• 제목/요약/키워드: design procedure

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A displacement-based seismic design procedure for buildings with fluid viscous dampers

  • Banuelos-Garcia, Francisco H.;Ayala, Gustavo;Lopez, Saul
    • Earthquakes and Structures
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    • 제18권5호
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    • pp.609-623
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    • 2020
  • This paper presents a displacement-based seismic design procedure for new structures with fluid viscous dampers and/or for existing structures, where these devices are required as a retrofit measure and damage control. To consider the non-proportional damping produced by these devices in a conventional modal spectral analysis, the effect of the fluid viscous dampers is approximated as the sum of a proportional damping matrix and a complementary matrix which is representative of non-proportional damping matrix. To illustrate the application of this procedure and evaluate the performance of structures designed with the procedure proposed, five regular plane frames: 8, 12, 17, 20 and 25-storey, and an 8-storey building are designed. The seismic demands used for design and validation were the records obtained at the SCT site during the 1985 Michoacan earthquake, and that of the 2017 Morelos - Puebla earthquake obtained at the Culhuacan site, both stations located on soft soil sites. To validate the procedure proposed, the performances and damage distributions used as design targets were compared with the corresponding results from the nonlinear step-by-step analyses of the designed structures subjected to the same seismic demands.

마찰 감쇠기를 사용한 구조물의 보강 설계법 제안 (Seismic Retrofit Design Procedure Using a Friction Damper)

  • 문기훈;한상환;조한철;이강석
    • 한국지진공학회논문집
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    • 제15권6호
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    • pp.45-53
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    • 2011
  • 본 연구의 목적은 마찰 감쇠기를 사용한 기존 구조물의 제진보강 설계절차를 제시하는 것이다. 보강된 구조물의 목표 지붕층 변위는 기존 구조물이 급격한 강도의 저감없이 보유내력을 발휘할 수 있는 최대변위를 초과하지 않도록 결정하였다. 보강 구조물의 변위는 비탄성 변위비 제안식을 이용하여 예측하였다. 제안된 방법의 유효성을 검증하기 위하여 80개의 지반운동 데이터를 사용하여 비선형 동적해석을 수행하였다. 해석결과 제안된 방법은 보강 구조물의 지붕층 변위를 정확히 예측할 수 있는 것으로 나타났다.

점진적 최적화 기법을 이용한 구조물의 위상 설계 (Topological design of structures using an evolutionary procedure)

  • 최창근;류명기;송명관
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 1996년도 가을 학술발표회 논문집
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    • pp.315-321
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    • 1996
  • The structural topology optimization presented in this paper is based on an evolutionary procedure, developed by Xie and Steven, in which the low stressed material of a structure is removed from the structure step-by-step until an optimal design is obtained. By appling this procedure a layout or topology of a structure can be found from a initial block of material. The purpose of this paper is to implement the evolutionary procedure, introduce some novel features and investigate its feasibility by studying a few examples.

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근사 극배치 개념에 의한 고정 차수 제어기 설계 (A Fixed-order Controller Design by the Approximate Pole Placement)

  • 고종문;허명준;이석원
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1999년도 추계학술대회 논문집 학회본부 B
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    • pp.472-474
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    • 1999
  • The design procedure originally proposed by Manabe is involved, because experiences and manual skills are necessary, especially, in the case of designing low fixed-order controllers for high-order plants, and the concept of manual skills are not clearly defined. So we propose a concept and a design procedure of Approximate Pole Placement that substitute for the manual skills. And the validity of the procedure is shown by example problems. Moreover, we also propose a procedure of adding the role of improving transient response performance to the feedforward compensator that previously has only the role of tracking in steady-state the validity of the procedure is also shown by example problems.

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MRA와 POD를 적용한 공력특성 최적설계 (MRA AND POD APPLICATION FOR AERODYNAMIC DESIGN OPTIMIZATION)

  • 구본찬;한준희;조태현;박경현;이도형
    • 한국전산유체공학회지
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    • 제20권2호
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    • pp.7-15
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    • 2015
  • This paper attempts to evaluate the accuracy and efficiency of a design optimization procedure by combining wavelets-based multi resolution analysis method and proper orthogonal decomposition (POD) technique. Aerodynamic design procedure calls for high fidelity computational fluid dynamic (CFD) simulations and the consideration of large number of flow conditions and design constraints. Thus, even with significant computing power advancement, current level of integrated design process requires substantial computing time and resources. POD reduces the degree of freedom of full system by conducting singular value decomposition for various field simulations. In this research, POD combined Design Optimization model is proposed and its efficiency and accuracy are to be evaluated. For additional efficiency improvement of the procedure, multi resolution analysis method is also being employed during snapshot constructions (POD training period). The proposed design procedure was applied to the optimization of wing aerodynamic performance. Throughout the research, it was confirmed that the POD/MRA design procedure could significantly reduce the total design turnaround time and also capture all detailed complex flow features as in full order analysis.

