• Title/Summary/Keyword: 제약성 최적화

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Optimization of a System Reliability by Zero-One Programming with GUB Structure (GUB 구조를 갖는 0-1 프로그래밍에 의한 시스템 신뢰성의 최적화)

  • Lee, Jae-Uk;Chun, Koo-Chae;Gen, Mitsuo
    • Journal of the Korean Institute of Telematics and Electronics
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    • v.26 no.2
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    • pp.124-131
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    • 1989
  • This paper showed that the system reliability optimization problem with sereval failure modes at each subsystem can be treated as efficient computational algorithm proposed here. This algorithm was developed by considering a generalized upper bounding which always exists in constraints when the system reliability optimization problem may be reformulated as 0-1 integer programming problem. We demonstrated the optimal allocation of redundant units for system reliability by using the proposed algorithm. Our algorithm is superior to others in terms of number of iterations and variables used.

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Three-Dimensional Offshore Wind Turbine Blade Design by using Efficient Two Step Optimization (효율적인 2단계 최적화를 통한 3차원 해상풍력터빈 블레이드 설계)

  • Lee, Ki-Hak;Hong, Sang-Won;Jeong, Ji-Hoon;Kim, Kyu-Hong;Lee, Dong-Ho;Lee, Kyung-Tae
    • 한국신재생에너지학회:학술대회논문집
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    • 2007.06a
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    • pp.432-436
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    • 2007
  • 본 연구의 목적은 3차원 풍력터빈 블레이드 최적형상설계를 위한 실용적이고 효율적인 설계 과정을 구현하는 것이다. 국내 연안의 해상풍력에 적용하기 위해서 통계적 모델을 이용하여 풍황 자료를 분석하였다. 설계에 관련된 많은 수의 설계변수를 효과적으로 관리하기 위해서 설계과정은 운용조건 최적화와 블레이드 형상설계의 2단계로 구성하였다. 실험계획법에 의해 추출된 각 운용조건점은 형상설계를 위한 입력값으로 제공된다. 형상설계 단계에서는 최소에너지손실 조건과 결합된 BEMT를 이용하여 각 블레이드 단면에서의 시위길이와 피치각 분포를 최적화하였다. 블레이드 단면 익형은 NREL S830을 이용하였고, 익형의 공력성능은 XFOIL을 이용하여 예측하였다. 설계된 블레이드 형상의 성능해석을 수행하고 그 결과를 바탕으로 반응면을 구성하였다. 좀 더 나은 성능을 가진 블레이드 형상을 찾기 위해서 초기설계공간에서 확률적 방법을 이용하여 타당성 있는 설계공간까지 운용조건 설계변수를 이동시키고 구배최적화 기법을 통해 각각의 제약함수를 만족하면서 연평균발생에너지를 최대로 하는 최적블레이드 형상을 구현하였다. 제시된 최적설계과정은 풍력터빈블레이드 개발에 실용적이고 신뢰성 있는 설계툴로서 사용이 가능하다.

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Three-Dimensional Offshore Wind Turbine Blade Design by using Efficient Two Step Optimization (효율적인 2단계 최적화를 통한 3차원 해상풍력터빈 블레이드 설계)

