ley de guiado, y puede calcularse la estrategia optima de guiado considerando las capacidades y la actitud del misil. Una tercera contribución de la Tesis es la resolución de este segundo diseño, la integración no lineal del guiado y del autopiloto (IGA) para el misil de doble control. Aproximaciones anteriores en la literatura han planteado este sistema en ejes cuerpo, resultando en un sistema muy inestable debido al bajo amortiguamiento del misil en cabeceo y guiñada. Las simplificaciones que se tomaron también causan que el misil se deslice alrededor del blanco y no consiga la intercepción. En nuestra aproximación el problema se plantea en ejes inerciales y se recurre a la dinámica de los cuaterniones, eliminado estos inconvenientes. No se limita a la dinámica de corto periodo del misil, porque se construye incluyendo de modo explícito la velocidad dentro del bucle de optimización. La formulación resultante en el IGA es independiente de la maniobra del blanco, que sin embargo se ha de incluir en el cálculo del modelo en Doble-bucle. Un típico inconveniente de los sistemas integrados con controlador proporcional, es el problema de las escalas. Los errores de guiado dominan sobre los errores de posición del misil y saturan el controlador, provocando la pérdida del misil. Este problema se ha tratado aquí con un controlador aumentado previo al bucle de optimización, que define un estado de equilibrio local para el sistema integrado, que pasa a actuar como un regulador. Los criterios de actuaciones para el IGA son los mismos que para el sistema de Doble-Bucle. Sin embargo el problema matemático resultante es muy complejo. El problema óptimo para tiempo finito resulta en una ecuación diferencial de Riccati con condiciones terminales, que no puede resolverse. Mediante un cambio de variable y la introducción de una matriz de transición, este problema se transforma en una ecuación diferencial de Lyapunov que puede resolverse mediante métodos numéricos. La solución resultante solo es aplicable en un entorno cercano del blanco. Cuando la distancia entre misil y blanco es mayor, se desarrolla una solución aproximada basada en la solución de una ecuación algebraica de Riccati para cada paso de integración. Los resultados que se han obtenido demuestran, a través de análisis numéricos en distintos escenarios, que la solución integrada es mejor que el sistema de Doble-Bucle. Las trayectorias resultantes son muy distintas. El IGA preserva el guiado del misil y consigue maximizar el uso de la propulsión, consiguiendo la interceptación del blanco en menores tiempos de vuelo. El sistema es capaz de lograr el impacto donde el Doble-Bucle falla, y además requiere un orden menos de magnitud en la cantidad de cálculos necesarios. El efecto de los ruidos radar, datos discretos y errores del radomo se investigan. El IGA es más robusto, resultando menos afectado por perturbaciones que el Doble- Bucle, especialmente porque el núcleo de optimización en el IGA es independiente de la maniobra del blanco. La estimación de la maniobra del blanco es siempre imprecisa y contaminada por ruido, y degrada la precisión de la solución de Doble-Bucle. Finalmente, como una cuarta contribución, se demuestra que el misil con guiado IGA es capaz de realizar una maniobra de defensa contra un blanco que ataque por su cola, sólo con control aerodinámico. Las trayectorias estudiadas consideran una fase pre-programada de alta velocidad de giro, manteniendo siempre el misil dentro de su envuelta de vuelo. Este procedimiento no necesita recurrir a soluciones técnicamente más complejas como el control vectorial del empuje o control por chorro para ejecutar esta maniobra. En todas las demostraciones matemáticas se utiliza el producto de Kronecker como una herramienta practica para manejar las parametrizaciones dependientes de variables, que resultan en matrices de grandes dimensiones. ABSTRACT Future missions for air to air endo-atmospheric missiles require the interception of targets with higher speeds and more maneuverable, including forthcoming unmanned supersonic combat vehicles. The interception will need to be achieved from any angle and off-boresight launch conditions. One of the most significant discussions in missile technology today is how to satisfy these new operational requirements by increasing missile maneuvering capabilities and in parallel, through the development of more advanced guidance and control methods. This Thesis addresses these two objectives by proposing a novel optimal integrated guidance and autopilot design scheme, applicable to more maneuverable missiles with forward and rearward aerodynamic controls. A first insight of these results have been recently published in the Journal of Aerospace Engineering in April 2015, [Ibarrondo and Sanz-Aránguez, 2015]. The value of this integrated solution is that it allows the missile to comply with the aforementioned requirements only by applying aerodynamic control. The proposed design is compared against more traditional guidance and control approaches with