• Journal of Mechanical Science and Technology
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• 제19권4호
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• pp.985-992
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• 2005

Vehicle Stability Control (VSC) system prevents vehicle from spinning or drifting out mainly by braking intervention. Although a control threshold of conventional VSC is designed by vehicle characteristics and centered on average drivers, it can be a redundancy to expert drivers in critical driving conditions. In this study, a manual adaptation of VSC is investigated by changing the control threshold. A control threshold can be determined by phase plane analysis of side slip angle and angular velocity which is established with various vehicle speeds and steering angles. Since vehicle side slip angle is impossible to be obtained by commercially available sensors, a side slip angle is designed and evaluated with test results. By using the estimated value, phase plane analysis is applied to determine control threshold. To evaluate an effect of control threshold, we applied a 23-DOF vehicle nonlinear model with a vehicle planar motion model based sliding controller. Controller gains are tuned as the control threshold changed. A VSC with various control thresholds makes VSC more flexible with respect to individual driver characteristics.

• 한국가시화정보학회지
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• 제22권1호
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• pp.28-33
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• 2024

We visualized the rupturing of liquid films flowing over a disk rotating with large angular velocity. A setup of high speed imaging for liquid flows on dark and reflective surfaces are suggested. From the result, rivulet structures are revealed to be strongly governed by three-dimensional surface structures developed in the film flow. Additionally, unique flow structures including the rivulet sliding and internal meandering are investigated. Generation mechanism of such structures are discussed in terms of the dynamic contact angle theory.

• 한국군사과학기술학회지
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• 제20권1호
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• pp.108-118
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• 2017

In this paper, the path tracking controller for a surface vessel based on the sliding mode control (SMC) with the switching law is proposed. In order to have no restriction on movement and improved tracking performance, the proposed control system is developed as follows: First, the kinematic and dynamic models in Cartesian coordinates are considered to solve the singularity problem at the origin. Second, the new multiple sliding surfaces are designed with the SMC and approach angle concept to solve the under-actuated property. Third, the switching control system is designed to improve tracking performance. To prove the stability of the proposed switching system under the arbitrary switching, the Lyapunov stability analysis method with the common Lyapunov function is used. Finally, the computer simulations are performed to demonstrate the performance, effectiveness and stability of the proposed tracking controller of a surface vessel.

• 소성∙가공
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• 제14권1호
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• pp.71-77
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• 2005

Thermal stability and dry sliding wear behavior of ultra-fine grained 6061 Al alloy fabricated by an accumulative roll-bonding (ARB) process have been investigated. After 4 ARB cycles, an ultra-fine grained microstructure of the 6061 Al alloy composed of grains with average size of 500nm, and separated mostly by high-angle boundaries was obtained. Though hardness and tensile strength of the ARB processed Al alloy increased with ARB cycles up to 4 cycles, the processed alloy exhibited decreased ductility and little strain hardening. Thermal stability of the ARB-processed microstructure was studied by annealing of the severely deformed alloy at $423K{\sim}573K$. The refined microstructure of the alloy remained stable up to 473K, and the peak aging treatment of the alloy at 450K for 8 hrs increased the thermal stability of the alloy. Sliding-wear rates of the alloy increased with the number of ARB cycles in spite of the increased hardness with the cycles. Wear mechanisms of the ultra-fine grained alloy were investigated by examining worn surfaces, wear debris, and cross-sections by a scanning electron microscopy (SEM).

• International Journal of Aeronautical and Space Sciences
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• 제15권2호
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• pp.163-172
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• 2014

This paper proposes a novel guidance law based on the block backstepping sliding mode control and extended state observer (ESO), which also takes into account the autopilot dynamic characteristics of the near space interceptor (NSI), and the impact angle constraint of attacking the maneuvering target. Based on the backstepping control approach, the target maneuvers and the parameter uncertainties of the autopilot are regarded as disturbances of the outer loop and inner loop, respectively. Then, the ESO is constructed to estimate the target acceleration and the inner loop disturbance, and the block backstepping sliding model guidance law is employed, based on the estimated disturbance value. Furthermore, in order to avoid the "explosion of complexity" problem, first-order low-pass filters are also introduced, to obtain differentiations of the virtual control variables. The stability of the closed-loop guidance system is also proven, based on the Lyapunov theory. Finally, simulation results demonstrate that the proposed guidance law can not only overcome the influence of the autopilot dynamic delay and target maneuvers, but also obtain a small miss distance.