  • Lee, Ki-Hak;Hong, Sang-Won;Jeong, Ji-Hoon;Kim, Kyu-Hong;Lee, Dong-Ho;Lee, Kyung-Tae
    • New & Renewable Energy
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    • v.3 no.3
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    • pp.63-71
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    • 2007
  • 본 연구의 목적은 3차원 풍력터빈 블레이드 최적형상설계를 위한 실용적이고 효율적인 설계과정을 구현하는 것이다. 국내 연안의 해상풍력에 적용하기 위해서 통계적 모델을 이용하여 풍황자료를 분석하였다. 설계에 관련된 많은 수의 설계변수를 효과적으로 관리하기 위해서 설계과정은 운용조건 최적화와 블레이드 형상설계의 2단계로 구성하였다. 실험계획법에 의해 추출된 각 운용조건 설계점은 형상설계를 위한 입력 값으로 제공된다. 형상설계 단계에서는 최소에너지손실 조건과 결합된 BEMT를 이용하여 각 블레이드 단면에서의 시위길이와 피치각 분포를 최적화하였다. 블레이드 단면 익형은 NREL S830을 이용하였고, 익형의 공력성능은 XFOIL을 이용하여 예측하였다. 설계된 블레이드 형상의 성능해석을 수행하고 그 결과를 바탕으로 반응면을 구성하였다. 좀 더 나은 성능을 가진 블레이드 형상을 찾기 위해서 초기설계공간에서 확률적 방법을 이용하여 타당성 있는 설계공간까지 운용조건 설계변수를 이동시키고 구배최적화 기법을 통해 각각의 제약함수를 만족하면서 연간에너지생산량을 최대로 하는 최적블레이드 형상을 구현하였다. 제시된 최적설계과정은 풍력터빈블레이드 개발에 실용적이고 신뢰성 있는 설계툴로서 사용이 가능하다.

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Generation Scheduling with Wind Power Generator (풍력발전원을 고려한 발전기 기동정지계획)

  • Lee, Jae-Hee;Kim, Jin-A;Joo, Sung-Kwan
    • Proceedings of the KIEE Conference
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    • 2009.07a
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    • pp.593_594
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    • 2009
  • 발전기 기동정지 계획은 다수의 발전기의 운영에서 비용을 최소화할 수 있는 기동 및 정지 시간을 결정하는 것이다. 대규모의 계통에서의 기동정지계획은 복잡한 계통 및 발전기 특성 제약이 시계열적으로 작용하기 때문에 최적화 분야에서도 어려운 문제에 해당한다. 더욱이 최근 증가하는 풍력발전원은 그 출력이 풍속에 따라 시시각각 변동하기 때문에 기동정지계획에서 함께 고려되는 것이 힘들었다. 본 논문은 이러한 풍력발전 출력의 불확실성을 랜덤발생하여 기댓값을 최적화하는 발전기 기동정지계획을 통해 풍력발전원이 기동정지계획에 미치는 영향을 분석하였다. 제시하는 방법으로 모의계통의 사례연구를 통해 유용성을 입증하였다.

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Preliminary Hull Form Generation by Form Parameter Method using GA (GA를 이용한 Form parameter 방법에 의한 초기선형 생성)

  • Kim, Su-Young;Shin, Sung-Chul;Shin, KYoung-Yup
    • Journal of the Korean Institute of Intelligent Systems
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    • v.12 no.1
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    • pp.44-51
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    • 2002
  • In order to generate hull form, fairness criteria applies to object function, B-spline curve vertices are considered as design variables, optimization is proceeded with satisfying geometric constraint conditions. GA(Genetic Algorithm) and optimality criteria apply to optimization process in this study.

A Study on Form Parameter Method by Optimum Vertex Point Search (조정점 최적탐색에 의한 Form Parameter 방법에 관한 연구)

  • 김수영;신성철;김덕은
    • Journal of the Society of Naval Architects of Korea
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    • v.39 no.4
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    • pp.60-65
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    • 2002
  • In order to generate hull form, we introduced optimization process. Fairness criteria is applied to object function, B-Spline control vertices are considered as design variables, optimization is proceeded with satisfying geometric constraint conditions. GA(Genetic Algorithm) and optimality criteria are applied to optimization process in this study.

Mathematical modeling approach for classroom assignment problem (수리적 모델링을 통한 강의실 배정문제 해법에 관한 연구)

  • Ahn, Namsu
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.18 no.10
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    • pp.580-587
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    • 2017
  • Recently, as the education population of Korea has been rapidly declining, many changes have been taking place in the university environment. Especially, community colleges linked to local communities have responded to these crises through various educational changes, such as three-year study transfers, work-parallelism, and employee commissioned education. However, such changes in the contents of education are causing a new type of classroom allocation problem, in which it is difficult to assign the limited number of classrooms to the major courses. In this paper, we classified the constraints involved in assigning classrooms into absolute constraints and relative constraints, mathematically modeled them, and allocated the classrooms optimally through optimization software. The results were satisfactory and enabled us to obtain superior results in terms of the various performance indices (classroom utilization rate, teacher satisfaction, etc.) than when assigning classrooms in the normal way.

