• 한국구조물진단유지관리공학회 논문집
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• 제16권1호
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• pp.27-34
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• 2012

본 연구에서는 기존의 모르타르 충전식 슬리브 철근이음에 대한 부착강도식으로부터 유도한 이 철근이음의 파괴모드 추정방법을 이용하여, AIJ 규준에 의하여 평가한 이 슬리브 철근이음의 강성을 검토하였다. 이것을 위하여 261개 모르타르 충전식 슬리브 철근이음의 기존 실험자료를 채택하여 실험의 결과를 분석한 결과에 의하면 모르타르 충전식 철근이음의 파괴모드 추정방법은 돌기가 없는 강관 슬리브에 SD500 철근을 사용한 철근이음을 제외한 모르타르 충전식 슬리브 철근이음에 대한 강성을 효과적으로 평가할 수 있었다. 그리고 이 슬리브 철근이음의 파괴모드 추정방법에 적용하여 철근의 인장파단 영역에 있는 실험체 중에 주물 슬리브와 돌기가 있는 강관 슬리브를 사용한 실험체에서 SD400 철근을 사용한 경우는 98%, SD500 철근을 사용한 경우는 모든 실험체가 단조가력 시의 강성이 AIJ 규준의 A급 이상인 것으로 나타났고, 철근의 인장파단 영역에 있는 모든 실험체는 슬리브의 종류와 슬리브에 매입한 철근 종류에 관계없이 반복가력 시의 강성이 AIJ 규준의 A급 이상인 것으로 나타났다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.876-881
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• 2003

Reliable attitude estimation during the launch and early orbit phase is a critical issue for a satellite. Typically gyroscopes and other sensors are utilized to estimate the attitude during this phase. It is difficult to estimate the attitude quickly and reliably using gyroscopes because it requires a large computational load and accurate sensor measurements. Furthermore, the gyroscope failure may lead to the loss of the satellite. This paper suggests a simple attitude estimation method of a low earth orbit satellite without using gyroscopes, but only using sun sensors and magnetometers in the sun-acquisition mode. Using Kompsat-I telemetry data, we verified that the suggested algorithm provides attitude estimation within 3 degrees on each axis.

• 품질경영학회지
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• 제36권1호
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• pp.31-39
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• 2008

This paper proposes a method of estimating the lifetime distribution at use condition for constant stress accelerated life tests when an infant-mortality failure mode as well as wear-out one exists. General limited failure population model is introduced to describe these failure modes. It is assumed that the log lifetime of each failure mode follows a location-scale distribution and a linear relation exists between the location parameter and the stress. An estimation procedure using the expectation and maximization algorithm is proposed. Specific formulas for Weibull distribution are obtained. An illustrative example and the simulation results are given.

• 한국경영과학회지
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• 제20권3호
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• pp.43-59
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• 1995

This paper presents a method for estimating the population variability distribution of the failure parameter (failure rate or failure probability) for each failure mode considered in PSA (Probabilistic Safety Assessment). We focus on the utilization of generic estimates from various industry compendia for the estimation. The estimates are complicated statistics of failure data from plants. When the failure data referred in two or more sources are overlapped, dependency occurs among the estimates provided by the sources. This type of problem is first addressed in this paper. We propose methods based on ML-II estimation in Bayesian framework and discuss the characteristics of the proposed estimators. The proposed methods are easy to apply in real field. Numerical examples are also provided.

• 한국콘크리트학회:학술대회논문집
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• 한국콘크리트학회 2003년도 봄 학술발표회 논문집
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• pp.311-314
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• 2003

Concrete structures such as bridge, pavement, airfield, and offshore structure are normally subjected to repeated load. This paper proposes a failure probability models of concrete subjected to split tension repeated-loads, based on experimental results. The fatigue tests were performed at the stress ratio of 0.1, the loading shape of sine, the frequency of 20Hz, and the stress levels of 90, 80 and 70%. The fatigue test specimen was 150mm in diameter and 75mm in thickness. The fatigue analysis did not include which exceeded 0.9 of statistical coefficient of determination values or did not failure at 2$\times$$10^6$ cycles. The graphical method, the moment method, and maximum likelihood estimation method were used to obtain Weibull distribution parameters. The goodness-of-fit test by Kolmogorov-Smirnov test was acceptable 5% level of significance. As a result, the proposed failure probability model based on the two-parameter($\alpha and \mu$) Weibull distribution was good enough to estimate accurately the fatigue life subjected to tension mode.