positive results, achieving reduced control efforts and lower miss distances with the integrated logic even in the presence of noises. In this Thesis it will be demonstrated how the dual control missile, where canard and tail fins are both movable, can enhance the capabilities of an existing missile airframe. Compared to a tail missile, dual control only requires two additional servos to actuate the canards in pitch and yaw. The tail section will be responsible to maintain the missile stabilized in roll, like in a classic tail missile. The additional complexity is that the vortices shed from the canard propagate downstream where they interact with the tail surfaces, altering the tail expected control characteristics. These aerodynamic phenomena must be properly described, as a preliminary step, with high enough precision for advanced guidance and control studies. As a first contribution we have developed a full analytical model of the nonlinear aerodynamics of a missile with dual control, including the characterization of this cross-control coupling effect. This development has been produced from a theoretical model validated with reliable practical data obtained from wind tunnel experiments available in the scientific literature, complement with computer fluid dynamics and semi-experimental methods. There are two modes of operating a missile with forward and rear controls, ”divert” and ”opposite” modes. In divert mode, controls are deflected in the same direction, generating an increment in direct lift and missile translation. Response is fast, but in this mode, dual control missiles may have difficulties in achieving large angles of attack and high level of lateral accelerations. When controls are deflected in opposite directions (opposite mode) the missile airframe rotates and the body angle of attack is increased to generate greater accelerations in steady-state, although the response time is larger. With the aero-model, a state dependent parametrization of the dual control missile short term dynamics can be obtained. Due to the cross-coupling effect, the open loop dynamics for the dual control missile is not linearly dependent of the fin positions. The short term missile dynamics are blended with the servo system to obtain an extended autopilot model, where the response is linear with the control fins turning rates, that will be the control variables. The flight control loop is optimized to achieve the maneuver required by the guidance law without exceeding any of the missile aerodynamic or mechanical limitations. The specific aero-limitations and relevant performance indicators for the dual control are set as part of the analysis. A second contribution of this Thesis is the development of a step-tracking multi-input autopilot that integrates non-linear aerodynamics. The designed dual control missile autopilot is a full three dimensional autopilot, where roll, pitch and yaw are integrated, calculating command inputs simultaneously. The autopilot control gains are state dependent, and calculated at each integration step solving a matrix Riccati equation of order 21x21. The resulting gains are sub-optimal as a full solution for the Hamilton-Jacobi-Bellman equation cannot be resolved in practical terms and some simplifications are taken. Acceleration mechanisms with an λ-shift is incorporated in the design. As part of the autopilot, a strategy is defined for proper allocation of control effort between canard and tail channels. This is achieved with an augmented feed forward controller that minimizes the total control effort of the missile to maneuver. The feedforward law also maintains the missile near trim conditions, obtaining a well manner response of the missile. The nonlinear controller proves to eliminate the non-minimum phase effect of the tail. Two guidance and control designs have been considered in this Thesis: the Two- Loop and the Integrated approaches. In the Two-Loop approach, the autopilot is placed in an inner loop and designed separately from an outer guidance loop. This structure assumes that spectral separation holds, meaning that the autopilot response times are much higher than the guidance command updates. The developed nonlinear autopilot is linked in the study to an optimal guidance law. Simulations are carried on launching close to collision course against supersonic and highly maneuver targets. Results demonstrate a large boost in performance provided by the dual control versus more traditional canard and tail missiles, where interception with the dual control close to collision course is achieved form 365deg all around the target. It is shown that for the dual control missile the optimal flight strategy results in using opposite control in its approach to target and quick corrections with divert just before impact. However the Two-Loop logic fails to achieve target interception when there are large deviations initially from collision course. One of the reasons is that part of the guidance command is not followed, because the missile is not able to control