• Title/Summary/Keyword: 모드분석

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Comparative Analysis of PBTI Induced Device Degradation in Junctionless and Inversion Mode Multiple-Gate MOSFET (PBTI에 의한 무접합 및 반전모드 다중게이트 MOSFET의 소자 특성 저하 비교 분석)

  • Kim, Jin-Su;Hong, Jin-Woo;Kim, Hye-Mi;Lee, Jae-Ki;Park, Jong-Tae
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.17 no.1
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    • pp.151-157
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    • 2013
  • In this paper, a comparative analysis of PBTI induced device degradation in nanowire n-channel junctionless and inversion mode Multiple-Gate MOSFET(MuGFETs) has been performed. It has been observed that the threshold voltage is increased after PBTI stress and the threshold voltage variation of junctionless device is less significant than that of inversion mode device. However the degradation rate of junctionless device is less significant than that of inversion mode device. The activation energy of the device degradation is larger in inversion mode device than junctionless device. In order to analyze the more significant PBTI induced device degradation in inversion mode device than junctionless device, 3-dimensional device simulation has been performed. The electron concentration in inversion mode device is equal to the one in junctionless device but the electric field in inversion mode device is larger than junctionless device.

Preliminary Analysis on Characteristics of Attitude Control based on Operation Scenario of Small SAR Satellite Mission, S-STEP (초소형 SAR 위성 S-STEP의 임무 시나리오에 따른 자세 제어 성능 예비 분석)

  • Lee, Eunji;Park, Jinhan;Song, Sung-Chan;Oh, Hyun-Ung
    • Journal of Aerospace System Engineering
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    • v.16 no.5
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    • pp.49-56
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    • 2022
  • S-STEP is a small SAR satellite mission that monitors time-limited emergency targets and military anomalies in areas of interest, achieving the average revisit in less than 30 minutes by deploying a constellation of 32 satellites in low orbit at an altitude of 510 km. The mission operation mode of S-STEP is divided into normal mode, observation mode, communication mode, and orbit maintenance mode. Further,, the attitude control mode is subdivides into initial detumbling, sun pointing, target pointing, ground station pointing, and thrust direction maintenance. Based on the preliminary mission operational scenario and the satellite's characteristics, this study analyzed the attitude control performance during initial detumbling and observation modes. It verifies that each mode's attitude control accuracy requirements within the time allotted by the scenario of the S-STEP achieved.

Analysis on the Effect of Driving Condition in PEM Fuel Cell Durability (자동차용 연료전지의 운전환경에 따른 내구성 분석)

  • Yoo, Seung-Eul;Goo, Young-Mo;Kim, Myoung-Hwan;Son, Ik-Jae;Yoon, Jong-Jin;Oh, Seung-Chan
    • 한국신재생에너지학회:학술대회논문집
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    • 2007.11a
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    • pp.161-164
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    • 2007
  • 연료전지의 상용화 시점에 이르러 내구성에 대한 기술 확보가 점점 더 부각되고 있다. 현재 연료전지의 내구성을 감소시키는 1차적인 요인은 핵심부품인 촉매, 전해질막, MEA(Membrane & Electrode Assembly) 등에 의한 것이며 2차적인 요인은 운전 시스템 및 환경 등에 의해 결정되어진다. 특히, 연료전지자동차는 이동용, 가정용, 발전용에 비하여 부하변동이 극심한 조건에서 운전되기 때문에 연료전지 시스템의 내구성 확보에 많은 제어기술이 요구된다. 본 연구에서는 연료전지자동차 운전조건(Driving mode)을 부하변동 기준에 의한 고전류, 중전류, 저전류의 3가지 모드로 분류하였다. 각각의 운전조건에서 일정 cycle마다 성능곡선을 측정하여 10만 cycle 이상의 반복운전을 수행하였으며 측정된 성능곡선을 empirical equation에 적용하여 시간에 따른 overvoltage 인자에 대한 분석을 하였다. 운전시간이 증가함에 따라 고전류 모드의 경우 activation overvoltage 인자 중 current density loss가 증가하여 OCV가 급격히 감소하였으나 내구성은 저전류 모드에 비하여 높게 나타났다. 저전류 모드의 경우 고전류 모드와 상반된 결과를 보였으며 성능감소요인은 activation 및 ohmic overvoltage의 점차적인 증가에 의한 것으로 분석되었다.

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Expert System for FMECA Using Minimal Cut Set and Fuzzy Theory (최소절단집합과 퍼지이론을 이용한 FMECA 전문가 시스템)

  • Kim, Dong-Jin;Kim, Jin-O;Kim, Hyung-Chul
    • Journal of the Korean Society for Railway
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    • v.12 no.3
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    • pp.342-347
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    • 2009
  • Failure Mode Effects and Criticality Analysis (FMECA) is one of most widely used methods in modern engineering system to investigate potential failure modes and its severity upon the system. While performing FMECA, the experts evaluates criticality and severity of each failure mode and visualize the risk level matrix putting those indices to column and row variable respectably. Which results uncertainty in the result. In order to handle the uncertainty and conclude risk level matrix, this paper proposes a new FMECA procedure using minimal cut set (MCS) and fuzzy theory. Severity is calculated by proposed structural importance while criticality is determined by typical equipment failure rate data from IEEE Std 493. Finally, the risk level is compounded of these indices.

