• 한국건설관리학회:학술대회논문집
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• 한국건설관리학회 2007년도 정기학술발표대회 논문집
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• pp.347-352
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• 2007

건설 산업의 숙련공 부족현상, 고령화 문제, 임금 상승으로 인한 채산성 악화, 품질의 균일성 및 안전성 확보 등은 향후 국내 건설 산업이 해결해야 할 당면 과제이다. 이러한 문제를 해결하기 위한 하나의 기술적인 접근방법으로써 국${\cdot}$내외에서는 건설 자동화에 대한 연구가 활발히 진행 중에 있으며, 최근 국내에서는 토공사 작업의 안전성을 확보하기 위해 백호(backhoe)를 대상으로 지능형 굴삭로봇을 개발하기 위한 연구가 진행 중에 있다. 본 연구에서는 지능형 굴삭 로봇을 개발하기 위해 필수적으로 요구되는 기반기술 중 실시간 지반형상 인식 및 토공량 자동산출을 위한 최신 요소기술을 분석하고 최적 대안을 제시하였으며, 이를 위해 국내외 문헌고찰 및 다양한 최신요소 기술의 분석을 통해 지반형상을 실시간으로 인식할 수 있는 5가지 요소기술들에 대한 분석을 선행하였다. 또한 로컬영역의 실시간 지반형상 인식 및 토공량 자동 산출을 위해 3차원 모델링 장비가 갖추어야할 주요 고려요소를 분석하고, AHP 기법을 이용하여 주요 고려요소별 가중치를 산정하고 각 요소기술별 선호지수를 도출하였다. 도출된 선호지수를 바탕으로 최신 요소기술 간의 우선순위를 선정함으로써 3차원 모델링 장비에 적용 가능한 최적 대안을 선정하였다.

• 한국소음진동공학회논문집
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• 제21권9호
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• pp.858-867
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• 2011

As applying an active control technique to a pneumatic vibration isolation system, the settling time for the payload excitation could be remarkably reduced as well as the improvement of isolation performance for the ground vibration. Some previous researches were dealt with the settling time through the simulation or experiment but, the discussion on the simulation or experimental results including moving parts, such as a XY-stage, on the isolation table rarely exists. As considering the moving part, the dynamic model could be time varying system and in such a case the force imposed on pneumatic vibration isolation table could be described by inertial forces of moving parts according to Newton's 3rd law, the action and reaction law. In this paper, the simulation procedure of the 3-DOF active pneumatic vibration isolation system including moving parts by TDC(time delay control) technique is proposed and the effectiveness through simulation results are also shown.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2000년도 제15차 학술회의논문집
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• pp.253-253
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• 2000

Each robot plays a role of its own behavior in dynamic robot-soccer environment. One of the most necessary conditions to win a game is control of robot movement. In this paper we suggest a win strategy using Cellular Neural Network to set optimal path and cooperative behavior, which divides a soccer ground into grid-cell based ground and has robots move a next grid-cell along the optimal path to approach the moving target.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.798-800
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• 2003

The time shift processing of ground measured surface temperature with the meteorological variables has no evaluated function. We introduce new evaluating function. To use this evaluating function, the algorithm of time-shift processing will be able to be reliable and get error-bar for all moving measured point's data. We will finally obtain the area averaged surface temperature by land observation.

• Ocean Systems Engineering
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• 제6권3호
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• pp.245-264
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• 2016

The iterative boundary element method (IBEM) developed originally before for cavitating two-dimensional (2-D) and three-dimensional (3-D) hydrofoils moving under free surface is modified and applied to the case of 2-D (two-dimensional) airfoils and 3-D (three-dimensional) wings over water. The calculation of the steady-state flow characteristics of an inviscid, incompressible fluid past 2-D airfoils and 3-D wings above free water surface is of practical importance for air-assisted marine vehicles such as some racing boats including catamarans with hydrofoils and WIG (Wing-In-Ground) effect crafts. In the present paper, the effects of free surface both on 2-D airfoils and 3-D wings moving steadily over free water surface are investigated in detail. The iterative numerical method (IBEM) based on the Green's theorem allows separating the airfoil or wing problems and the free surface problem. Both the 2-D airfoil surface (or 3-D wing surface) and the free surface are modeled with constant strength dipole and constant strength source panels. While the kinematic boundary condition is applied on the airfoil surface or on the wing surface, the linearized kinematic-dynamic combined condition is applied on the free surface. The source strengths on the free surface are expressed in terms of perturbation potential by applying the linearized free surface conditions. No radiation condition is enforced for downstream boundary in 2-D airfoil and 3-D wing cases and transverse boundaries in only 3-D wing case. The method is first applied to 2-D NACA0004 airfoil with angle of attack of four degrees to validate the method. The effects of height of 2-D airfoil from free surface and Froude number on lift and drag coefficients are investigated. The method is also applied to NACA0015 airfoil for another validation with experiments in case of ground effect. The lift coefficient with different clearance values are compared with those of experiments. The numerical method is then applied to NACA0012 airfoil with the angle of attack of five degrees and the effects of Froude number and clearance on the lift and drag coefficients are discussed. The method is lastly applied to a rectangular 3-D wing and the effects of Froude number on wing performance have been investigated. The numerical results for wing moving under free surface have also been compared with those of the same wing moving above free surface. It has been found that the free surface can affect the wing performance significantly.