its axial acceleration without a throttleable engine. Also the separation hypothesis may not be applicable for a high dynamic vehicle like a dual control missile approaching a maneuvering target. If the guidance and autopilot are combined into a single loop, the guidance law will have information of the missile states and could calculate the most optimal approach to the target considering the actual capabilities and attitude of the missile. A third contribution of this Thesis is the resolution of the mentioned second design, the non-linear integrated guidance and autopilot (IGA) problem for the dual control missile. Previous approaches in the literature have posed the problem in body axes, resulting in high unstable behavior due to the low damping of the missile, and have also caused the missile to slide around the target and not actually hitting it. The IGA system is posed here in inertial axes and quaternion dynamics, eliminating these inconveniences. It is not restricted to the missile short term dynamic, and we have explicitly included the missile speed as a state variable. The IGA formulation is also independent of the target maneuver model that is explicitly included in the Two-loop optimal guidance law model. A typical problem of the integrated systems with a proportional control law is the problem of scales. The guidance errors are larger than missile state errors during most of the flight and result in high gains, control saturation and loss of control. It has been addressed here with an integrated feedforward controller that defines a local equilibrium state at each flight point and the controller acts as a regulator to minimize the IGA states excursions versus the defined feedforward state. The performance criteria for the IGA are the same as in the Two-Loop case. However the resulting optimization problem is mathematically very complex. The optimal problem in a finite-time horizon results in an irresoluble state dependent differential Riccati equation with terminal conditions. With a change of variable and the introduction of a transition matrix, the equation is transformed into a time differential Lyapunov equation that can be solved with known numerical methods in real time. This solution results range limited, and applicable when the missile is in a close neighborhood of the target. For larger ranges, an approximate solution is used, obtained from solution of an algebraic matrix Riccati equation at each integration step. The results obtained show, by mean of several comparative numerical tests in diverse homing scenarios, than the integrated approach is a better solution that the Two- Loop scheme. Trajectories obtained are very different in the two cases. The IGA fully preserves the guidance command and it is able to maximize the utilization of the missile propulsion system, achieving interception with lower miss distances and in lower flight times. The IGA can achieve interception against off-boresight targets where the Two- Loop was not able to success. As an additional advantage, the IGA also requires one order of magnitude less calculations than the Two-Loop solution. The effects of radar noises, discrete radar data and radome errors are investigated. IGA solution is robust, and less affected by radar than the Two-Loop, especially because the target maneuvers are not part of the IGA core optimization loop. Estimation of target acceleration is always imprecise and noisy and degrade the performance of the two-Loop solution. The IGA trajectories are such that minimize the impact of radome errors in the guidance loop. Finally, as a fourth contribution, it is demonstrated that the missile with IGA guidance is capable of performing a defense against attacks from its rear hemisphere, as a tail attack, only with aerodynamic control. The studied trajectories have a preprogrammed high rate turn maneuver, maintaining the missile within its controllable envelope. This solution does not recur to more complex features in service today, like vector control of the missile thrust or side thrusters. In all the mathematical treatments and demonstrations, the Kronecker product has been introduced as a practical tool to handle the state dependent parametrizations that have resulted in very high order matrix equations.

Rem : a los dos lados del espejo = (Rem at both sides of the mirror)

