• 대한전기학회:학술대회논문집
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• 대한전기학회 2002년도 하계학술대회 논문집 D
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• pp.2646-2648
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• 2002

This paper deals with a comparative evaluation of the reliability of control rod drive mechanisms including their driving methods for nuclear power plants. Basically there exist two types of electromagnetic-jack-type drive mechanisms in commercial use that are called as Control Rod Drive Mechanism and Control Element Drive Mechanism. Each type has corresponding drive sequence to make the movements of insertion and withdrawal. A state-space model is derived for each model graphically. Then the evaluation of the reliability is carried out on the programming tool called SHARPE. The evaluation does not give any meaningful numerical values for the reliability but just shows a relative degree to each other in view of reliability.

• 한국통신학회논문지
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• 제34권6B호
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• pp.559-567
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• 2009

본 논문에서는 콘텐츠 재분배 기능을 갖는 CDN (RDCDN)의 구조를 제안하고, 제안된 구조에 대한 특성과 콘텐츠 재분배 알고리즘에 대해 설명한다. 본 논문에서 제안한 방식은 대리시스템의 메모리 공간을 효율적으로 관리하며, 부하조절을 위한 특별한 알고리즘 없이 능동적인 부하조절 기능을 수행할 수 있다. 또한, 주 대리시스템(Main surrogate) 기능을 통해, 각 대리시스템에서 임의적인 콘텐츠 삭제가 일어나는 경우, 발생할 수 있는 신뢰성 저하를 방지할 수 있다. 제안한 방식의 특성을 평가하기 위해, 기존 DCDN과 비교하여 대리시스템의 메모리 사용량, 대리시스템 신뢰성의 우수함을 확인하였으며, 콘텐츠 재분배 비율에 관한 시뮬레이션을 통해 RDCDN의 콘텐츠 재분배 기능의 특성을 파악하였다. 또한, 기존 상업용 CDN 모델과 DCDN의 성능을 비교하여 RDCDN의 성능의 우수성을 분명히 확인하였다.

• 천문학회보
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• 제44권2호
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• pp.57.3-57.3
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• 2019

Space applications of the motion have been served with DC motors for decades. But their functionality with a gearbox and lubricants and their weights are always an issue for its application. A piezo-motor has an advantage on the direct driving with higher accuracy, smaller size, and no-EMI. We use the piezo-motor to rotate a filter wheel directly in a balloon-borne coronagraph launched on September 2019. The piezo-motor works well in a temperature range from -10 to 40 Celsius with high reliability and high positioning / tilt accuracy (~0.1degree) with a photo-encoder. We verify its functionality for 7 days. In this talk, we report the design, test processes of the filter wheel including its balloon flight result.

• 시스템엔지니어링워크숍
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• 통권4호
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• pp.90-94
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• 2004

System engineering(SE) management techniques applied for space launch system development are introduced to assess the current status and address the effwctiveness of these techniques. Management plans and guides are prepared for the work breakdown structure , data, comfiguration, interface control, Quality assurance, procurement, reliability, risk and verification/validation . Further improvement is required for the system engineering management plan(SEMP) to merge the international cooperation into current engineering managment system.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2003년도 통신소사이어티 추계학술대회논문집
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• pp.277-280
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• 2003

In this paper, we analyze the performance of transmitter and receiver of W-CDMA system using the channel coding and space time code in downlink over ITU-R realistic channel model. We can improve the reliability of communications and increase the data rate by channel coding, and we can get a diversity gain by using the space time code over fading channels. We also apply the RAKE receiver to improve tile performance in multi-Path fading channel environment.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2008년도 한국우주과학회보 제17권2호
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• pp.32.1-32.1
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• 2008

It is well known that solar and space weather activities can influence the performance and reliability of modern technological system and can endanger human life. Since 2007, the Korea Astronomy and Space Science Institute (KASI) has initiated a research project for the construction of Korean Space Weather Prediction Center (K-SWPC) to make preparations for the next solar cycle maximum (~2012). In this talk, we briefly introduce the current progress of KASI activities for K-SWPC; extension of ground observation system, construction of space weather database and network, development of prediction models, and space weather effects. In addition, future plans for KSWPC will be discussed.

