フィールドにおけるテスト印加と低電力論理BISTに関する研究

Advances in semiconductor process technology have resulted in various aging issues in field operation of Very Large Scale Integration (VLSI) circuits. For example, HCI (Hot carrier injection), BTI (Bias Temperature Instability), TDDB (Time Dependent Dielectric Breakdown) are well-known aging phenomena, and they can increase the circuit delay resulting in serious reliability problems. In order to avoid system failures caused by aging, recent design usually sets a certain timing margin in operational frequency of the circuit. However, it is difficult to determine the size of the proper timing margin because of the difficulty of prediction of its aging speed in actual use that is related to operational environment. Pessimistic prediction may result in performance sacrificing although it will improve the reliability of the system. BIST-based field test is a promising way to guarantee the reliability of the circuit through detecting the aging-induced faults during the circuit operation. However, the field test has a limitation on test application time, which makes it difficult to achieve high test quality. Therefore an effective test application method at field is required. In addition to the requirement of short test application time, the BIST-based field test requires performing at-speed testing in order to detect timing-related defects. However, it is well known that power dissipation during testing is much higher than that in normal circuit operation. Because excessive power dissipation causes higher IR-drop and higher temperature, it results in delay increase during testing, and in turn, causing false at-speed testing and yield loss. While many low power test methods have been proposed to tackle the test power issue, inadequate test power reduction and lower fault coverage still remain as important issues. Moreover, low power testing that just focuses on power reduction is insufficient. When the test power is reduced to a very low level, a timing-related defect may be missed by the test, and a defective circuit will appear to be a good part passing the test. Therefore, appropriate test power control is necessary though it was out of considering in the existing methods. In this dissertation, we first proposed a new test application to satisfy the limitation of short test application time for BIST-based field test, and then we proposed a new low power BIST scheme that focuses on controlling the test power to a specified value for improving the field test quality. In chapter 3, a new field test application method named “rotating test” is presented in which a set of generated test patterns to detect aging-induced faults is partitioned into several subsets, and apply each subset in one test session at field. In order to maximize the test quality for rotating test, we proposed test partitioning methods that refer to two items: First one aims at maximizing fault coverage of each subset obtained by partitioning. Second one aims at minimizing the detection time interval of all faults in rotating test to avoid system failures. Experimental results demonstrated the effectiveness of the proposed partitioning methods. In chapter 4, we proposed a new low power BIST scheme which can control the scan-in power, scan-out power and capture power while keeping test coverage at high level. In this scheme, a new circuit called pseudo low-pass filter (PLPF) is developed for scan-in power control, and a multi-cycle capture test technique is employed to reduce the capture power. In order to control scan-out power dissipated by test responses, we proposed a novel method that selects some flip-flops in scan chains at logic design phase, and fills the selected flip-flops with proper values before starting scan-shift operation so as to reduce the switching activity associated with scan-out. The experimental results for ISCAS-89 and ITC-99 benchmark circuits show that significant scan-in power reduction rate (the original rate of 50% is reduced to 7~8%) and capture power reduction rate (the original rate of 20% is reduced to 6~7%) were derived. With the scan-out controlling method, the scan-out power can be reduced from 17.2% to 8.4%, which could not be achieved by the conventional methods. Moreover, in order to control the test power to the specified rate to accommodate the various test power requirements. A scan-shift power controlling scheme was also discussed. It showed the capability of controlling any scan-shift toggle rate between 6.7% and 50%.九州工業大学博士学位論文 学位記番号:情工博甲第289号　学位授与年月日:平成26年3月25日1. INTRODUCTION|2. PRELIMINARY|3. BIST-BASED FIELD ROTATING TEST FOR AGING-INDUCED FAULT DETECTION|4. TEST POWER REDUCTION FOR LOGIC-BIST|5. SUMMARY九州工業大学平成25年

Space programs summary no. 37-63, volume 1 for the period 1 March - 30 April 1970. Flight projects

Mariner Mars 1971, Mariner Venus-Mercury 1973 and Viking Orbiter 1975 status report

Mariner Venus/Mercury 1973 study

Mariner Venus/Mercury 1973 flyby mission and description of spacecraft and subsystem

Deployable antenna phase A study

Applications for large deployable antennas were re-examined, flight demonstration objectives were defined, the flight article (antenna) was preliminarily designed, and the flight program and ground development program, including the support equipment, were defined for a proposed space transportation system flight experiment to demonstrate a large (50 to 200 meter) deployable antenna system. Tasks described include: (1) performance requirements analysis; (2) system design and definition; (3) orbital operations analysis; and (4) programmatic analysis

Modeling and Analysis of Power Processing Systems

The feasibility of formulating a methodology for the modeling and analysis of aerospace electrical power processing systems is investigated. It is shown that a digital computer may be used in an interactive mode for the design, modeling, analysis, and comparison of power processing systems

State of the art survey of technologies applicable to NASA's aeronautics, avionics and controls program

The state of the art survey (SOAS) covers six technology areas including flightpath management, aircraft control system, crew station technology, interface & integration technology, military technology, and fundamental technology. The SOAS included contributions from over 70 individuals in industry, government, and the universities

Geostationary platform systems concepts definition study. Volume 2: Technical, book 3

The supporting research and technology, and space demonstrations required to support the 1990s operational geostationary platforms are identified. Also the requirements on and interfaces with the Space Transportation System hardware elements supporting the geostationary platform program, including the shuttle, orbital transfer vehicles, teleoperator, etc., are investigated to provide integrated support requirements. Finally, a preliminary evaluation of the practicability and capabilities of an experimental platform from the standpoint of technology, schedule, and cost is given

Accessing Space: A Catalogue of Process, Equipment and Resources for Commercial Users, 1990

A catalogue is presented which is intended for commercial developers who are considering, or who have in progress, a project involving the microgravity environment of space or remote sensing of the Earth. An orientation is given to commercial space activities along with a current inventory of equipment, apparatus, carriers, vehicles, resources, and services available from NASA, other government agencies and U.S. industry. The information describes the array of resources that commercial users should consider when planning ground or space based developments. Many items listed have flown in space or been tested in labs and aboard aircraft and can be reused, revitalized, or adapted to suit specific requirements. New commercial ventures are encouraged to exploit existing inventory and expertise to the greatest extent possible

Orbiting solar observatory 8 high resolution ultraviolet spectrometer experiment

Oscillations, physical properties of the solar atmosphere, motions in the quiet solar atmosphere, coronal holes, motions in solar active regions, solar flares, the structure of plage regions, an atlas, and aeronomy are summarized. Photometric sensitivity, scattered light, ghosts, focus and spectral resolution, wavelength drive, photometric sensitivity, and scattered light, are also summarized. Experiments are described according to spacecraft made and experiment type. Some of the most useful data reduction programs are described