Cuando se trata de Rem Koolhaas, su espejo no refleja una sola imagen sino múltiples, es un prisma poliédrico. Su espejo nos devuelve el Rem mediático, el intelectual, el conceptualizador, el constructor, el analista, el periodista, el actor... En el caso de esta investigación, fijamos el punto de mira en el Rem COMUNICADOR. “Rem a los dos lados del espejo” se enmarca en una investigación sobre los medios de comunicación de arquitectura, su reflejo en la producción arquitectónica y viceversa. Se trata de llegar a discernir si comunicación y producción arquitectónica colisionan y confluyen en el caso de grandes comunicadores como Rem Koolhaas, si el mensaje y el medio transmisor adquieren las mismas cualidades. Centrándose en la figura de Rem Koolhaas, la tesis aborda la evolución de su faceta comunicativa y las transformaciones sucesivas en el campo de la comunicación arquitectónica, en paralelo a su evolución conceptual a lo largo de su trayectoria. La investigación, por tanto, no se centra tanto en su componente teórica o en la práctica arquitectónica de OMA, sino en la exposición de su producción al mundo, especialmente a través de sus ensayos y libros. “Delirious New York” y “SMLXL” son un reflejo del momento conceptual en que se inscriben, y contienen mucha información sobre los referentes gráficos que irremediablemente han influido en su composición. Especialmente, la aparición de “SMLXL” supuso un revulsivo para el mundo de la comunicación arquitectónica, porque puso el foco sobre la importancia de dejar atrás un discurso narrativo linea y unifocal, para afrontar la comunicación barajando múltiples variables, y aproximaciones, en un proceso similar al desarrollo de un proyecto de arquitectura. Presenta un diseño muy novedoso y una edición extremadamente cuidada, que atiende a parámetros mucho más ambiciosos que los meramente narrativos. Profundiza en la necesidad de una temática global, planteando cuál es la aproximación más apropiada para cada uno de los proyectos que describe, transmitiendo al lector una percepción más allá de lo estrictamente visual, más próximo a lo sensorial. Además, su enorme repercusión a nivel internacional y el gran interés que despertó (no solamente entre los arquitectos, sino también entre diseñadores gráficos, publicistas, personas provenientes de todo tipo de tendencias artísticas y público en general), provocó la globalización del fenómeno de las publicaciones arquitectónicas y puso de manifiesto la importancia de la comunicación como una disciplina en sí misma, dentro de la producción arquitectónica en la era actual. A pesar de la importancia de “SMLXL” a todos los niveles, la presente tesis plantea que, donde realmente se culmina esa experiencia comunicativa, es en “Content”, al incluir nuevos parámetros relacionados con la fusión conceptual de continente y contenido. Es en esta publicación donde el objeto de la comunicación y la expresión de la misma se convierten en un único elemento, que se rige por leyes similares. En este caso, la ley fundamental es la aplicación hasta sus máximas consecuencias de la “cultura de la congestión”, tanto en el mensaje como en el medio, generando lo que hemos convenido en denominar “comunicación congestiva”. Esta concepción deviene en que necesariamente se materialice como un producto efímero, desechable, casi virtual, porque responde a las condiciones de un momento muy concreto y específico y fuera de ese contexto pierde su significación.. La “cultura de la congestión” empieza a surgir en los planteamientos de Koolhaas en la Architectural Association School of Architecture de Londres, bajo la tutela de Elia Zenghelis. Posteriormente se desarrolla en su manifiesto retroactivo sobre Manhattan, “Delirious New York”, donde declara la guerra abierta al urbanismo del movimiento moderno y afirma que la ciudad realmente contemporánea es aquella que es fruto de un desarrollo no planificado, hiperdensa y posible gracias a los avances tecnológicos de su era. Finalmente comienza a materializarse en la Diploma Unit 9 de la AA, donde entra como profesor en 1975, dejando una huella indeleble en las generaciones posteriores de arquitectos que pasaron dicha unidad. Rem Koolhaas es ante todo un intelectual y por ello, todo el constructo teórico sobre la metrópolis comienza a reflejarse en su obra a través de OMA desde el comienzo de su producción. Podemos decir a grandes rasgos que su carrera está marcada por dos hitos históricos fundamentales que determinan tres etapas diferenciadas en su producción. En sus primeros años de profesión, Koolhaas sigue fascinado por la metrópolis urbana y la aplicación del método paranoico crítico a su producción arquitectónica. Es un arquitecto profundamente surrealista. Entiende este método como una estrategia de conocimiento y aproximación al mundo que le rodea: “dejar salir el inconsciente pero sostenerlo con las muletas de la racionalidad”. Pero lo que en realidad le interesa es su aplicación a la gran escala, el “Bigness”, y por ello, participa en proyectos muy ambiciosos de los que surgen conceptos que, más allá de resultar premiados o no, han dejado una huella ideológica en el devenir de la arquitectura. Entre estos proyectos, cabe destacar su propuesta para el Parque de la Villette o la Très Grande Bibliotèque de París. Sus proyectos de esta época destilan una gran carga conceptual, que devienen en unos interiores sorprendentes pero una apariencia exterior sobria o incluso podríamos decir "povera", por el uso de materiales efímeros, poco habituales en la macro-arquitectura hasta ese momento. Súbitamente, en 1997, explotó el denominado “Efecto Bilbao”, de la mano de Frank Gehry (1). El Museo Guggenheim de Bilbao, con su espectacularidad, sus formas pregnantes e imposibles, impacta