• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2003년도 유체기계 연구개발 발표회 논문집
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• pp.397-403
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• 2003

In an attempt to solve multiobjective optimization problems, weighted sum method is most widely used for the advantage that a designer can consider the relative significance of each object functions by weight values but it can be highly sensitive to weight vector and occasionally yield a deviated optimum from the relative weighting values designer designated because the multiobjective function has the form of simple sum of the product of the weighting values and the object functions in traditional approach. To search the design solution well agree to the designer's weighting values, we proposed new multiobjective function which is the functional of each normalized objective functions and considered to find the design solution comparing the distance between the characteristic line and the ideal optimum. In this study, proposed multiobjective function was applied to design high efficiency and low noise axial flow fan and the result shows this approach will be effective for the case that the qualify of the design can be highly affected by the designer's subjectiveness represented as weighting values in multiobjective design optimization process.

• 한국경영과학회:학술대회논문집
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• 한국경영과학회 2005년도 추계학술대회 및 정기총회
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• pp.338-341
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• 2005

In this paper, we present analytic forms of the ordered weighted averaging (OWA) operator weighting functions, each of which has properties of rank-based weights and a constant level of orness, irrespective of the number of objectives considered. These analytic forms provide significant advantages for generating OWA weights over previously reported methods. First, OWA weights can be efficiently generated by use of proposed weighting functions without solving a complicated mathematical program. Moreover, convex combinations of these specific OWA operators can be used to generate OWA operators with any predefined values of orness once specific values of orness are α priori stated by decision maker. Those weights have a property of constant level of orness as well. Finally, OWA weights generated at a predefined value of orness make almost no numerical difference with maximum entropy OWA weights in terms of dispersion.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1998년도 하계학술대회 논문집 B
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• pp.549-551
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• 1998

In this paper, we design the optimal satellite-tracking antenna $H_{\infty}$ control system using genetic algorithm(GA). To do this, we give gain and dynamics parameters to the weighting functions and apply GA with reference model to the optimal determination of weighting functions and design parameter ${\gamma}$ that are given by Glover-Doyle algorithm which can design $H_{\infty}$ controller in the state space. These weighting functions and design parameter ${\gamma}$ are simultaneously optimized in tile search domain guaranteeing the robust stability of closed-loop system. The effectiveness of this satellite-tracking antenna $H_{\infty}$ control system is verified by computer simulation.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1997년도 하계학술대회 논문집 B
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• pp.587-589
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• 1997

In this paper we design the model following ${\mu}$-synthesis control system for optimal fuel-injection of diesel engine using genetic algorithms. To do this, we give gain and dynamics parameters to the weighting functions and apply genetic algorithms with reference model to the optimal determination of weighting functions that are given by D-K iteration method which can design ${\mu}$-synthesis controller in the state space. These weighting functions are optimized simultaneously in the search domain selected adequately. The effectiveness of this ${\mu}$-synthesis control system for fuel-injection is verified by computer simulation.

• 한국염색가공학회지
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• 제9권6호
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• pp.51-57
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• 1997

The lightness, chroma and hue tolerances with respect to the standard colour position in the CIELAB space have been studied in detail using the various existing data sets and the set form this study. The lightness tolerance showed a clear dependency upon the metric lightness for medium to light colour, but in the case of dark colours there was a discrepancy between the data sets. Both the chroma and hue tolerances showed dependency upon both the chroma and hue-angle and not the single dependency upon the metric chroma, as assumed in the CIE94 formula. New weighting functions were derived from the above experimental evidence, and finally a new formula, LCD(Leeds Colour Difference) was proposed. The LCD formula is nearly as simple and flexible as CIE94 but smoothes the individual weighting functions, especially for lightness tolerances for light colours and chromaticity discrimination near the blue region.

• 한국도로학회논문집
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• 제11권1호
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• pp.47-58
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• 2009

요금을 지불하게 되는 유료도로에 대해서는 별도의 가중치를 산정하여 교통계획 모형 내에서 모델링 할 수 있도록 해야 하나 현존하는 유료도로의 가중치 산정방법에서 발생하는 문제점은 현실과 유사한 통행패턴을 설명하기에 부적당하다. 본 연구는 국가교통DB센터에서 이미 정산된 가중치, 차종별 시간가치를 적용한 가중치 그리고 차로수별 교통량 비율로 수정된 가중치로서 총 세 개의 대안을 선정하여 비교 분석하였다. 그 결과 국가교통DB센터에서 정산되어 차로수의 구분없이 동일한 가중치를 적용하였을 경우에는 허용오차범위 내에 포함된 샘플수가 다른 시나리오에 비해 비교적 다수 포함되었으나 현재 유료도로의 차로수별 할인율과 할증률을 반영하지 않고 정산되었다는 점에서 현실에 맞지 않는 방법론으로 분석되었다. 또한 차종별 시간가치를 이용한 가중치는 현재 적용되는 가중치 중에서 가장 이론적으로 정립되었다고 할 수 있으나 가중치의 비율이 낮게 적용됨으로서 배정교통량이 과다예측 되는 결과로 나타났다. 그러나 차종별 시간가치와 차로수별 교통량 비율을 합산하여 재 산정한 가중치를 적용한 결과는 세 개의 대안 중 가장 현실에 근접한 통행배정 결과로 분석되었다. 또한 통행배정 방법에 있어 총량OD평형배정방법이 PCU통행배정방법보다 현실에 가까운 배정결과가 나타나는 것으로 나타났다.

