• 한국소음진동공학회논문집
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• 제23권1호
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• pp.84-91
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• 2013

Ultrasonic flip-chip bonding needs a precise bonding tool which delivers ultrasonic energy into chip bumps effectively to use the selected resonance mode and frequency of the horn structure. The bonding tool is excited at the resonance frequency and the input and output ports should locate at the anti-nodal points of the resonance mode. In this study, we propose new design method with topology optimization for ultrasonic bonding tools. The SIMP(solid isotropic material with penalization) method is used to formulate topology optimization and OC(optimal criteria) algorithm is adopted for the update scheme. MAC(modal assurance criterion) tracking is used for the target frequency and mode. We fabricate two prototypes of ultrasonic tools which are based on 3D optimization models after reviewing 2D and 3D topology optimization results. The prototypes are satisfied with the ultrasonic frequency and vibration amplitude as the ultrasonic bonding tools.

• 한국전자통신학회논문지
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• 제17권2호
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• pp.245-254
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• 2022

본 논문에서는 항 재밍 GPS 안테나의 설계 최적화에 관하여 연구하였다. 이를 위해 항 재밍 성능 분석 기준 및 방법을 제시하였다. 제시된 방법을 적용하기 위한 안테나 시스템의 구조는 7개의 방사소자가 배열된 구조이다. 여기서 6개 방사소자는 원형 등각 배열되었으며, 나머지 1개 방사소자는 원형 중앙에 배치하였다. 제시된 기준 및 방법을 기반으로 상기 안테나를 최적화 하였으며, 최적화된 안테나의 설계 요소(원형 배열의 반지름)의 전기적 길이는 0.48 λ이다. 모의실험 결과, 주 빔의 조향각도(θ, ϕ)가 (0°, 0°)인 경우, 항 재밍을 위한 패턴 널 형성 범위(θ 기준)가 57°부터 90°가 됨을 확인하였다.

• Structural Engineering and Mechanics
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• 제75권4호
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• pp.477-485
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• 2020

Finite element (FE) model based structural damage detection (SDD) methods play vital roles in effectively locating and quantifying structural damages. Among these methods, structural model updating should be conducted before SDD to obtain benchmark models of real structures. However, the characteristics of updating parameters are not reasonably considered in existing studies. Inspired by the l_∞ norm regularization, a novel anti-sparse representation method is proposed for structural model updating in this study. Based on sensitivity analysis, both frequencies and mode shapes are used to define an objective function at first. Then, by adding l_∞ norm penalty, an optimization problem is established for structural model updating. As a result, the optimization problem can be solved by the fast iterative shrinkage thresholding algorithm (FISTA). Moreover, comparative studies with classical regularization strategy, i.e. the l₂ norm regularization method, are conducted as well. To intuitively illustrate the effectiveness of the proposed method, a 2-DOF spring-mass model is taken as an example in numerical simulations. The updating results show that the proposed method has a good robustness to measurement noises. Finally, to further verify the applicability of the proposed method, a six-storey aluminum alloy frame is designed and fabricated in laboratory. The added mass on each storey is taken as updating parameter. The updating results provide a good agreement with the true values, which indicates that the proposed method can effectively update the model parameters with a high accuracy.

• 한국산학기술학회논문지
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• 제19권4호
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• pp.657-663
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• 2018

본 연구에서는 농업용 트랙터에 조립식으로 결합되는 캐빈에 사용되는 방진고무의 진동절연성능을 향상시키기 위하여 형상최적설계를 수행하였다. 초탄성거동을 보이는 고무의 물성을 평가하기 위하여 일축 및 이축 인장시험을 수행하였고 이를 이용하여 유한요소해석에 입력 가능한 재료 모델을 도출하였다. 실제 트랙터의 운전 상태에서 진동을 측정하여 방진고무로 전달되는 입력 가진 및 이로 인한 캐빈 프레임의 응답을 정량화하였다. 비선형 거동을 보이는 방진고무의 특성을 반영하기 위해 정해석을 이용하여 방진고무의 하중-변위 곡선을 도출하였다. 이로부터 특정 하중 혹은 변위가 가해진 상태에서 방진고무의 강성을 계산할 수 있었으며 이를 캐빈의 조화가진해석에 사용하였다. 해석결과와 시험 결과의 비교를 통하여 해석모델 및 기법의 타당성을 검증하였다. 방진고무의 형상설계를 위하여 다구찌의 인자설계법이 사용되었으며 이를 통하여 강성이 최소화된 방진고무의 형상을 찾을 수 있었다. 방진고무의 최적 형상을 고려하여 조화가진해석을 수행한 결과 초기설계 대비 35 % 이상 개선된 진동저감효과를 확인할 수 있었다.

• 한국군사과학기술학회지
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• 제12권3호
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• pp.272-281
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• 2009

In this paper, three-dimensional optimal evasive maneuver patterns for air-to-surface attack missiles against proportionally navigated anti-air defense missiles were investigated. An interception error of the defense missile is produced by an evasive maneuver of the attack missile. It is assumed that the defense missiles are continuously launched during the flight of attack missile. The performance index to be minimized is then defined as the negative square integral of the interception errors. The direct parameter optimization technique based on SQP and a co-evolution method based on the augmented Lagrangian formulation are adopted to get the attack missile's optimal evasive maneuver patterns. The overall shape of the resultant optimal evasive maneuver is represented as a deformed barrel-roll.