al mundo. Nace la era de la “Arquitectura del Espectáculo”; la transformación de la ciudad a través de ICONOS que actúen como nodos de atracción y concentración en torno a los cuales supuestamente se revitaliza la actividad económica, cultural y sociopolítica de la ciudad, como si a través de un único gesto se pudieran regenerar todos los tejidos internos de la urbe. Rem Koolhaas comprende rápidamente que la aproximación a la ciudad ha cambiado y, sobre todo, el mercado. En el mundo de la globalización, la única manera de llegar a materializar el “Bigness”, es encerrando sus ejercicios intelectuales en formas pregnantes, bellas, icónicas, espectaculares. Koolhaas encuentra su marca personal en la estética “Stealth”, proveniente de los aviones de combate facetados para evitar los radares, elaborados en los años 80. De esta época surgen proyectos como la Casa da Música de Oporto o la Biblioteca de Seattle; ambos edificios son iconos facetados, de belleza pregnante, que dejan una huella indeleble en la ciudad y provocan, al igual que el Guggenheim, un cierto efecto de recuperación y revitalización en el entorno en que se asientan, al menos de manera temporal. En cualquier caso, Koolhaas nunca abandona los ejercicios meramente teóricos, pero segrega su actividad en dos: OMA produce aquello que tiene vocación de ser construido y se rige por los parámetros del mercado global y AMO, la otra cara del espejo de Rem, aplica el pensamiento arquitectónico a campos no explorados, sin la dependencia de agentes externos, pudiendo permitirse ser un laboratorio puramente experimental. En este escenario, llega el 11 de septiembre de 2001 y el ataque a las Torres Gemelas de Nueva York tiene efectos devastadores a todos los niveles, significando, en un período de tiempo sorprendentemente corto, un cambio en el orden mundial. Rem Koolhaas da entonces un giro de 180 grados, dirige su mirada hacia China, donde entiende que sus aportaciones tienen un beneficio social más directo que en occidente. (2) Para presentar al mundo su nuevo cambio de rumbo y la creación del “Think Tank” AMO, plantea una gran exposición en la NeueGallerie de Berlín bajo el título de “Content”, experiencia paralela a la edición del libro con el mismo título, que inicialmente nace como “catálogo de la exposición, pero que internamente siempre se concibió como el documento más trascendente en el estudio desde “SMLXL”. Sin embargo, en muchos aspectos se trata de su opuesto: una publicación con formato revista, de tapa blanda, con paginado muy fino, formato de "folleto de supermercado" y contenido hiperdenso. Es un experimento efímero, fugaz, ligero, barato, de “usar y tirar”. De hecho, está fuera de stock, ya no se edita. Probablemente Rem Koolhaas desaprobaría que se hiciera una investigación que pusiera el foco sobre el mismo, porque diez años después de su publicación seguramente opine que su vigencia ha caducado. Sin embargo, muestra con una claridad meridiana el estado conceptual y vital de OMA en el momento de su publicación y representa, además un verdadero hito en la comunicación arquitectónica, un punto de no retorno, el máximo exponente de lo que hemos denominado “comunicación congestiva”. La presente tesis plantea que “Content” contiene la esencia de la mayor aportación de Rem Koolhaas al mundo de la arquitectura: la transformación profunda y definitiva de la comunicación arquitectónica mediante la convergencia del estado conceptual y la transmisión del mismo. Su legado arquitectónico y conceptual ha marcado a todas las generaciones posteriores de manera indeleble. Sus ensayos, sus teorías, sus proyectos y sus edificaciones ya pertenecen a la historia de la arquitectura, sin ninguna duda. Pero es su revisión del concepto de la comunicación en arquitectura lo que ha tenido y tendrá un reflejo inmediato en las generaciones futuras, no solamente en la comunicación sino en su arquitectura, a través de un intercambio biyectivo. El planteamiento a futuro sería determinar qué sucede tras “Content”, tras la hiperdensidad máxima, tras la cultura de la congestión visual; qué es lo que propone Koolhaas y qué se va a plantear también en el mundo de la comunicación arquitectónica. Para ello, estudiaremos en profundidad sus últimos proyectos relacionados con la comunicación, como su propuesta para la Biennale de Arquitectura de Venecia de 2014, su intensa investigación sobre el “Metabolismo” en “Project Japan: Metabolism Talks...”, o la dirección de sus últimos planteamientos territoriales. En los últimos tiempos Rem Koolhaas habla de “Preservación”, de “Sobriedad”, de “Esencialismo”, de “Performance”... El autor intelectual de la cultura de la congestión habla ahora de la “low density”...como no podía ser de otra manera en la otra cara del espejo. En definitiva, el color blanco como suma de todos los colores, todas las longitudes de onda del espectro visible recibidas al tiempo. ABSTRACT When talking about Rem Koolhaas, the mirror does not only reflect one but numerous images: it is nothing but a polyhedral prism. His mirror gives us