• 한국지반공학회논문집
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• 제37권8호
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• pp.37-49
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• 2021

옹벽은 절, 성토부가 포함된 토지의 효율적 이용을 위하여 설치하는 대표적인 옹벽 구조물이다. 과거 국토개발 시기에는 시공성, 구조적 안정성 및 경제성에 치중하였다면, 최근에는 친환경적이고 내진 안정성을 갖춘 옹벽기술개발의 필요성이 증대되고 있는 실정이다. 본 연구에서는 자연석을 활용한 친환경적 옹벽 구조물(Eco-BELT)을 제시하고 지진 시 동적 거동특성을 2, 3차원 수치해석을 이용하여 분석하였다. 자연석과 배면 뒤채움 흙 사이에 형성되는 접촉면을 고려하여 수치해석에 적용하였으며 동적거동에 영향을 미치는 주요 변수로서 뒤채움재의 다짐도를 기준으로 다짐도 증가에 따른 동적거동을 분석하고 T형 후방지지물의 유무에 따른 내진성능 향상을 수치해석적으로 검토하였다. 그 결과 다짐도 증가 시 옹벽 수평변위가 최대 29.5% 감소하여 다짐도 증가에 따른 내진안정성 증대효과를 확인하고 T형 후방지지물 설치 시 최대 수평변위는 약 21.2~21.9%가 감소하는 것으로 산출되어 지진하중 재하 시 T형 후방지지물의 보강효과를 확인하였다.

• International Journal of Aeronautical and Space Sciences
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• 제17권3호
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• pp.366-377
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• 2016

This paper presents a vision-based guidance method that allows a fixed-wing aircraft to orbit around a target at a given radius. The guidance method uses a simple formula that regulates a relative side-bearing angle estimated by a vision system. The global asymptotic stability of the associated guidance law is demonstrated, and a linear analysis is performed to facilitate the proper selection of the relevant control parameters. A flight experiment is presented to demonstrate the feasibility and performance of the proposed guidance method.

• 박물관보존과학
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• 제2권
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• pp.19-25
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• 2000

광주 신창동 저습지 유적에서 출토된 수침목재유물에 적합한 보존처리 방법을 설정하고자 동일유적에서 출토된 2종의 자연목재를 PEG(Poly-Ethylene Glycol), Sucrose, Lactitol로 처리하고 약제별 치수안정성 및 처리목재의 습윤↔건조 특성을 상호 비교하였다. 그 결과 상수리나무류는 저분자의 PEG#200(MW:200)과 고분자량의 PEG#4000(MW:3,350)을 이용한 2단계 PEG처리(PEG-2Step)에서, 단풍나무류는 PEG#4000만을 단독으로 적용한 처리에서 가장 높은 치수안정성을 나타내었다. 또한 처리 후 습윤↔건조 실험에서는 2단계 PEG처리한 시험재의 치수변화가 가장 작게 나타났다. 반면 Sucrose와 Lactitol의 경우 약제 확산속도가 빠르지만 Sucrose처리재는 84%의 높은 습도조건에서 흡습량이 급격히 증가하면서 약제가 다량 용출되었고, Lactitol은 습윤↔건조 후 미세한 할렬과 함께 처리재가 팽창되는 현상이 발생되었다. 또한 습윤↔건조 실험에서 2단계 PEG처리를 제외한 모든 시험재에서 갈라짐이 발생하였다. 이번 실험결과 신창동 저습지 출토수침목재는 2단계 PEG처리법을 적용한 경우에 치수안정성이 가장 높고 습도변화에 대한 적응성도 양호한 것으로 나타났다.

• 제어로봇시스템학회논문지
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• 제10권11호
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• pp.1065-1070
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• 2004

Optimal collision avoidance algorithm for unmanned aerial vehicles based on proportional navigation guidance law is investigated this paper. Although proportional navigation guidance law is widely used in missile guidance problems, it can be used in collision avoidance problem by guiding the relative velocity vector to collision avoidance vector. The optimal navigation coefficient can be obtained if an obstacle if an obstacle moves at constant velocity vector. The stability of the proposed algorithm is also investigated. The stability can be obtained by choosing a proper navigation coefficient.