Flying-Wing Type UAV Design Optimization for Flight Stability Enhancement (전익기형 무인기의 비행 안정성 향상을 위한 형상 최적화 연구)

  • Seong, Dong-gyu;Juliawan, Nadhie;Tyan, Maxim;Kim, Sanho;Lee, Jae-woo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.48 no.10
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    • pp.809-819
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    • 2020
  • In this study, the twist angle and wing planform shapes were selected as design variables and optimized to secure the stability of the flying-wing type UAV. Flying-wing aircraft has no separated fuselage and tails, which has advantages in aerodynamic characteristics and stealth performance, but it is difficult to secure the flight stability. In this paper, the sweep back angle and twist angle were optimized to obtain the lateral stability, the static margin and wing planform shapes were optimized to improve the longitudinal stability of the flying-wing, then effect of the twist angle was confirmed by comparing the stability of the shape with the winglet and the shape with the twist angle. In the optimization formulation, focusing on improving stability, constraints were established, objective functions and design variables were set, then design variable sensitivity analysis was performed using the Sobol method. AVL was used for aerodynamic analysis and stability analysis, and SQP was used for optimization. The CFD analysis of the optimized shape and the simulation of the dynamic stability proved that the twist angle can be applied to the improvement of the lateral stability as well as the stealth performance in the flying-wing instead of the winglet.

A Study for Performance Evaluation of Distributed Mobility Management based on Proxy Mobile IPv6 (PMIPv6기반의 분산 이동성 관리 방식의 성능 평가에 관한 연구)

  • Wie, Sunghong;Jang, Jaeshin
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.19 no.1
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    • pp.97-105
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    • 2015
  • Recently, due to an explosive growth of the internet traffic, the limitations of a current framework for a mobility management have been focused. The current centralized mobility management is prone to several problems and limitations: suboptimal routing, low scalability, signaling overhead, and a single point of failure. To overcome these problems and limitations, IETF is working about the distributed mobility management scheme that the centralized mobility functions of HA(Home Agents) are distributed to networks edges such as access routers. These distributions of mobility functions overcome the limitations of the centralized mobility managements and go with the trend of flat networks e.g. more simple network architecture. This paper analyzes the distributed mobility management based on Proxy Mobile IPv6 and demonstrates the performance superiority.

Opitmal Design Technique of Nielsen Arch Bridges by Using Genetic Algorithm (유전자 알고리즘을 이용한 닐센아치교의 최적설계기법)

  • Lee, Kwang Su;Chung, Young Soo
    • Journal of Korean Society of Steel Construction
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    • v.21 no.4
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    • pp.361-373
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    • 2009
  • Using the genetic algorithm, the optimal-design technique of the Nielsen arch bridge was proposed in this paper. The design parameters were the arch-rise ratio and the steel weight ratio of the Nielsen arch bridge, and optimal-design techniques were utilized to analyze the behavior of the bridge. The optimal parameter values were determined for the estimated optimal level. The parameter determination requires the standardization of the safety, utility, and economic concepts as the critical factors of a structure. For this, a genetic algorithm was used, whose global-optimal-solution search ability is superior to the optimization technique, and whose object function in the optimal design is the total weight of the structure. The constraints for the optimization were displacement, internal stress, and time and space. The structural analysis was a combination of the small displacement theory and the genetic algorithm, and the runtime was reduced for parallel processing. The optimal-design technique that was developed in this study was employed and deduced using the optimal arch-rise ratio, steel weight ratio, and optimal-design domain. The optimal-design technique was presented so it could be applied in the industry.