the image of Rem the media celebrity, the intellectual, the conceptualizer, the builder, the analyst, the journalist, the actor... This research sets the spotlight on Rem the COMMUNICATOR. "Rem on both sides of the mirror" belongs to a research on architectural media, its influence on the architectural production and vice versa. It is aimed at getting to discern whether communication and architectural production collide and converge in the case of great communicators such as Rem Koolhaas, and whether the message and transmission media acquire the same features. Focusing on the figure of Rem Koolhaas, this thesis addresses the evolution of his communicative facet and the successive transformations in the field of architectural communication, parallel to the conceptual evolution he underwent throughout his career. Therefore, this research is not so much focused on his theoretical component or on the OMA’s architectural practice, but on the exhibition of his production to the world, especially through his essays and books. "Delirious New York" and "SMLXL" hold up a mirror to the conceptual moment they are part of, and contain a great deal of information about the graphic references that have inevitably influenced his work. Specially, the launch of "SMLXL" was a salutary shock for the architectural communication world, since it set the spotlight on the importance of leaving a linear and unifocal narrative behind in order to face communication considering multiple variables and approaches, based on a process similar to the development of an architectural project. It offers a very innovative design and an extremely careful editing, which deals with parameters much more ambitious than those merely narrative. It explores the need for a global subject and suggests the most appropriate approach for each of the projects described, giving the reader a closer insight to the sensory that goes beyond what’s strictly visual. In addition, its huge international impact and the great interest shown, not only by architects but also by graphic designers, publishers, people from all kinds of artistic trends and the general public, led to the globalisation of the architectural publications phenomenon and brought the importance of communication as a discipline in itself, within the architectural production in the age at hand, to light. Despite the importance of "SMLXL" at all levels, this thesis suggests that the communication experience really culminates in "Content", for it includes new conceptual parameters associated with the container-content conceptual fusion. It is in this book where the purpose of communication and the expression of such become a single element, ruled by similar laws. In this particular case, the fundamental law is to implement the "culture of congestion" to its extreme consequences in both the message and the media, leading to what we have agreed to refer to as "congestive communication”. This concept leads to its inevitable materialisation into an ephemeral, disposable, almost virtual product, because it meets the conditions of a very concrete and specific time, and outside that context it loses its significance. The "culture of congestion" emerged in Koolhaas’ approaches under the guidance of Elia Zenghelis, in the Architectural Association School of Architecture of London. Subsequently, his retroactive manifesto on Manhattan, "Delirious New York" developed it, waging an all-out war against the modern movement urbanism and maintaining that the really contemporary cities are those hyperdense ones that rise as a result of an unplanned development and thanks to the typical technological advances of their time. Finally it began to materialise in the Diploma Unit 9 of the AA, in which he started lecturing in 1975, leaving an indelible mark on subsequent generations of architects who passed that unit. First and foremost, Rem Koolhaas is an intellectual and, therefore, all the theoretical construct in the metropolis began to be reflected in his work through OMA since the beginnings of his production. Broadly speaking, we can say that his career is influenced by two essential historic events, which determine three different stages in his production. In the early years of his career, Koolhaas was still fascinated by the urban metropolis and the implementation of the paranoiac-critical method to his architectural production. He was then a deeply surreal architect. He understood this method as a knowledge strategy and an approach to the world around him: "let the subconscious out but hold it with the crutches of reasonableness”. However, he was actually interested in its implementation on a broad scale, the "Bigness", and therefore, he took part in ambitious projects that led to the accrual of concepts that, beyond being rewarded, left an ideological impression on the evolution of architecture. These projects included his proposal for the Parc de la Villette or the Très Grande Bibliotèque in Paris. The projects he carried out during this period showed a great conceptual background, which