• Korean Journal of Agricultural Science
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• v.30 no.2
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• pp.164-174
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• 2003

This study was performed to suggest a rational method for the stability evaluation of agricultural reservoir in the very soft ground. The stability methods for agricultural reservoir was used to compare and analyze with various condition by limit equilibrium method. The behavior of settlement-displacement obtained by field monitoring system was used to compare and analyze with various stability methods, and to investigate the applicability of the methods for stability evaluation of agricultural reservoir. The horizontal displacement was abruptly increased when physical properties of soft clay reached its maximum values and therefore, the values of these properties could be used to the fundamental data for stability evaluation. The evaluation of the stability of agricultural reservoir was suggested to use the inclination of curve rather than critical line.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.41 no.4
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• pp.365-376
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• 2021

In general, domestic streams and rivers are composed of alluvial rivers consisting of sand and gravel beds. These rivers can cause erosion and riverbed changes due to sudden changes in flow rates, such as floods, torrential rains, and heavy rains. In particular, there are various types of erosion, such as contraction erosion caused by changes in river shape, or local erosion occurring around obstacles such as piers, abutments or embankments. In addition, river changes can occur in various forms, such as static or dynamic periods, due to limitations such as flow rate, velocity, and shear stress. This study focused on the erosions of embankments directly related to human casualties among various river structures, and evaluated limit velocities and critical shear stress in order to identify changes in strength of natural materials by identifying the characteristics of natural hoan materials and resistance to erosions. In particular, the limitations of materials according to the type of materials in the river, characteristics of particles, and size of particles were studied using Soil loss, which is a change in the volume of the revetment material, and it is intended to be used as basic data for river design and restoration.

• KSCE Journal of Civil and Environmental Engineering Research
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• v.4 no.3
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• pp.11-18
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• 1984

There are two different methods in the stability analysis of slopes depending upon the 1ocations and the types of assumed failure planes, which are the infinite slope analysis and the finite slope analysis. The infinite slope analysis is simple and easier in its application. However, since the method neglects the end effects and assumes the failure plane to be located at the shallow depth and parallel to the slope, the slopes to be analyzed by the method should be limited to a certain range. Thus, it is intended in this paper to define the infinite slopes whose stability may be analyzed by the infinite slope analysis. As a result, it is obtained that the method of infinite slope analysis may be applied to the slopes which have the ratio of the slope height to the depth of the failure plane of 9 or bigger.

• Journal of the Korean Geotechnical Society
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• v.24 no.3
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• pp.5-11
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• 2008

This paper pertains to the incorporation of a genetic algorithm methodology for determining the critical slip surface and the corresponding factor of safety of soil slopes using inclined slice method. The analysis is formulated as a constrained optimization problem to solve the nonlinear equilibrium equations and finding the factor of safety and the critical slip surface. The sensitivity of GA optimization method is presented in terms of development of failure surface. Example problem is presented to demonstrate the efficiencies of the genetic algorithm approach. The results obtained by this method are compared with other traditional optimization technique.

• Proceedings of the KSEEG Conference
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• 2001.04a
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• pp.203-205
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• 2001

• Journal of Advanced Navigation Technology
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• v.20 no.5
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• pp.475-481
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• 2016

In this paper, the new stability condition of linear discrete interval time-varying systems with time-varying delay time is proposed. The considered system has interval time-varying system matrices for both non-delayed and delayed states with time-varying delay time within given interval values. The proposed condition is derived by using Lyapunov stability theory and expressed by very simple inequality. The restricted stability issue on the interval time-invariant system is expanded to interval time-varying system and a powerful stability condition which is more comprehensive than the previous is proposed. As a results, it is possible to avoid the introduction of complex linear matrix inequality (LMI) or upper solution bound of Lyapunov equation in the derivation of sufficient condition. Also, it is shown that the proposed result can include the many existing stability conditions in the previous literatures. A numerical example in the pe revious works is modified to more general interval system and shows the expandability and effectiveness of the new stability condition.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.3
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• pp.217-224
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• 2020