• 한국정밀공학회지
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• 제18권5호
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• pp.137-146
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• 2001

A robust controller with the sliding mode is proposed for stable dynamic walking of the biped robot in this paper. For the robot system to be controlled, which is modeled as 14 DOF rigid bodies by the method of multi-body dynamics, the joint angle trajectories are determined by the velocity transformation matrix. Also Hertz force model and Hysteresis damping element are utilized for the ground reaction and impact forces during the contact with the ground. The biped robot system becomes unstable since those forces contain highly confused noise components and some discontinuity, and modeling uncertainties such as parameter inaccuracies. The sliding mode control is applied to solve above problems. Under the assumption of the bounded estimation errors on the unknown parameters, the proposed controller provides a successful way to achieve the stability and good performance in spite of the presence of modeling imprecisions of uncertainties.

• 한국산학기술학회논문지
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• 제18권6호
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• pp.21-28
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• 2017

농기계 상하차를 위한 전동 유압 슬라이딩 데크 시스템을 개발하는데 있어 경량화가 필수적이며, 이를 해결하기 위해 덤프 각도에 따른 슬라이딩 데크의 진출길이를 계산하고, 허용가능 각도 중 가강 큰 하중 받는 각도에서 재질과 두께를 변경하며 구조해석을 진행, 최적 두께와 재질을 선정하였다. 먼저 슬라이딩 데크 진출길이 계산식을 도출하기 위해 전체 시스템의 구성을 파악하고, 시스템을 단순화 하는 작업을 시행하였다. 또한 시스템의 입 출력 관계를 파악하기 위해 자유도 계산을 수행 하였고, 단순화한 모델을 이용하여 덤프각도에 따른 슬라이딩 데크의 진출길이 계산식을 도출하였다. 도출한 계산식을 수치해석 프로그램을 이용하여 덤프각도에 따른 슬라이딩 데크 진출길이 계산을 수행하였고, 시스템의 최대 최소 각도에서의 진출길이를 파악 하였다. 신뢰성 확보를 위해 시스템의 축소모형을 제작하여 실험을 통해 계산식을 검증하였다. 슬라이딩 데크 재질과 두께를 결정하기 위해 데크를 단순화 하였고, 데크 제작에 쓰이는 대표적인 재질 두 가지를 선정하였다. 단순화한 모델을 해석 프로그램을 사용하여 최대 하중을 받는 조건에서 두께와 재질에 따른 변형량과 응력을 비교하였다. 해석결과 ATOS80을 이용할 경우 두께를 줄이면서 더 적은 변형량을 가지게 되어 경량화를 이룰 수 있다.

• 한국지반공학회논문집
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• 제34권12호
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• pp.19-27
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• 2018

테르쟈기는 트랩도어 처짐에 기반한 상부지반의 수직활동면을 가정한 2차원 아칭식을 제안하였다. 이후 관련 식은 3차원 터널굴착조건과 경사활동면을 고려할 수 있도록 확장되었다. 본 연구에서는 3차원 터널굴착조건에서 비등방지반조건을 반영하여 터널 횡방향 및 종방향에서의 지반물성치 및 활동면의 경사각을 달리하여 고려할 수 있도록 더욱 확장된 아칭식을 유도하고 제시하였다. 제시된 식을 이용하여 다양한 조건(지반물성치, 경사활동면, 굴착조건, 상재하중, 토압계수)에서 발생되는 수직응력에 대해 조사하였고 테르쟈기의 2차원 아칭식과도 비교하였다. 조사결과, 발생 수직응력은 굴착폭 및 굴착길이, 경사각, 상재하중이 증가할수록 증가했고 점착력과 마찰각, 토압계수가 감소할수록 증가하였으며, 굴착길이가 작을 때와 횡방향 지반물성치에 의해서 더 큰 영향을 받는 것으로 나타났다. 또한 테르쟈기 2차원 아칭식과 비교하여 발생 수직응력은 더 작은 것으로 나타났고 그 차이정도는 지반물성치, 경사활동면, 3차원 터널굴착 조건에 따라 매우 큰 영향을 받는 것으로 나타났다. 제시된 3차원 아칭식은 터널굴착으로 인한 복잡한 아칭현상을 보다 잘 이해하는데 도움을 줄 수 있을 것으로 판단된다.

