• 지식경영연구
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• 제16권2호
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• pp.249-278
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• 2015

Employees' knowledge integration capabilities and innovative behavior are still of crucial importance in the effective knowledge management. Recently researchers and practitioners are interested in both the potential benefits of unlearning and the negative aspects of learning inertia. The purpose of this study is to examine the relationships among learning inertia, unlearning, knowledge integration capabilities(knowledge exploitation and knowledge exploration) and innovative behavior. The results of analysis show that learning inertia is employees' psychological obstacle factor affecting knowledge integration capabilities and unlearning, that unlearning of employees is a key factor affecting knowledge integration capabilities, and that knowledge integration capabilities are driving forces leading to innovative behaviors of employees. For theoretical and practical implications, the research presents the grounds for arguments that knowledge integration capabilities are employees' dynamic capabilities from the knowledge management perspective, that unlearning is a driving force of employees' positive behaviors, and that organizations trying to perform the dynamic knowledge management need to identify the causes of employees' psychological resistance to learning. Limitations arisen in the course of the research and suggestions for future research directions are also discussed.

• 전력전자학회논문지
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• 제8권3호
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• pp.266-273
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• 2003

풍력 발전 시스템의 제어 알고리즘 개발 및 개발 제품의 성능 시험을 위해 회전자 블레이드를 대신하여 발전기축에 토오크를 입력할 수 있는 풍력 발전기 시뮬레이터를 개발하였다. 제안된 알고리즘은 풍속의 변화에 따른 블레이드의 출력 토오크 변화를 실시간으로 계산하여 직류 전동기 구동을 위한 토오크 지령값으로 사용하며, 특히 회전자 블레이드의 관성이 일반적으로 전동기보다 매우 큰 점에 착안하여 가감속시 회전자 관성에 의한 영향을 고려할 수 있도록 설계되었다. 즉, 바람으로부터 획득하는 운동에너지 중에서 미리 회전자 블레이드 관성 모멘트에 저장/변환되는 에너지를 계산하여 나머지 성분만 발전기 축에 전달하도록 하여 실제로 커다란 관성체를 사용하지 않고도 효과적으로 회전자 블레이드와 발전기부의 동특성을 실제 상황에 가깝게 모의할 수 있다. 직류 전동기를 사용하여 풍속의 변화에 따른 풍력 터빈 시뮬레이터를 설계 제작하고, 시뮬레이션 및 실험을 통해 그 성능을 보였다.

• 천문학회보
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• 제42권2호
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• pp.49.3-50
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• 2017

There have been recent studies which revealed a tendency that thermal inertia decreases with the size of asteroidal bodies, and suggestions that thermal inertias of cometary bodies should be much smaller than those asteroidal counterparts, regardless of comets' nuclear sizes, which hints a way to differentiate cometary candidates from asteroids using thermal inertia information. We thus selected two comet-like objects from AKARI satellite of JAXA, namely, 107P/ (4015) Wilson-Harrington and P/2006 HR30 (Siding Spring), and applied simple thermophysical model to test the idea. Both targets did not show any comet-like activity during the observations. From the model, we found Wilson-Harrington to have size of 3.7-4.4 km, geometric albedo 0.040-0.055 and thermal inertia of 100-250 J m-2 K-1 s-0.5, which coincide with previous works, and HR30 to have size of 24-27 km, geomoetric albedo of 0.035-0.045 with thermal inertia of 250-1000 J m-2 K-1 s-0.5. HR30 is found to have the rotation pole near the ecliptic plane (the latitude between -20 and +60 deg). Based on the results, we conjecture that comet-like objects are not clearly distinguishable from asteroidal counterpart using thermal inertia.

• Structural Engineering and Mechanics
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• 제26권1호
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• pp.1-14
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• 2007

Because of complexity, the literature regarding the free vibration analysis of a Timoshenko beam carrying "multiple" spring-mass systems is rare, particular that regarding the "exact" solutions. As to the "exact" solutions by further considering the joint terms of shear deformation and rotary inertia in the differential equation of motion of a Timoshenko beam carrying multiple concentrated attachments, the information concerned is not found yet. This is the reason why this paper aims at studying the natural frequencies and mode shapes of a uniform Timoshenko beam carrying multiple intermediate spring-mass systems using an exact as well as a numerical assembly method. Since the shear deformation and rotary inertia terms are dependent on the slenderness ratio of the beam, the shear coefficient of the cross-section, the total number of attachments and the support conditions of the beam, the individual and/or combined effects of these factors on the result are investigated in details. Numerical results reveal that the effect of the shear deformation and rotary inertia joint terms on the lowest five natural frequencies of the combined vibrating system is somehow complicated.

