5,966 research outputs found

    Shuttle orbiter Ku-band radar/communications system design evaluation

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    Tasks performed in an examination and critique of a Ku-band radar communications system for the shuttle orbiter are reported. Topics cover: (1) Ku-band high gain antenna/widebeam horn design evaluation; (2) evaluation of the Ku-band SPA and EA-1 LRU software; (3) system test evaluation; (4) critical design review and development test evaluation; (5) Ku-band bent pipe channel performance evaluation; (6) Ku-band LRU interchangeability analysis; and (7) deliverable test equipment evaluation. Where discrepancies were found, modifications and improvements to the Ku-band system and the associated test procedures are suggested

    Power-efficient design of 16-bit mixed-operand multipliers

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    Thesis (M. Eng.)--Massachusetts Institute of Technology, Dept. of Electrical Engineering and Computer Science, 2004.Includes bibliographical references (p. 53).Multiplication is an expensive and slow arithmetic operation, which plays an important role in many DSP algorithms. It usually lies in the critical-delay paths, having an effect on performance of the system as well as consuming large power. Consequently, significant improvements in both power and performance can be achieved in the overall DSP system by carefully designing and optimizing power and performance of the multiplier. This thesis explores several circuit-level techniques for power-efficiently designing multipliers, including supply voltage reduction, efficient multiplication algorithms, low power circuit logic styles, and transistor sizing using dynamic and static tuners. Based on these techniques, several 16-bit multipliers have been successfully designed and implemented in 0.13[micro]m CMOS technology at the supply voltage of 1.5V and 0.9V. The multipliers are modified to handle multiplications of two 16-bit operands in which each can be either signed magnitude or two's complement formats. Examining power-performance characteristics of these multipliers reveals that both array and tree structures are feasible solutions for designing 16-bit multipliers, and complementary CMOS and single-ended CPL-TG logics are promising candidates for power-efficient design. The appropriate choices of structures and logic styles depend on power and performance constraints of the particular design.by Sataporn Pornpromlikit.M.Eng

    Systematic Model-based Design Assurance and Property-based Fault Injection for Safety Critical Digital Systems

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    With advances in sensing, wireless communications, computing, control, and automation technologies, we are witnessing the rapid uptake of Cyber-Physical Systems across many applications including connected vehicles, healthcare, energy, manufacturing, smart homes etc. Many of these applications are safety-critical in nature and they depend on the correct and safe execution of software and hardware that are intrinsically subject to faults. These faults can be design faults (Software Faults, Specification faults, etc.) or physically occurring faults (hardware failures, Single-event-upsets, etc.). Both types of faults must be addressed during the design and development of these critical systems. Several safety-critical industries have widely adopted Model-Based Engineering paradigms to manage the design assurance processes of these complex CPSs. This thesis studies the application of IEC 61508 compliant model-based design assurance methodology on a representative safety-critical digital architecture targeted for the Nuclear power generation facilities. The study presents detailed experiences and results to demonstrate the benefits of Model testing in finding design flaws and its relevance to subsequent verification steps in the workflow. Additionally, to study the impact of physical faults on the digital architecture we develop a novel property-based fault injection method that overcomes few deficiencies of traditional fault injection methods. The model-based fault injection approach presented here guarantees high efficiency and near-exhaustive input/state/fault space coverage, by utilizing formal model checking principles to identify fault activation conditions and prove the fault tolerance features. The fault injection framework facilitates automated integration of fault saboteurs throughout the model to enable exhaustive fault location coverage in the model

    Intelligent Hardware-Enabled Sensor and Software Safety and Health Management for Autonomous UAS