강구조물설계에서 부재선정의 시스템화 방법론 (Member Selection Procedure in the Steel Structural Design)

  • 이영호;김상철;김흥국;이병해
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 1995년도 가을 학술발표회 논문집
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    • pp.197-206
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    • 1995
  • In structural design procedure, The procedure of member selection manages complex data relationship and reflects structural expert's knowledge. It is a difficult problem to construct an effective system with the conventional l programming technique. Knowledge_based s!'stem is a software system capable of supporting the explicit representation of expert's knowledge in member selection process through member data and reasoning mechanisms. This study describes useful methodology for structuring knowledge and representing relation between member data and knowledge. And this study shows the application of this member for member selection in the steel structural design.

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비용요소를 고려한 치수공차설계 (Dimension-Tolerance Design with Cost Factors)

  • 강병철;윤원영
    • 품질경영학회지
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    • 제26권1호
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    • pp.172-191
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    • 1998
  • In this paper, dimension tolerance design for components is studied. Three cost factors are considered: machining cost, rework cost, and loss related to product quality which is affected by the tolerances of components. We propose a procedure to determine the optimal tolerances of components and a, pp.y the procedure to design the tolerances of fine motion stage in semicoduct machine. We compare the proposed procedure with the existing model for determining tolerance economically.

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Assessment of FEMA356 nonlinear static procedure and modal pushover analysis for seismic evaluation of buildings

  • Khoshnoud, Hamid Reza;Marsono, Kadir
    • Structural Engineering and Mechanics
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    • 제41권2호
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    • pp.243-262
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    • 2012
  • Nonlinear static analysis as an essential part of performance based design is now widely used especially at design offices because of its simplicity and ability to predict seismic demands on inelastic response of buildings. Since the accuracy of nonlinear static procedures (NSP) to predict seismic demands of buildings affects directly on the entire performance based design procedure, therefore lots of research has been performed on the area of evaluation of these procedures. In this paper, one of the popular NSP, FEMA356, is evaluated and compared with modal pushover analysis. The ability of these procedures to simulate seismic demands in a set of reinforced concrete (RC) buildings is explored with two level of base acceleration through a comparison with benchmark results determined from a set of nonlinear time history analyses. According to the results of this study, the modal pushover analysis procedure estimates seismic demands of buildings like inter story drifts and hinges plastic rotations more accurate than FEMA356 procedure.

계기비행절차 설계 프로그램 개발 (Development of a Design Program for Instrument Flight Procedure)

  • 송재훈;김혁;정홍기;이장연
    • 항공우주기술
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    • 제13권2호
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    • pp.185-193
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    • 2014
  • 본 논문에서는 계기비행절차 설계 프로그램 개발 과정을 개괄적으로 살펴보고자 한다. 제품의 시장 경쟁력 강화를 위하여 외산 제품에 대하여 조사하고 분석하였다. 개발 요구조건 도출을 위하여 계기비행절차 설계 기준에 대하여 살펴보고, 소프트웨어 프로그램 개발 및 시험평가 과정에 대하여 설명하였다.

Robust model matching design using normalized left coprime factorization approach

  • Hanajima, Naohiko;Eisaka, Toshio;Yanagita, Yoshiho;Tsuchiya, Takeshi;Tagawa, Ryozaburo
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국제학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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    • pp.360-365
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    • 1993
  • In this paper, we propose a new design procedure of the Robust Model Matching(RM) using the Normalized Left Coprime Factorization (NLCF) approach. The RMM aims at reducing the sensitivity of a given control system, but standard design procedures are not for robust stability. Therefore we try applying the robust stability condition based on NLCF to RMM procedure. We first formulate the RMM using the robust stability condition of NLCF approach, then we propose the new procedure of the RMM. The point is that the condition includes the measure of sensitivity of the RMM. In the proposed procedure, a cost function is determined through the condition and solved by H$_{\infty}$ contro technique. Finally we show a design example and check the performance..

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