• International Journal of Aeronautical and Space Sciences
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• 제16권3호
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• pp.394-406
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• 2015

In this work, an efficient aircraft landing simulation strategy is proposed to develop an efficient and reliable hard-landing monitoring procedure. Landing stage is the most dangerous moment during operation cycle of aircraft and it may cause structural damage when hard-landing occurs. Therefore, the occurrence of hard-landing should be reported accurately to guarantee the structural integrity of aircraft. In order to accurately determine whether hard-landing occurs or not from given landing conditions, full nonlinear structural dynamic simulation can be performed, but this approach is highly time-consuming. Thus, a more efficient approach for aircraft landing simulation which uses a hierarchical aircraft landing model and an extended inertia relief technique is proposed. The proposed aircraft landing model is composed of a multi-body dynamics model equipped with landing gear and tire models to extract the impact force and inertia force at touch-down and a linear dynamic structural model with an extended inertia relief method to analyze the structural response subject to the prescribed rigid body motion and the forces extracted from the multi-body dynamics model. The numerical examples show the efficiency and practical advantages of the proposed landing model as an essential component of aircraft hard-landing monitoring procedure.

• 한국수학교육학회지시리즈E:수학교육논문집
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• 제22권1호
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• pp.53-63
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• 2008

수학 영재교육에서 여러 학문영역의 지식을 종합하며, 이를 바탕으로 창의적으로 문제를 해결하는 능력과 경험을 가지는 것은 매우 중요하다. 본 연구에서는 물리학의 역학분야에서 연구되는 관성능률 개념을 수학적 문제해결의 도구로 활용하여 몇몇 등식들, 부등식들에 대한 새로운 증명방법을 제시하며, 관성능률을 이용한 문제해결 방법의 특징들을 고찰하였다.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2001년도 춘계학술대회 논문집 전기기기 및 에너지변환시스템부문
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• pp.332-334
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• 2001

This paper presents the simulator system of high-speed elevator system, which can be implemented as 3-mass system as well as equivalent 1-mass system. In order to implement the equivalent inertia of total elevator system, conventional simulator has generally utilized mechanical inertia (flywheel) with large radius, which makes the size and weight of total simulator system large. In addition, the mechanical inertia should be replaced each time in order to test the another elevator system. In this paper, the simulation method using electrical inertia is presented so that the volume and weight of simulator system are greatly reduced and the adjustment of value of the inertia can be achieved easily by software. Experimental results show the feasibility of this simulator system.

• 드라이브 ㆍ 컨트롤
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• 제15권3호
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• pp.8-13
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• 2018

This paper presents a phase portrait analysis-based safety control algorithm for excavators, using adaptive sliding mode control. Since working postures and material types cause the excavator's rotational inertia to vary, the rotational inertia was estimated, and this estimation was used to design an adaptive sliding mode controller for collision avoidance of the excavator. In order to estimate the rotational inertia, the recursive least-squares estimation with multiple forgetting was applied with the information of the swing velocity of the excavator. For realistic evaluation, an actual working scenario-based performance evaluation was conducted. Based on the estimated rotational inertia and an analysis of estimation errors, sliding mode control inputs were computed. The actual working scenario-based performance evaluation of the designed safety algorithm was conducted, and the results showed that the developed safety control algorithm can efficiently avoid a collision with an object in consideration of rotational inertia variations.

• 전자공학회논문지SC
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• 제40권5호
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• pp.317-325
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• 2003

2관성 시스템을 제어할 때 자주 발생하는 진동은 빠른 속도 응답을 얻거나 외란 제거를 어렵게 한다. 본 논문은 2관성 모터시스템에 대해서 유전자 알고리즘을 사용하여 세 가지 속도 제어기(I-P, I-PD, 상태 피드백)의 자동 극배치 제어기를 설계하는 방법을 제시한다. 오버슈트와 세틀링 시간을 줄이는 관점에서 유전자 알고리즘을 사용하여 최적의 파라미터를 선정한 다음 이들을 각 제어기의 이득을 계산 할 때 사용한다. 몇 가지의 시뮬레이션을 통해서 제안한 제어기의 성능을 보인다. 제안한 제어기는 유연한 샤프트를 갖는 2관성 모터 시스템의 제어기의 자동 설계법이 될 수 있다.

• 항공우주기술
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• 제10권2호
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• pp.121-127
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• 2011

추력기 기반 자세제어계 제어기 설계에서 인공위성의 관성모멘트는 중요한 설계 요소이다. 설계 과정에서 불확실성을 고려하기는 하지만 큰 규모의 태양전지판과 같은 유연 구조물을 가지는 정지궤도 위성의 경우 추력기의 작동 제어주기와 유연모드의 간섭을 피하기 위해 정확한 관성모멘트의 측정이 요구된다. 천리안 위성의 경우 전이궤도에서 임무궤도로 전환하기 전에 관성모멘트의 측정이 수행되었는데, 본 논문에서는 천리안위성의 관성모멘트 측정 방법을 유추해서 기술하고, 실제 궤도상 시험에서 측정된 관성모멘트 값과 비교하였다. 이를 통해, 자세제어계 상세 설계 단계에서 고려된 불확실성 범위 내에 관성모멘트 값이 유지되었음을 확인하여 설계의 적합성을 검증하였다.