• Earthquakes and Structures
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• 제21권6호
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• pp.601-612
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• 2021

The paper concerns the selection of a design accelerograms used for the slope stability assessment under earthquake excitation. The aim is to experimentally verify the Arias Intensity as an indicator of the excitation threat to the slope stability. A simple dynamic system consisting of a rigid block on a rigid inclined plane subjected to horizontal excitation is adopted as a slope model. Strong ground motions recorded during earthquakes are reproduced on a shaking table. The permanent displacement of the block serves as a slope stability indicator. Original research stand allows us to analyse not only the relative displacement but also the acceleration time history of the block. The experiments demonstrate that the Arias Intensity of the accelerogram is a good indicator of excitation threat to the stability of the slope. The numerical analyses conducted using the experimentally verified extended Newmark's method indicate that both the Arias Intensity and the peak velocity of the excitation are good indicators of the impact of dynamic excitation on the dam's stability. The selection can be refined using complementary information, which is the dominant frequency and duration of the strong motion phase of the excitation, respectively.

• 한국초전도ㆍ저온공학회논문지
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• 제3권1호
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• pp.56-63
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• 2001

The thermal stability conditions are investigated for superconducting magnet systems cooled conductively by cryocooler without liquid cryogens. The worst scenario in the systems is that the heat generation in the resistive state exceeds the refrigeration. causing a rise in the temperature of the magnet winding and leading to the burnout. It is shown by an analytical solution that in the continuous resistive state, the temperature may increase indefinitely or a stable steady-state may be reached, depending upon the relative size of the magnet with respect to the refrigeration capacity of the cryocooler. The stability criteria include the temperature-dependent Properties of the magnet materials and the refrigeration characteristics of the cryocooler. A useful graphical scheme is Presented and discussed to demonstrate the physical importance of the results.

• 제어로봇시스템학회논문지
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• 제20권12호
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• pp.1246-1251
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• 2014

This article presents an optimum yaw moment distribution scheme for a vehicle with electronic stability control (ESC) and active rear steering (ARS). After computing the control yaw moment in the yaw moment controller, it should be distributed into tire forces, generated by ESC and ARS. In this paper, yaw moment distribution is formulated as an optimization problem. New objective function is proposed to tune the relative magnitudes of the tire forces. Weighed pseudo-inverse control allocation (WPCA) is adopted to solve the problem. To check the effectiveness of the proposed scheme, simulation is performed on a vehicle simulation package, CarSim. From the simulation, the proposed optimum yaw moment distribution scheme is shown to effective for vehicle stability control.

• 한국지반공학회:학술대회논문집
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• 한국지반공학회 2006년도 춘계 학술발표회 논문집
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• pp.720-723
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• 2006

This study performed slope stability analysis by changing analysis methods and shear strength with the slope stability analysis program. The conclusions of the study are as follows. 1) The safe factor of clayey soil applied with Bishop's simple method turned out to be similar to or slightly higher than those of other methods, for both dry and saturated conditions. 2) The safe factor of sandy soil applied with GLE method turned out to be slightly higher than those of other methods. But when applied with Bishop's simple method, it appeared to be slightly higher than those of other methods. 3) The safe factor of ordinary soil applied with GLE method showed the highest result. 4) Janbu method showed the lowest safe factor among all the methods for the above three types of soils.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 추계 학술대회논문집
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• pp.134-140
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• 2007

Nonlinear parabolized stability equations for compressible flow in general curvilinear coordinate system are derived to deal with a broad range of transition prediction problems on complex geometry. A highly accurate finite difference PSE code has been developed using an implicit marching procedure. Blasius flow is tested. The results of the present computation show good agreement with DNS data. Nonlinear interaction can make the T-S fundamental wave more unstable and the onset of its amplitude decay is shifted downstream relative to linear case. For nonlinear calculations, rather small difference in initial amplitude can produce large change during nonlinear region. Compressible secondary instability at Mach number 1.6 is also simulated and showed that 1.1% initial amplitude for primary mode is enough to trigger the secondary growth.

• International Journal of Aeronautical and Space Sciences
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• 제9권2호
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• pp.71-78
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• 2008

New formation flight controller for unmanned aerial vehicles is proposed. A behavioral decentralized control approach called formation geometry center control is adopted. Trajectory tracking as well as formation geometry keeping are the purpose of the formation flight, and therefore two controllers are designed: a trajectory tracking controller for reference trajectory tracking, and a position controller for formation geometry keeping. Each controller is designed using Lyapunov stability theorem to guarantee the asymptotic stability. Formation flight controller is finally obtained by combining the trajectory tracking controller and the formation geometry keeping controller using a weighting parameter that depends on the relative distance error between unmanned aerial vehicles. Numerical simulations are performed to validate the performance of the proposed controller.