• 산업공학
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• 제25권4호
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• pp.422-430
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• 2012

In this article, we introduced the estimation method by 'Safety Integrity Level'(SIL) for the criterion of safety assurance and performed a case study on a flame scanner. SIL requires probabilistic evaluation of each set of equipment used to reduce risk in a safety related system. FMEDA(Failure Modes, Effects and Diagnostic Analysis) method is widely used to evaluate the safety levels and provides information on the failure rates and failure mode distributions necessary to calculate a diagnostic coverage factor for a part or a component. Basically, two parameters resulting from FMEDA are used for SIL classification of the device : SFF(Safe Failure Fraction) and PFD(Probability of Failure on Demand). In this case study, it is concluded that the flame scanner is designed to fulfill the condition of SIL 3 in the aspect of SFF and PFD.

• 한국지반공학회논문집
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• 제19권5호
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• pp.175-187
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• 2003

일반적으로 사질토 지반의 원형수직구에 설치된 흙막이벽에 작용하는 토압은 삼차원 아칭효과로 인하여 평면변형조건의 옹벽에 작용하는 토압과는 다르며, 원통형 벽체의 설계를 위해서는 벽체에 작용하는 토압의 정확한 산정이 필요하다. 원형수직구에 설치된 벽체 배면지반의 파괴모드는 지중응력상태에 의존하게 되는데, 파괴모드는 실질적으로 원기둥형 활동면을 갖는 경우와 깔대기형 파괴면을 갖는 경우로 구분할 수 있다. 기존의 연구결과에 의하면 각각의 파괴모드에 대하여 원통형 벽체에 작용하는 토압공식이 제안되었으나, 도입된 가정으로 인하여 불합리한 경향을 보이는 문제점이 있다. 본 연구에서는 원통형 벽체에 작용하는 토압을 산정하기 위하여 각각의 파괴모드에 대하여 제안된 토압공식을 살펴보고, 각 토압공식에서 가정된 사항을 수정 제안하였다. 각각의 파괴모드에 대하여 수정 제안된 토압공식들은 상재하중과 벽면마찰을 고려하였으며, 활동면에서의 힘의 평형관계를 실제적으로 고려하였다.

• Journal of Mechanical Science and Technology
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• 제20권8호
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• pp.1224-1231
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• 2006

The stability and control derivatives of DURUMI-lI UAV using the flight test are obtained. The flight test data is gathered from the normal flight condition (normal mode) and the flight condition assumed as the right elevator fixed (fault mode). Using real-time parameter estimation techniques, applied to Fourier transform regression method, simulates the aircraft motion. From the result, the fault of control surface is to be detected. In this paper, the results of the real- time parameter estimation techniques are compared with the results of the Advanced Aircraft Analysis (AAA). Using the aerodynamic derivatives, it provides the base line of normal/failure for the control surface by using the on-line parameter estimation of Fourier transform regression. In flight, this approach maybe helpful to detect and isolate the fault of primary control surface. It is explained how to perform the flight condition assumed as the right elevator fixed in the flight test. Also, it is mentioned how to switch between the normal flight condition and the assumed fault flight condition.

• 대한기계학회논문집A
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• 제32권12호
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• pp.1123-1131
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• 2008

This paper provides V-factor estimation under combined mechanical and thermal load for circumferential cracks. Results are based on finite element analyses and effect of types and magnitudes of the thermal stress, crack geometry, the loading mode and plastic strain hardening on variations of the V-factor are investigated. The results of finite element analyses are compared with R6 values. As a result, it is shown that R6 gives generally conservative results. The conservatism is especially increased for the combination of large mechanical and thermal load. As a result, new estimation method which uses failure assessment line in R6 is proposed for V-factor and gives less conservative results.

• 한국경영과학회:학술대회논문집
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• 대한산업공학회/한국경영과학회 2000년도 춘계공동학술대회 논문집
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• pp.381-384
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• 2000

This paper proposes a method of estimating the lifetime distribution at use condition for constant stress accelerated lift tests when extrinsic failure mode as well as intrinsic one exists. A mixture of two log-normal distributions is introduced to describe these failure modes and it is assumed that a linear relation exists between the location parameter and stress. An estimation procedure using the expectation and maximization algorithm is proposed and a numerical example is given.