evolved into surprising interiors but a sober, or even "povera", exterior appearance, thanks to the use of ephemeral materials that were atypical in the macro-architecture field until that moment. Suddenly, in 1997, the so-called "Bilbao effect" boomed thanks to Frank Gehry (1). The Guggenheim Museum of Bilbao amazed the world with its spectacular nature and its pregnant and impossible shapes. It was the beginning of the era of “The architecture of spectacle”: the transformation of the city through ICONS that would act as nodes of attraction and gathering, around which the economic, cultural and socio-political activity of the city was supposed to be revitalized, as if through a single gesture all internal tissues of the city could be rebuilt. Rem Koolhaas quickly realized that the approach to the city, and especially to the global market, had changed. In the world of globalisation, the only way to get to materialise such "Bigness" was by keeping his intellectual exercises in pregnant, beautiful, iconic and spectacular shapes. Koolhaas found his personal brand in the Stealth aesthetic, resulting from the eighties American combat aircrafts whose shape was faceted in order to avoid radars. Projects such as the Casa da Música in Porto or the Seattle Library date from this period; both buildings are faceted icons of pregnant beauty that left an indelible mark on the city and caused, like the Guggenheim, some degree of recovery and revitalization on the environment in which they were based, at least temporarily. In any case, Koolhaas never gave the merely theoretical exercises up, but he segregated his work in two: OMA produced what was destined to be built and ruled by the parameters of the global market and AMO, Rem’s other side of the mirror, applied the architectural thought in unexplored fields, notwithstanding external agents and being able to work as a purely experimental laboratory. In light of this backdrop, September 11th 2001 came and the attacks on the Twin Towers in New York had devastating effects at all levels, leading to a change in the world order, in a surprisingly short period of time. Rem Koolhaas made a 180° turn directing his vision towards China, where he believed his contributions would have a more direct social benefit than in the Western world. (2) In order to introduce his new course of direction and the creation of the AMO "Think Tank", he planned a major exhibition in the Neue Nationalgalerie of Berlin under the title "Content", in parallel with edition of the book with the same title, which was at first the "exhibition catalog” but, deep down, was always conceived as the most important document of the Office since "SMLXL". However, in many ways it was just the opposite: a publication characterised by its magazine format, soft cover, very fine paging, "supermarket brochure" form and hyperdense content. It was an ephemeral, brief, light, cheap and "disposable" experiment. In fact, it is currently out of stock and out of print. Rem Koolhaas would probably disapprove of a research that sets the spotlight on him, for he would probably say that his validity has expired given that it has been ten years since its publication. However, it shows OMA’s conceptual and vital status at the time of its publication with crystalline clarity and it is also a true milestone in architectural communication. A point of no return. The epitome of the so-called "congestive communication ". This thesis suggests that "Content" contains the essence of Rem Koolhaas’ greatest contribution to the world of architecture: the deep and definitive transformation of architectural communication through the convergence of the conceptual state and the transmission thereof. His architectural and conceptual legacy has left an indelible mark on all subsequent generations. There is no doubt his essays, theories, projects and buildings already belong to the history of architecture. But it is his review on the concept of communication in architecture that has had and shall have an immediate influence on future generations, not only in their communication but also in their architecture, through a bijective exchange. Future approaches should try to determine what happens after "Content", after the maximum hyperdensity, after the visual culture of congestion; what shall Koolhaas suggest as well as what shall happen in the world of architectural communication. To this end, we shall study his latest communication-related projects, such as the design of the Venetian Architecture Biennale in 2014, his intensive research on the "Metabolism" in "Project Japan: Metabolism Talks ...", or the course of his latest territorial approaches in depth. Most recently, Rem Koolhaas has talked about "Preservation", "Sobriety" of "Essentialism", "Performance", etc. The mastermind of the culture of congestion now speaks of the "low density"... as it could not be otherwise, on the other side of the mirror. Summarizing, the white color as the sum of all colors; all wavelengths of the visible spectrum received at the same time.