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    Unmanned Aerial Systems (UAS) can only be deployed if they can effectively complete their mission and respond to failures and uncertain environmental conditions while maintaining safety with respect to other aircraft as well as humans and property on the ground. We propose to design a real-time, onboard system health management (SHM) capability to continuously monitor essential system components such as sensors, software, and hardware systems for detection and diagnosis of failures and violations of safety or performance rules during the ight of a UAS. Our approach to SHM is three-pronged, providing: (1) real-time monitoring of sensor and software signals; (2) signal analysis, preprocessing, and advanced on-the- y temporal and Bayesian probabilistic fault diagnosis; (3) an unobtrusive, lightweight, read-only, low-power hardware realization using Field Programmable Gate Arrays (FPGAs) in order to avoid overburdening limited computing resources or costly re-certi cation of ight software due to instrumentation. No currently available SHM capabilities (or combinations of currently existing SHM capabilities) come anywhere close to satisfying these three criteria yet NASA will require such intelligent, hardwareenabled sensor and software safety and health management for introducing autonomous UAS into the National Airspace System (NAS). We propose a novel approach of creating modular building blocks for combining responsive runtime monitoring of temporal logic system safety requirements with model-based diagnosis and Bayesian network-based probabilistic analysis. Our proposed research program includes both developing this novel approach and demonstrating its capabilities using the NASA Swift UAS as a demonstration platform

    Specification-driven design of custom hardware in HOP

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    technical reportWe present a language "Hardware viewed as Objects and Processes" (HOP) for specifying the structure, behavior, and timing of hardware systems. HOP embodies a simple process model for lock-step synchronous processes. Processes may be described both as a black-box and as a collection of interacting sub-processes. The latter can be statically simplified using an algorithm 'PARCOMP'. PARCOMP symbolically simulates a collection of interacting processes. The advantages claimed for HOP include simple semantics, intuitiveness, high expressive power, and numerous provisions to support easily verifiable designs all the way to VLSI layout. After introducing HOP, and presenting some of the results obtained from experimenting with the HOP design system, we present the design of a large hardware system (the "Utah Simulation Engine") currently being developed to speed-up distributed discrete event simulation using Time Warp. Issues in the specification driven design of this system are discussed and illustrated using HOP

    Development of a Hardware-in-the-loop Simulation Platform for Safety Critical Control System Evaluation

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    During the lifetime of a nuclear power plant (NPP) safety electronic control system components become obsolete [7]. It is difficult to find replacement components qualified for nuclear applications [50]. Due to strict regulations, replacement components undergo extensive verification and operational analysis [70]. Therefore, the need for a platform to evaluate replacement safety control systems in a non-intrusive manner is evident. Verifying the operation or functionality of potential replacement electronic control systems is often performed through simulation [71]. To enable simulation, a physical interface between potential control systems and computer based simulators is developed. System connectivity is establish using Ethernet and standard industrial electrical signals. The interface includes a National Instruments (NI) virtual instrument (VI) and data acquisition system (DAQ) hardware. The interface supports simulator controlled transmission and receipt of variables. The transmission of simulated process variables to and from an external control system is enabled. This is known as hardware-in-the-loop (HIL) simulation [49]. Next, HIL interface performance is verified and the following are identified; a measure of availability; the effect of varied configurations; and limitations. Further, an HIL simulation platform is created by connecting a NPP simulator and a programmable logic controller (PLC) to the interface, Canadian Deuterium Uranium (CANDU) reactor training simulator and Invensys Tricon version nine (v9) safety PLC respectively. The PLC is programmed to operate as shutdown system no. 1 (SDSl) of a CANDU reactor. Platform availability is verified and the response of the PLC as SDSl and is monitored during reactor shutdown. Proper execution of the steam generator level low (SGLL) logic on the PLC and variable transmission are observed. Thus, a platform and procedure for the evaluation of replacements for obsolete electronic control system components is demonstrated

    A Primer on Architectural Level Fault Tolerance

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    This paper introduces the fundamental concepts of fault tolerant computing. Key topics covered are voting, fault detection, clock synchronization, Byzantine Agreement, diagnosis, and reliability analysis. Low level mechanisms such as Hamming codes or low level communications protocols are not covered. The paper is tutorial in nature and does not cover any topic in detail. The focus is on rationale and approach rather than detailed exposition
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