1,516 research outputs found

    Hardware Certification for Real-time Safety-critical Systems: State of the Art

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    This paper discusses issues related to the RTCA document DO-254 Design Assurance Guidance for Airborne Electronic Hardware and its consequences for hardware certification. In particular, problems related to circuits’ compliance with DO-254 in avionics and other industries are considered. Extensive literature review of the subject is given, including current views on and experiences of chip manufacturers and EDA industry with qualification of hardware design tools, including formal approaches to hardware verification. Some results of the authors’ own study on tool qualification are presented

    Digital signal processor fundamentals and system design

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    Digital Signal Processors (DSPs) have been used in accelerator systems for more than fifteen years and have largely contributed to the evolution towards digital technology of many accelerator systems, such as machine protection, diagnostics and control of beams, power supply and motors. This paper aims at familiarising the reader with DSP fundamentals, namely DSP characteristics and processing development. Several DSP examples are given, in particular on Texas Instruments DSPs, as they are used in the DSP laboratory companion of the lectures this paper is based upon. The typical system design flow is described; common difficulties, problems and choices faced by DSP developers are outlined; and hints are given on the best solution

    Bit error rate test for optical communication link using prbs generated by an fpga - hardware implementation

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    Signal Processing and new Modulations Formats are usually developed using MATLAB and then back tested off-line with recorded signals. Once an algorithm is proven useful it has to be implemented in an FPGA to be tested live. In this project, the student will study the main parameters of advanced modulation formats, transfer MATLAB based algorithm to an FPGA, polish and optimize the FPGA software, experimentally test in a real-time scenario the implementation.The Objective involved realizing a PRBS-BERT to analyze the optical link performance. The configuration of the board for the application involved studying the daughter board, the interconnect (i.e. HSMC) and thereby establishing connection between the Cyclone III Starter Kit and the THDB_ADA daughter board. Finally, the PRBS design was downloaded and verified in the setup. Another important study involved analyzing the necessary precautions to be taken with regard to the board design

    Bit error rate test for optical communication link using prbs generated by an fpga - system design

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    Bit Error Rate Testing(BERT) was implemented using Cyclone III FPGA Starter Kit along with THDB_ADA board and interfaced with several kilometers long optical fiber, to study the link performance of the optical communication system. In this, a single FPGA acts as both transmitter and receiver. The logic to transmit the PRBS bits using LFSR and receive them at the receiver to check for bit errors was implemented

    Java Card:An analysis of the most successful smart card operating system

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    To explain why the Java Card operating system has become the most successful smart card operating system to date, we analyze the realized features of the current Java Card version, we argue it could be enhanced by adding a number of intended features and we discuss a set of complementary features that have been suggested. No technology can be successful without the right people and the right circumstances, so we provide some insights in the personal and historical historic aspects of the success of Java Card

    Space power distribution system technology. Volume 2: Autonomous power management

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    Electrical power subsystem requirements, power management system functional requirements, algorithms, power management subsystem, hardware development, and trade studies and analyses are discussed

    Avionics architecture studies for the entry research vehicle

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    This report is the culmination of a year-long investigation of the avionics architecture for NASA's Entry Research Vehicle (ERV). The Entry Research Vehicle is conceived to be an unmanned, autonomous spacecraft to be deployed from the Shuttle. It will perform various aerodynamic and propulsive maneuvers in orbit and land at Edwards AFB after a 5 to 10 hour mission. The design and analysis of the vehicle's avionics architecture are detailed here. The architecture consists of a central triply redundant ultra-reliable fault tolerant processor attached to three replicated and distributed MIL-STD-1553 buses for input and output. The reliability analysis is detailed here. The architecture was found to be sufficiently reliable for the ERV mission plan
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