The use of a high gain flight control system to achieve high bandwidth performance increase the instability of a helicopter. To investigate these phenomena numerically, high fidelity EC155B1 helicopter model and simplified flight control system that include actuator, digital processor and noise rejection filter was developed. A study conducts an analytical investigation of roll axis stability of the helicopter model as feedback gain increases. And this study analyzes roll-rate and roll-attitude feedback gains limited by rotor flap mode. The results indicate that the phase delays caused by the filter can severely limit the usable values of the roll-rate and roll-attitude feedback gains.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.33 no.7
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• pp.85-91
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• 2005

Supersonic jet fighter aircraft must have been guaranteed appropriate for controllability and stability in HAoA(High Angle of Attack) region. Limit value of aircraft enter the deep stall at HAoA is related to problem of aircraft configuration design. But, In order to guarantee the aircraft safety in HAoA, control law is designed using digital Fly-By-Wire flight control system in modern versions of supersonic jet fighter aircraft. Also, In order to recovery if aircraft enter the deep stall or spin, anti-spin control law and MPO(Manual Pitch Override) mode is designed. AoA limiter and MPO is designed in longitudinal axis and HAoA departure prevention logic, roll command limiter, rudder fader and anti-spin logic is designed in lateral-directional axis. In this paper, we introduce the T-50 HAoA flight control law and propose that aircraft stability and adequate of these control law from HAoA flight test.

• Proceedings of the Korea Water Resources Association Conference
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• 2019.05a
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• pp.85-85
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• 2019

하천시설물 설계, 시공 및 관리에 있어서 구성재료의 보호능력에 따라 예상하지 못한 조건에서 쉽게 파손될 수 있다. 이러한 영향은 하천환경의 변화를 야기시킬 수 있다. 제방 표면 재료는 제외 비탈면의 침식 방지를 목적으로 사용되는 재료로 주로 호안블록. 식생 매트, 사석, 돌망태, 식생등이 주로 사용되고 있다. 국내에서는 2000년대 이전에는 자연 흙사면의 식생, 돌망태, 단순 돌기형 콘크리트 블록 등이 주로 사용되었으며 2000년대 이후에는 하천환경을 고려하여 식생의 생장이 가능한 친환경 호안 블록 및 식생 매트의 적용이 일반적으로 시공되고 있다. 제방의 수리적 설계를 위해서는 재료 표면의 수리 특성, 즉, 조도계수 및 한계 유속, 한계 소류력이 제시되어야 하는데 이는 실험을 통해서 결정되어야 한다. 때문에 본 연구에서는 자연형 하상재료를 이용하여 바이오 폴리머 첨가시 증가하는 방어능력에 대한 향상도를 평가하는 실험적 평가 방법을 제안하기위해 홍수시 수리조건을 반영하여 상류에서부터 사류까지 다양한 유속범위에 따른 세굴 및 침식에 대한 실험을 진행하였다. 본 연구에서는 자연하천과 유사한 조건의 경사를 가지는 경사수로에서 실험연구를 통해 제방재료의 안정성 평가방법을 개발하였고, 안정성 평가를 위한 실험진행은 기 개발된 바닥응력을 직접측정하는 장치와 PIV시스템을 이용하여 수리특성을 측정하였다.(Park J.H. et al. 2016, Flow Measurment and instrumentation.) 기존 문헌에서 제시되었던 측정 장치를 이용하여 바이오폴리머의 첨가에 유무에 따라 세굴에 대한 방어능력의 향상정도를 측정하고자 세굴 및 침식에 대한 평가 방법을 제시하고 있다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.11
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• pp.998-1007
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• 2015

The $H_{\infty}$ control theory using LMI method is applied to design an attitude controller of radial type satellite that has strongly coupled channels due to the large product of inertia. It is observed that the cross-over frequency of open-loop with $H_{\infty}$ controller is lower than that of open-loop without controller, which is not typical phenomenon in an optimal control design result: it is interpreted that due to a large product of inertia, there is certain limit in increasing agility of satellite by just tuning weighting function. ${\mu}$-analysis is performed to verify the stability and performance robustness with the assumption of +/-5% MOI variation. ${\mu}$-analysis result shows that the variation of principal MOI degrades the stability and performance robustness more than the variation of POI does.