• 한국항공우주학회지
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• 제34권1호
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• pp.74-80
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• 2006

본 논문은 레이더와 같은 지상의 다수위협이 존재하는 상황에서 무인항공기의 비행경로 최적화에 관한 것이다. 레이더에 의한 피탐성, 즉 비행체에 의해 반사되는 레이더 신호강도를 최소화하면서 목적지까지의 비행시간을 최소화하는 관점에서 성능지수를 제안하였다. 1차의 시간지연 시스템으로 가정된 비행체의 경사각을 제어입력으로 고려하였으며, Sequential Quadratic Programming기법에 기반한 입력 파라미터 최적화 기법을 사용하여 궤적최적화를 수행하였다. 제안된 무인 항공기 경로계획 기법은 Voronoi 선도기법과 비교하였을 때, 생존성을 증대시키면서도 항공기의 역학적 특성을 고려한 비행경로를 제공한다.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2003년도 춘계학술대회논문집
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• pp.1032-1037
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• 2003

Although the holes on the shell case are very important fer the acoustic performance, it is difficult to solve the problem because the case includes thin bodies. Hence, in the past, only the method of trial and error, which depends on the engineer's intuition and experience, was available fur the design of holes. Many researchers have tried to solve the thin-body acoustic problems, since the conventional boundary element method (BEM ) using the Helmholtz integral equation fails to yield a reliable solution fer the numerical modelling of radiation anti scattering of sound from thin bodies. In the area of the analysis of thin-body acoustic problem, three approaches are generally used; the multi-domain BEM, the indirect variational BEM, and the normal derivative integral equation And there has been just a f9w study reported on the design optimization for the acoustic radiation problems by using only the conventional BEM. For the thin-body acoustics, however, no further study in the optimization fields has been reported. In this research, the normal derivative integral equation is adopted as an analysis formulation in the thin-body acoustics, and then used fur the optimization. The analytical approaches for the design of holes are proposed by using a topology optimization technique and a genetic algorithm. The proposed approaches are implemented and validated using numerical examples.

• 제어로봇시스템학회논문지
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• 제15권10호
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• pp.982-987
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• 2009

On the controller switching time, even though on-line/off-line controller outputs are the same, a problem which deteriorates the performance of bumpless transfer can happen in case that any discrepancy between the two controller inputs is transferred directly to the controller output. In this paper, we analyze the cause of that phenomenon in existing research results and propose a new method which improves that problem. In order to solve this problem, the off-line controller is augmented to an anti-windup structure and an improved bumpless transfer method is derived by using the changed input of the off-line controller instead of the plant input. We exemplify the performance of the proposed method by comparing with the performance of the existing method via numerical examples.

• 한국정밀공학회지
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• 제23권6호
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• pp.136-142
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• 2006

Optimization of the aircraft panel assembly constructed by skin and stringers is investigated. For the design of panel assembly of the aircraft structure, it is necessary to determine the best shape of the stringer which accomplishes lowest weight under the condition of no instability. A panel assembly can fail in a variety of instability modes under compression. Overall modes of flexure or torsion can occur and these can interact in a combined flexural/torsion mode. Flexure and torsion can occur symmetrically or anti-symmetrically. Local instabilities can also occur. The local instabilities considered in this paper are buckling of the free and attached flanges, the stiffener web and the inter-rivet buckling. A program is developed to find out critical load for each instability mode at the specific stringer shape. Based on the developed program, optimization is performed to find optimum stringer shape. The developed instability analysis program is not adequate for sensitivity analysis, therefore RSM (Response Surface Method) is utilized instead to model weight and instability constraints. Since the problem has many local minimum, Genetic algorithm is utilized to find global optimum.

• Steel and Composite Structures
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• 제29권5호
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• pp.635-645
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• 2018

Beam-column joints play a significant role in static and dynamic performances of reinforced concrete frame structures. This study contributes a numerical approach of topologically optimal design of carbon fiber reinforced plastics (CFRP) to retrofit existing beam-column connections with crack patterns. In recent, CFRP is used commonly in the rehabilitation and strengthening of concrete members due to the remarkable properties, such as lightweight, anti-corrosion and simplicity to execute construction. With the target to provide an optimal CFRP configuration to effectively retrofit the beam-column connection under semi-failure situation such as given cracks, extended finite element method (X-FEM) is used by combining with multi-material topology optimization (MTO) as a mechanical description approach for strong discontinuity state to mechanically model cracked structures. The well founded mathematical formulation of topology optimization problem for cracked structures by using multiple materials is described in detail in this study. In addition, moved and regularized Heaviside functions (MRHF), that have the role of a filter in multiple materials case, is also considered. The numerical example results illustrated in two cases of beam-column joints with stationary cracks verify the validity, benefit and supremacy of the proposed method.