• 대한소아치과학회지
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• 제47권2호
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• pp.176-187
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• 2020

이 연구는 모델 스캐너로 석고 모형을 스캔한 디지털 모형(Model scanned digital model, MSD)과 구내 스캐너로 구강을 스캔한 디지털 모형(Intraoral scanned digital model, ISD)에서 계측한 치아 근원심 폭경(Tooth width, TW)과 치열궁 길이(Arch length, AL)의 신뢰도와 재현성, 치열궁 길이 편차(Arch length discrepancy, ALD) 분석의 타당도를 평가하였다. 만 12 - 18세의 남, 여 30명에게 석고 모형, MSD, ISD를 획득하고, 2번 계측한 TW, AL의 신뢰도는 Pearson 상관 분석, 4명의 재현성은 군간 상관 분석 그리고 TW, AL 및 ALD의 타당도는 대응표본 t검정으로 평가하였다. 결과적으로 모든 군에서 계측한 TW, AL는 높은 신뢰도와 재현성을 보였고 MSD군의 ALD분석은 적절한 타당도를 보였다. ISD 군의 TW는 가장 높은 타당도를 보인 반면에, AL와 ALD분석은 유의미하게 짧게 측정되어 낮은 타당도를 보였으므로 임상가는 디지털 모델을 이용하여 공간 분석 시행 시 이를 고려해야 할 것이다.

• 한국국방경영분석학회지
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• 제1권1호
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• pp.131-135
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• 1975

One of the pending issues of the Ministry of Defense is the efficient management of space parts for the weapon systems. It has been known that more than 000 million dollars are needed for spare parts for the weapon systems annually. Though the problem demands a serious consideration, there has not been any systematic study on the problem as far as the author knows. One way to approach the problem is through an investigation of the system reliability under constraints. A measure of how well a system performs or meets its design objectives is provided by the concept of system reliability. If successful operation is desired for a specified period of time, reliability is defined as the probability that the system will perform satisfactorily for the required time period. This interpretation of reliability is normally applied to devices which are subject to random failures such as electrical or mechanical systems. It has been found necessary to express system reliability in terms of the reliability of the components or subsystems which comprise the system. The major subsystems of an aircraft, for example, include the electronics, powerplant, airframe and armament subsystems. Therefore, the optimal spare part kit can be found by maximizing the system reliability subject to cost or other constraints.

• 한국시뮬레이션학회논문지
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• 제27권1호
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• pp.25-32
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• 2018

본 논문은 모델 기반 내장형 소프트웨어의 자동 생성 코드에 대한 효율적인 신뢰성 시험 절차와 구체화된 동적 시험 방안에 대해서 제시하고 있다. 모델 정적/동적 시험 각각을 코드 정적/동적 시험 전에 수행함으로서 코드 신뢰성 시험 수행의 이점이 있음을 기술하였다. 또한, 모델과 코드의 신뢰성 시험 상관관계를 모델의 경우 Model Advisor와 Verification and Validation tool, 코드의 경우 Polyspace와 LDRA를 이용하여 살펴보고 제시한 절차대로 수행한 신뢰성 시험의 결과를 보여주고 있다.

• 시스템엔지니어링학술지
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• 제12권2호
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• pp.19-27
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• 2016

Many countries concentrated on the space developments to enhance the national security and the people's quality of life. A space launch vehicle for accessing the space is a typical large complex system that is composed of the high-technology like high-performance, high-reliability, superhigh-pressure, etc. The project developing large complex system like space launcher is mostly conducted in the uncertain environment. To achieve a goal of the project, its success probability should be enhanced consistently by reducing its uncertainty during the life cycle: it's possible to reduce the project's uncertainty by performing the risk management (RM) that is a method for identifying and tracing potential risk factors in order to eliminate the risks of the project. In this paper, we introduce the risk management (RM) process applied for a Space Launch Vehicle R&D Project.