Experiments on the Energy Saving and Performance Effects of IEEE 802.110 Power-Saving Mode (PSM) (IEEE 802.llb 무선 LAN에서 전력절감모드의 전력 절약 효과 및 통신성능 분석)

  • 권도한;박창윤;정충일
    • Proceedings of the Korean Information Science Society Conference
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    • 2004.10c
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    • pp.133-135
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    • 2004
  • IEEE 802.11 표준에서 지원하는 전력절감모드(Power-Saving Mode)의 실제 전력 효율성과 통신 성능의 차이를 다양한 트랙픽 환경에서 실험한다. 그리고 전력절감모드로 운영 중인 스테이션이 다른 스테이션의 통신 성능에 미치는 영향도 조사한다. 일반적으로 전력절감모드는 전력 소비면에서는 효율적이지만 통신성능을 저하시킨다. 그러나 트래픽의 종류에 따라 통신 성능의 저하에는 차이가 발생하며 별도의 혼잡제어를 하지 않는 트래픽의 경우에는 전력절감모드의 운영이 성능면에서 의미가 있음을 확인하였다.

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5G 단독모드 기기 보안 인증 현황

  • Kwon, Sungmoon;Park, Seongmin;Kim, Dowon
    • Review of KIISC
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    • v.31 no.6
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    • pp.37-40
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    • 2021
  • 미국, 중국 등에 이어 국내에서도 KT에서 2021년 7월 5G 단독모드(StandAlone)를 상용화 하였다. 5G 비단독모드(Non-StandAlone)에서는 다년간 사용되었던 기존 LTE(Long Term Evolution) 망의 장비를 재활용하기 때문에 신규 장비의 도입은 5G 기지국으로 제한된다. 그러나 5G 단독모드에서는 새롭게 정의된 5G 장비들을 사용하기 때문에 이에 대한 위협 분석과 보안 기능의 정의에 따라 각 장비에 보안의 구현이 제대로 되어 있는지 검증하는 절차가 요구된다. 이러한 환경에서 본 논문은 5G 단독모드 기기의 보안 인증 현황을 제공하고자 한다.

Long Term Monitoring of Dynamic Characteristics of a Jacket-Type Offshore Structure Using Dynamic Tilt Responses and Tidal Effects on Modal Properties (동적 경사 응답을 이용한 재킷식 해양구조물의 장기 동특성 모니터링 및 조류 영향 분석)

  • Yi, Jin-Hak;Park, Jin-Soon;Han, Sang-Hun;Lee, Kwang-Soo
    • KSCE Journal of Civil and Environmental Engineering Research
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    • v.32 no.2A
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    • pp.97-108
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    • 2012
  • Dynamic responses were measured using long-term monitoring system for Uldolmok tidal current pilot power plant which is one of jacket-type offshore structures. Among the dynamic quantities, the tilt angle was chosen because the low frequency response components can be precisely measured by dynamic tiltmeter, and the natural frequencies and modal damping ratio were successfully identified using proposed LS-FDD (least squared frequency domain decomposition) method. And the effects of tidal height and tidal current velocity on the variation of natural frequencies and modal damping ratios were investigated in time and frequency domain. Also the non-parametric models were tested to model the relationship between tidal conditions and modal properties such as natural frequencies and damping ratios.

Seismic Fragility Analysis of Multi-Modes Structures Considering Modal Contribution Factor (모드기여도를 고려한 복수모드구조물의 지진취약도분석)

  • 조양희;조성국
    • Journal of the Earthquake Engineering Society of Korea
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    • v.6 no.4
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    • pp.15-22
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    • 2002
  • In the course of seismic probabilistic risk assessment(SPRA), seismic fragility analysis(SFA) is utilized as a tool to evaluate the actual seismic capacity of structures. This paper introduces a methodology of SFA and its evaluation procedures, especially focusing on the basic fragility variables. A new definition of the response spectrum shape factor as one of the most critical basic variables is suggested. The new factor is expressed as a term of linear algebraic sum using the modal contribution factor. The efficiency of new response spectrum shape factor is evaluated and validated to use in practice through the case study of the nuclear power plant structures. The case study results show that the proposed method can be effectively applicable to multi-mode structures with composite modal damping.

The effect of Local Vibration Modes on the Flutter (국부진동모드가 플러터해석에 미치는 영향연구)

  • Shin, Young-Sug;Kim, Heon-Ju;Kim, Seong-Tae;Kim, Jae-Young;Hwang, Chul-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.10
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    • pp.919-926
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    • 2011
  • The fin of high speed air vehicle is composed of skins and strong skeletons. In the flutter analysis, the eigenmodes of a fin are used for evaluating the unsteady aerodynamic force and the modal approach is applied for solving the flutter equation in both time and frequency domain. Therefore, the proper eigenmodes used for a modal flutter analysis should be chosen. For the appropriate choice of eigenmodes, when there exist local modes of a skin in the high modes, the effects of those modes on the unsteady aerodynamic force and flutter characteristics are anlalyzed.