• 제목/요약/키워드: 신뢰도 최적설계

검색결과 496건 처리시간 0.026초

Reliability-Based Optimum Design for Tubular Frame Structures (골조 파이프 구조물의 최적신뢰성 설계)

  • 백점기
    • Journal of Ocean Engineering and Technology
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    • 제2권1호
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    • pp.95-105
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    • 1988
  • This paper describes the development of a reliability-based optimum design technique for such three dimensional tubular frames as off shore structures. The objective function is formulated for the structural weight. Constraints that probability of failure for the critical sections does not exceed the allowable probability of failure are set up. In the evaluation of the probability of failure, fatigue as well as buckling and plasticity failure are taken into account and the mean-value first-order second-moment method(MVFOSM) is applied for its calculation. In order to reduce the computing time required for the repeated structural analysis in the optimization process, reanalysis method is also applied. Application to two and three dimensional simple frame structures is performed. The influence of material properties, external forces, allowable failure probabilities and interaction between external forces on the optimum design is investigated.

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Topology Optimization Considering Reliability (신뢰성을 고려한 위상최적설계)

  • Min, Seung-Jae;Bang, Seung-Hyun
    • Proceedings of the KSME Conference
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.468-473
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    • 2004
  • New reliability-based topology optimization method is proposed by utilizing single-loop single vector approach, which approximate searching the most probable point in the probabilistic design domain analytically, to reduce the time cost and dealing with several constraints to handle practical design requirements. To examine uncertainties in the topology design of a structure, the modulus of elasticity of the material and applied loadings are considered as probabilistic design variables. The results of design examples show that the proposed method provides efficiency curtailing the time for the optimization process and accuracy satisfying the specified reliability.

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Reliability analysis of surface settlement during shield TBM tunneling (쉴드 TBM 터널 굴착시 지표침하에 관한 신뢰성해석)

  • Han, Myeong-Sik;Cho, Kuk-Hwan
    • Journal of Korean Tunnelling and Underground Space Association
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    • 제18권3호
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    • pp.305-318
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    • 2016
  • This study is to evaluate the uncertainty of the soil parameters associated with the Gap parameter during shield TBM tunnel excavation of ${\bigcirc}{\bigcirc}$ International Airport Terminal 2 connecting railway construction basic design. And This study is to evaluate the adequacy of the shield TBM design by performing a reliability analysis of the Surface settlement. In addition, By analyzing the reliability indices of the design constants and Sensitivity probability of failure to be used in designing an integer parameter Gap, and By evaluating the design constants of a great influence on the surface subsidence, it was to provide a basis for carrying out an optimum design.

Jansen mechanism을 이용한 4족 보행로봇 설계

  • No, Chi-Ho
    • Proceeding of EDISON Challenge
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    • 제6회(2017년)
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    • pp.602-607
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    • 2017
  • 본 연구는 4족 보행 로봇을 설계하기 위해 linkage of jansen mechanism을 선택하였고 설정한 보행 목적에 맞는 최적 링크의 길이를 구하기 위해 Edison SW를 사용하여 해석을 하고 수치적 해석을 동원하여 목표에 대한 신뢰를 높인다.

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Optimal Supersonic Diffuser Design of Integrated Rocket Ramjet Engine (IRR형 Ramjet Intake 초음속 확산부 형상 최적설계)

  • 민병영;이재우;변영환
    • Journal of the Korean Society of Propulsion Engineers
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    • 제6권2호
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    • pp.65-74
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    • 2002
  • Optimal supersonic diffuser shape of integrated rocket ramjet engine was derived which maximizes the total pressure recovery. Mass flux is considered as a design constraint and the second oblique shock angle of the external ramp, the cowl-lip angle and the throat area are selected as design variables. Refined response surface method through design space transformation technique was developed and employed, and high confidence level of the regression model could be obtained. Genetic algorithm was implemented for both system optimizer and subspace regression model optimization. Virtual nozzle was located at the end of throat to adjust the back pressure. With only 20 aerodynamic analyses, optimal supersonic diffuser shape which has 14% improved total pressure recovery characteristics was successfully designed.

