79 resultados para engineering design process


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El objetivo de este proyecto es el estudio detallado y fabricación de los filtros de cavidades con resonadores helicoidales. Este proyecto está motivado por el hecho de que es una tecnología cada vez más presente en el mercado y su uso resulta muy ´útil en aplicaciones donde se requiere que los componentes sean de tamaño reducido. Esto se debe a que las cavidades helicoidales son de las que presentan menor tamaño para una frecuencia dada. La estructura del proyecto se va a dividir en tres grandes bloques. El primero es el estudio teórico de esta tecnología. En la introducción se verán los principales usos de estos dispositivos, dando ejemplos comerciales, para luego poder compararlos con el prototipo que se ha construido. A continuación, en los primeros capítulos, se detallará la geometría de los resonadores, las ecuaciones que deben aplicarse para calcular las dimensiones y los elementos de diseño. Se comentarán algunas modificaciones opcionales que se pueden aplicar al filtro en el caso de que se requieran especificaciones especiales para la aplicación para la que esté destinado el dispositivo. En segundo lugar se procederá a diseñar modelos de filtros helicoidales para distintas bandas de frecuencia, con el programa de diseño CST Microwave Studio. Estos serán ajustados y parametrizados con el fin de obtener unos requerimientos que serán fijados previamente. Y por ´ultimo se mostrará como ha sido el proceso de prototipado del filtro de tres cavidades para la banda de FM que se ha llevado a cabo y estarán plasmadas las medidas que se han realizado para determinar las características que tiene el prototipo. Este proyecto está planteado como un manual para que el interesado en la fabricación de este tipo de filtros pueda afrontar el diseño desde el inicio y ser capaz de construir un prototipo que cumpla con las características que sean requeridas. ABSTRACT. The main purpose of this project is the detailed study of helical resonator filters and their manufacturing. This technology is increasingly present in the market, and its use is very convenient in applications where it is required for the components to be of reduced size. This is due to helical resonators being smaller than conventional cavity filters for a given frequency. The projects structure will be divided into three sections. First, the theoretical study of this technology will be presented. In the introduction, the main uses of these devices will be shown and commercial examples will be given, which can then be compared with the built prototype. Afterwards, in the first chapters, the geometry of the resonators, the required equations to calculate their dimensions and the design elements will be detailed. Some optional modifications that can be applied to the filter in the case of special specifications will be discussed. Second, some models of helical filters will be designed for different frequency bands, using the design software CST Microwave Studio. These will be adjusted and parameterized in order to meet requirements that will be set previously. Finally, the development of the prototyping process of a three cavities filter for the FM band will be shown, and the measurements that were made to determine the prototypes features will be reflected. This project is designed as a handbook; the individual concerned in the manufacture of these filters should be able to follow the design process from the start and build a prototype that has the required characteristics.

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Abstract. The ASSERT project de?ned new software engineering methods and tools for the development of critical embedded real-time systems in the space domain. The ASSERT model-driven engineering process was one of the achievements of the project and is based on the concept of property- preserving model transformations. The key element of this process is that non-functional properties of the software system must be preserved during model transformations. Properties preservation is carried out through model transformations compliant with the Ravenscar Pro?le and provides a formal basis to the process. In this way, the so-called Ravenscar Computational Model is central to the whole ASSERT process. This paper describes the work done in the HWSWCO study, whose main objective has been to address the integration of the Hardware/Software co-design phase in the ASSERT process. In order to do that, non-functional properties of the software system must also be preserved during hardware synthesis. Keywords : Ada 2005, Ravenscar pro?le, Hardware/Software co-design, real- time systems, high-integrity systems, ORK

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This research is concerned with the experimental software engineering area, specifically experiment replication. Replication has traditionally been viewed as a complex task in software engineering. This is possibly due to the present immaturity of the experimental paradigm applied to software development. Researchers usually use replication packages to replicate an experiment. However, replication packages are not the solution to all the information management problems that crop up when successive replications of an experiment accumulate. This research borrows ideas from the software configuration management and software product line paradigms to support the replication process. We believe that configuration management can help to manage and administer information from one replication to another: hypotheses, designs, data analysis, etc. The software product line paradigm can help to organize and manage any changes introduced into the experiment by each replication. We expect the union of the two paradigms in replication to improve the planning, design and execution of further replications and their alignment with existing replications. Additionally, this research work will contribute a web support environment for archiving information related to different experiment replications. Additionally, it will provide flexible enough information management support for running replications with different numbers and types of changes. Finally, it will afford massive storage of data from different replications. Experimenters working collaboratively on the same experiment must all have access to the different experiments.

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The satellite remote sensing missions are essential for long-term research around the condition of the earth resources and environment. On the other hand, in recent years the application of microsatellites is of interest in many space programs for their less cost and response time. In microsatellite remote sensing missions there are tight interrelations between different requirements such as orbital altitude, revisit time, mission life and spatial resolution. Also, all of these requirements can affect the whole system level design characteristics. In this work, the remote sensing microsatellite sizing process is divided into three major design disciplines; a) orbit design, b) payload sizing and c) bus sizing. Finally, some specific design cases are investigated inside the design space for evaluating the effect of different design variables on the satellite total mass. Considering the results of the work, it is concluded that applying a systematic approach at the initial design phase of such projects provides a good insight to the not clearly seen interactions inside their highly extended design space