• 한국유체기계학회 논문집
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• 제7권2호
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• pp.7-13
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• 2004

In an attempt to solve multiobjective optimization problems, weighted sum method is most widely used for the advantage that a designer can consider the relative significance of each object functions by weight values but it can be highly sensitive to weight vector and occasionally yield a deviated optimum from the relative weighting values designer designated because the multiobjective function has the form of simple sum of the product of the weighting values and the object functions in traditional approach. To search the design solution agree well to the designer's weighting values, we proposed new multiobjective function which was the functional of each normalized objective functions and considered to find the design solution comparing the distance between the characteristic line and the ideal optimum. In this study, proposed multiobjective function was applied to design high efficiency and low noise axial flow fan and the result shows this approach is effective for the case that the quality of the design can be highly affected by the designer's subjectiveness represented as weighting values in multiobjective design optimization process.

• 전기학회논문지
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• 제62권10호
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• pp.1425-1435
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• 2013

The useful method for determining parameters of weighting functions used to design the $H_{\infty}$ current controller for attenuating the current ripple due to saliencies which SPMSM(Surface Permanent Magnet Synchronous Motor) also incorporates is described. To analyze the effect, the current ripple due to the structural and the saturation saliencies, the SPMSM model with nonlinear inductance function depending on the two independent variables, rotor position and stator current is simulated. After analysis, parameters of the weighting functions for $H_{\infty}$ current controller is selected to satisfy the robust stability, robust performance and specific performance in time and frequency domain by using the PSO(Particle Swarm Optimization) algorithm in the linear SPMSM model. Especially, the robust performance is proved that the selected weighting functions play a role in reducing the current ripple caused by the saliencies of SPMSM at the desired frequency range by the simple experiment.

• 전기전자학회논문지
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• 제1권1호
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• pp.19-30
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• 1997

인공위성 추적 안테나 제어 시스템은 로테이터에 해당하는 DC 서보모터에 의해 안테나의 방위각 및 앙각을 제어함으로써 인공위성의 현재 위치를 추적하고자 하는 시스템이다. 한편 제어 시스템의 설계를 위한 위성추적 시스템의 선형모델은 일반적인 DC 서보모터의 위치 제어 시스템과는 달리 바람에 의한 토오크 외란과 베어링 및 공기역학적 마찰로 인한 전달함수의 파라메타 변동이 존재하므로 이러한 시스템의 불확실성에도 불구하고 만족스러운 명령추종성를 가지는 강인한 제어 시스템의 설계가 요구된다. 본 연구에서는 유전 알고리즘을 사용하여 복잡한 최적화의 과정없이 가중치 함수와 설계 파라메타 ${\gamma}$를 동시에 최적화함으로써 시스템의 파라메타 변동에 대한 강인한 안정성과 기준모델에 따른 최적의 명령추종성을 가지는 위성추적 안테나 $H{\infty}$ 제어 시스템을 설계한다. 이를 위해 강인한 안정성을 가지는 해집단내에서 기준모델의 출력을 최적으로 추종하도록 유전 알고리즘을 사용하여 적절히 주어진 가중치 함수의 게인 및 동특성 파라메타와 설계 파라메타 ${\gamma}$를 동시에 최적화한다. 끝으로 컴퓨터 시뮬레이션을 통하여 설계된 위성추적 안테나 $H{\infty}$ 제어 시스템의 유용성을 확인한다.

• 제어로봇시스템학회논문지
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• 제4권2호
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• pp.163-169
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• 1998

In this paper, we design an optimal model following ${\mu}-$synthesis control system for fuel-injection of diesel engine which has robust performance and satisfactory command tracking performance in spite of uncertainties of the system. To do this, we give gain and dynamics parameters to the weighting functions and apply genetic algorithm with reference model to the optimal determination of the weighting functions that are given by the D-K iteration method which can design ${\mu}-$synthesis controller in the state space. These weighting functions are optimized simultaneously in the search domain which guarantees the robust performance of the system. The ${\mu}-$synthesis control system for fuel-injection designed by the above method has not only the robust performance but also a better command tracking performance than those of the ${\mu}-$synthesis control system designed by trial-and-error method. The effectiveness of this ${\mu}-$synthesis control system for fuel-injection is verified by computer simulation.