4 resultados para High level architecture

em Lume - Repositório Digital da Universidade Federal do Rio Grande do Sul


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O aumento na complexidade dos sistemas embarcados, compostos por partes de hardware e software, aliado às pressões do mercado que exige novos produtos em prazos cada vez menores, tem levado projetistas a considerar a possibilidade de construir sistemas a partir da integração de componentes já existentes e previamente validados. Esses componentes podem ter sido desenvolvidos por diferentes equipes ou por terceiros e muitas vezes são projetados utilizando diferentes metodologias, linguagens e/ou níveis de abstração. Essa heterogeneidade torna complexo o processo de integração e validação de componentes, que normalmente é realizado através de simulação. O presente trabalho especifica mecanismos genéricos e extensíveis que oferecem suporte à cooperação entre componentes heterogêneos em um ambiente de simulação distribuída, sem impor padrões proprietários para formatos de dados e para a descrição do comportamento e interface dos componentes. Esses mecanismos são baseados na arquitetura DCB (Distributed Co-Simulation Backbone), voltada para co-simulação distribuída e heterogênea e inspirada nos conceitos de federado (componente de simulação) e federação (conjunto de componentes) que são definidos pelo HLA (High Level Architecture), um padrão de interoperabilidade para simulações distribuídas. Para dar suporte à co-simulação distribuída e heterogênea, esse trabalho descreve mecanismos que são responsáveis pelas tarefas de cooperação e distribuição, chamados de embaixadores, assim como o mecanismo gateway, que é responsável pela interoperabilidade entre linguagens e conversão de tipos de dados. Também é apresentada uma ferramenta de suporte à geração das interfaces de co-simulação, que são constituídas de dois embaixadores configuráveis e um gateway para cada federado, gerado a partir de templates pré-definidos.

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This thesis presents the study and development of fault-tolerant techniques for programmable architectures, the well-known Field Programmable Gate Arrays (FPGAs), customizable by SRAM. FPGAs are becoming more valuable for space applications because of the high density, high performance, reduced development cost and re-programmability. In particular, SRAM-based FPGAs are very valuable for remote missions because of the possibility of being reprogrammed by the user as many times as necessary in a very short period. SRAM-based FPGA and micro-controllers represent a wide range of components in space applications, and as a result will be the focus of this work, more specifically the Virtex® family from Xilinx and the architecture of the 8051 micro-controller from Intel. The Triple Modular Redundancy (TMR) with voters is a common high-level technique to protect ASICs against single event upset (SEU) and it can also be applied to FPGAs. The TMR technique was first tested in the Virtex® FPGA architecture by using a small design based on counters. Faults were injected in all sensitive parts of the FPGA and a detailed analysis of the effect of a fault in a TMR design synthesized in the Virtex® platform was performed. Results from fault injection and from a radiation ground test facility showed the efficiency of the TMR for the related case study circuit. Although TMR has showed a high reliability, this technique presents some limitations, such as area overhead, three times more input and output pins and, consequently, a significant increase in power dissipation. Aiming to reduce TMR costs and improve reliability, an innovative high-level technique for designing fault-tolerant systems in SRAM-based FPGAs was developed, without modification in the FPGA architecture. This technique combines time and hardware redundancy to reduce overhead and to ensure reliability. It is based on duplication with comparison and concurrent error detection. The new technique proposed in this work was specifically developed for FPGAs to cope with transient faults in the user combinational and sequential logic, while also reducing pin count, area and power dissipation. The methodology was validated by fault injection experiments in an emulation board. The thesis presents comparison results in fault coverage, area and performance between the discussed techniques.

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The focus of this thesis is to discuss the development and modeling of an interface architecture to be employed for interfacing analog signals in mixed-signal SOC. We claim that the approach that is going to be presented is able to achieve wide frequency range, and covers a large range of applications with constant performance, allied to digital configuration compatibility. Our primary assumptions are to use a fixed analog block and to promote application configurability in the digital domain, which leads to a mixed-signal interface. The use of a fixed analog block avoids the performance loss common to configurable analog blocks. The usage of configurability on the digital domain makes possible the use of all existing tools for high level design, simulation and synthesis to implement the target application, with very good performance prediction. The proposed approach utilizes the concept of frequency translation (mixing) of the input signal followed by its conversion to the ΣΔ domain, which makes possible the use of a fairly constant analog block, and also, a uniform treatment of input signal from DC to high frequencies. The programmability is performed in the ΣΔ digital domain where performance can be closely achieved according to application specification. The interface performance theoretical and simulation model are developed for design space exploration and for physical design support. Two prototypes are built and characterized to validate the proposed model and to implement some application examples. The usage of this interface as a multi-band parametric ADC and as a two channels analog multiplier and adder are shown. The multi-channel analog interface architecture is also presented. The characterization measurements support the main advantages of the approach proposed.