The Multi-objective Optimal Design of Thermopile Sensor Having Beam or Membrane Structure (빔 혹은 멤버레인 구조를 가지는 써모파일 센서의 다목적 최적설계)

  • Lee, Jun-Bae;Kim, Tae-Yoon
    • Journal of Sensor Science and Technology
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    • 제6권1호
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    • pp.6-15
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    • 1997
  • This paper presents the multi-objective optimal design of thermopile sensor having beam or membrane structure. The thermopile sensor is composed of $Si_{3}N_{4}/SiO_{2}$ dielectric membrane, Al-polysilicon thermocouples and $RuO_{2}$ thin film for black body. The sensing method is based on the Seebeck effect which is originated from the temperature difference of the two positions, black body and silicon rim. The objective functions of the presented design are sensitivity, detectivity and thermal time constant. The modelling of the sensor is proposed including the package. The multi-objective optimization technique is applied to the design of the sensor not only inspecting the modelling equation but also simulating mathematical programming method. Especially, fuzzy optimization technique is adapted to get the optimal solution which enables the designer to reach the more practical solution. The design constraint of the voltage output originated from the change of the environmental temperature is included for practical use.

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Study of the Efficient Aerodynamic Shape Design Optimization Using the Approximate Reliability Method (근사신뢰도기법을 이용한 효율적인 공력 형상 설계에 관한 연구)

  • Kim Suwhan.;Kwon Jang-Hyuk
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2004년도 추계 학술대회논문집
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    • pp.187-191
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    • 2004
  • The conventional reliability based design optimization(RBDO) methods require high computational cost compared with the deterministic design optimization(DO) methods. To overcome the computational inefficiency of RBDO, single loop methods have been proposed. These need less function calls than that of RBDO but much more than that of DO. In this study, the approximate reliability method is proposed that the computational requirement is nearly the same as DO and the reliability accuracy is good compared with that of RBDO. Using this method, the 3-D viscous aerodynamic shape design optimization with uncertainty is performed very efficiently.

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System Reliability Analysis for Nonnormal Distributions and Optimization Using Experimental Design Technique (실험계획법을 이용한 비정규 분포에 대한 신뢰도 계산 방법과 최적 설계에의 적용)

  • Seo, Hyun-Seok;Chang, Jin-Ho;Kwak, Byung-Man
    • Proceedings of the KSME Conference
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    • 대한기계학회 2001년도 춘계학술대회논문집C
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    • pp.327-332
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    • 2001
  • An experimental design technique is developed for estimating the moments of system response functions. It is easy to implement and provides accurate results compared with other traditional methods. It is based on the work of Taguchi, later improved by D'Errico and Zaino. The existing experimental techniques, however, is applicable only for normally distributed cases. In this article the three-level Taguchi method is extended to obtain optimum choice for levels and weights to handle nonnormal distributions. A systematic procedure for reliability analysis is then proposed by using the Pearson system and the narrow system reliability bounds. Illustrative examples including a tolerance optimization problem are shown very accurate comparing with those by Monte-Carlo simulations and the first-order reliability method.

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An parameter optimization of SOVA decoder for the IMT-2000 complied Turbo code (IMT-2000 표준의 터보코드를 위한 SOVA 복호기 최적화 설계)

  • 김주민;정덕진
    • The Journal of Korean Institute of Communications and Information Sciences
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    • 제26권5B호
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    • pp.592-598
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    • 2001
  • IMT-2000에서는 이미 터보코드가 채널코딩 기법으로 제안되어 있으며 특별히 3GPP 규격에서는 제한길이 4인 1/3 터보코드가 채택되어 있다. 기존의 논문에서는 일반적인 터보 코드의 성능에 대한 분석이 많이 제시되어 왔으나, 3GPP 규격의 터보 복호를 위한 SOVA 복호기의 성능 파라미터 추출과 그에 따른 성능 분석 수행되지 않았다. 본 연구에서는 효율적인 구조의 3GPP SOVA 복호기를 설계하기 위해서 외부정보의 스케일링과 신뢰도 갱신길이 라는 두 가지 파라미터에 따른 SOVA 복호기의 성능을 분석하고 최적의 파라미터 값을 제시하고자 한다. 이 파라미터의 최적화를 위하여 C++를 이용한 모의실험 결과, 3GPP 규격의 (13,15) 1/3 코드에서 스케일링 값은 1/2로 신뢰도 갱신길이는 10으로 최적화 되었다.

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