• Journal of Biosystems Engineering
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• 제3권1호
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• pp.1-19
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• 1978

Power tiller is a major unit of agricultural machinery being used on farms in Korea. About 180.000 units are introduced by 1977 and the demand for power tiller is continuously increasing as the farm mechanization progress. Major farming operations done by power tiller are the tillage, pumping, spraying, threshing, and hauling by exchanging the corresponding implements. In addition to their use on a relatively mild slope ground at present, it is also expected that many of power tillers could be operated on much inclined land to be developed by upland enlargement programmed. Therefore, research should be undertaken to solve many problems related to an effective untilization of power tillers on slope ground. The major objective of this study was to find out the travelling and tractive characteristics of power tillers being operated on general slope ground.In order to find out the critical travelling velocity and stability limit of slope ground for the side sliding and the dynamic side overturn of the tiller and tiller-trailer system, the mathematical model was developed based on a simplified physical model. The results analyzed through the model may be summarized as follows; (1) In case of no collision with an obstacle on ground, the equation of the dynamic side overturn developed was: $$\sum_n^{i=1}W_ia_s(cos\alpha cos\phi-{\frac {C_1V^2sin\phi}{gRcos\beta})-I_{AB}\frac {v^2}{Rr}}=0$$ In case of collision with an obstacle on ground, the equation was: $$\sum_n^{i=1}W_ia_s\{cos\alpha(1-sin\phi_1)-{\frac {C_1V^2sin\phi}{gRcos\beta}\}-\frac {1}{2}I_{TP} \( {\frac {2kV_2} {d_1+d_2}\)-I_{AB}{\frac{V^2}{Rr}} \( \frac {\pi}{2}-\frac {\pi}{180}\phi_2 \} = 0 $$ (2) As the angle of steering direction was increased, the critical travelling veloc\ulcornerities of side sliding and dynamic side overturn were decreased. (3) The critical travelling velocity was influenced by both the side slope angle .and the direct angle. In case of no collision with an obstacle, the critical velocity $V_c$ was 2.76-4.83m/sec at $\alpha=0^\circ$, $\beta=20^\circ$ ; and in case of collision with an obstacle, the critical velocity $V_{cc}$ was 1.39-1.5m/sec at $\alpha=0^\circ$, $\beta=20^\circ$ (4) In case of no collision with an obstacle, the dynamic side overturn was stimu\ulcornerlated by the carrying load but in case of collision with an obstacle, the danger of the dynamic side overturn was decreased by the carrying load. (5) When the system travels downward with the first set of high speed the limit {)f slope angle of side sliding was $\beta=5^\circ-10^\circ$ and when travels upward with the first set of high speed, the limit of angle of side sliding was $\beta=10^\circ-17.4^\circ$ (6) In case of running downward with the first set of high speed and collision with an obstacle, the limit of slope angle of the dynamic side overturn was = $12^\circ-17^\circ$ and in case of running upward with the first set of high speed and collision <>f upper wheels with an obstacle, the limit of slope angle of dynamic side overturn collision of upper wheels against an obstacle was $\beta=22^\circ-33^\circ$ at $\alpha=0^\circ -17.4^\circ$, respectively. (7) In case of running up and downward with the first set of high speed and no collision with an obstacle, the limit of slope angle of dynamic side overturn was $\beta=30^\circ-35^\circ$ (8) When the power tiller without implement attached travels up and down on the general slope ground with first set of high speed, the limit of slope angle of dynamic side overturn was $\beta=32^\circ-39^\circ$ in case of no collision with an obstacle, and $\beta=11^\circ-22^\circ$ in case of collision with an obstacle, respectively.

• 한국항공우주학회지
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• 제31권2호
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• pp.63-71
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• 2003

본 논문에서는 유연우주비행체의 강인 선회기동을 위한 슬라이딩 모드 제어기법에 대해 연구하였다. 본 연구에서는 유연우주비행체의 1축 선회기동을 위한 선회목표각, 목표각속도 및 중앙동체와 유연부착물 사이에 작용하는 내부 반력 모멘트를 포함하는 슬라이딩 평면을 설계하였다. Lyapunov 제어기법과 비교한 결과 두 제어기법 모두 공칭 시스템에 대한 명령 추종성을 확인하였으며, 특히 슬라이딩 모드 제어기법의 적용결과 시스템 파라메터의 변동 및 외란의 영향에도 좋은 제어결과를 얻을 수 있음을 확인하였다. 1축 선회제어 결과를 확장하여 임의의 3축 선회기동을 수행할 수 있는 슬라이딩 모드 제어기를 설계하였다. 3축 선회기동 제어를 위해 쿼터니언을 이용하여 비행체의 자세를 결정하였고, 3개의 축 각각에 대해 설계된 슬라이딩 평면으로부터 선회기동시 발생하는 각 축간의 커플링 효과를 고려하여 제어기를 설계하였다. 설계된 제어기는 효과적인 3축 선회기동을 수행할 수 있음을 수치 시뮬레이션을 통해 보여주고 있다.