• 인터넷정보학회논문지
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• 제7권4호
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• pp.45-55
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• 2006

본 논문에서는 현장감 있는 모의훈련을 위해 가상영상이 아닌 지상기반 CCD 카메라영상에 지정된 시나리오대로 가상표적을 전시하는 방법을 제안한다. 이를 위해 고해상도 GeoTIFF(Geonraphic Tag Image File Format) 위성영상과 DTED(Digital Terrain Elevation Data)를 이용하여 현실감 있는 3차원 모델을 생성(운용자용)하고 입력된 CCD 영상(운용자 훈련자용)으로부터 도로를 추출하였다. 그러나 위성영상과 지상기반 센서영상은 관측위치, 분해능, 스케일 등에 많은 차이가 있어 특징기반 정합이 어렵다. 따라서 본 논문에서는 영상 워핑함수인 TPS(Thin-Plate Spline) 보간 함수를 일치하는 두 개의 제어점 집합에 적용하여 3차원 모델에 표시된 이동경로를 따라 CCD 영상에도 표적을 전시하는 이동 동기화 방법을 제안하였다. 실험에서는 대전지역의 위성영상과 CCD 영상을 이용하여 제안한 알고리즘의 유효성을 입증하였다.

• 전자공학회논문지CI
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• 제48권5호
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• pp.55-63
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• 2011

본 논문은 방위각 및 고저방향으로 카메라 움직임이 있는 감시장치의 비디오 프레임 연속영상을 1)각각 $N{\times}M$ 개의 서브블록으로 나눈 후 각각의 서브블록에 대해 FFT 위상상관 기법을 적용하여 이동표적 위치를 구하고, 2)연속영상을 정합 후 차영상을 구하여 적응 문턱 값을 적용해서 표적후보군을 구하였으며, 3)두 기법을 적용하여 클러터를 제거하는 새로운 표적탐지기법을 제안하였다. 블록 내 다양한 크기의 영상 움직임이 있을 경우 FFT 위상상관 기법은 적용하여 움직임을 구하면 큰 영상의 움직임이 가장 큰 위상상관 값으로 나타나는 특성을 이용하여 배경환경에 강인한 이동표적 위치(블록)탐지를 하였다. 또한, 차영상을 영상분리하기 위한 적응 문턱 값은 카메라 움직임 등 배경환경 변화를 고려한 학습가중치를 이용하여 구하였다. 제안된 알고리즘 성능입증은 다양한 배경환경에서 카메라 이동/정지조건에서 다양한 이동표적에 대해 탐지 가능함을 시뮬레이션을 통해 확인하였으며 탐지성능은 ROC 커브를 통해 확인하였다.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2005년도 춘계학술대회 논문집
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• pp.144-150
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• 2005

After the historic opening of the first section of KTX(Korea Train eXpress), it has been made changes three times in a plan to pass through cities of Daejeon, Daegu in the construction of the high speed train's second section(underground${\to}$ on ground${\to}$ under ground${\to}$ on ground). Thereafter, it has been repeatedly argued that the plan to pass through underground caused many problems such as prevention of an accident in tunnel, the difficulty of maintainence, the disadvantage of passengers' moving line. Thus construction on ground plan is coming up again with relation to the interest among local people. There have been lots of national budget loss, construction period delay in this project and people hardly trust policies about national project and nor do engineers. It will be presented that the railway line which is accorded with the characteristics of region, an agreement with local communities about national project, the reasonable procedure to determine how to pass through cities, resolve the conflict among neighborhood, and the role of engineers.

• International Journal of Aeronautical and Space Sciences
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• 제2권1호
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• pp.28-43
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• 2001

Developed in these two series of paper is a complex dynamic model representing the motion of aircraft on the ground and a computer program for numerical simulation. The first part of paper presents the theoretical derivation of equations of motion of the landing gear system based on the physical principle. Developed model is 'structured' in the sense that the undercarriage system is regarded as an assembly of strut, tire, and wheel, where each component is modeled by a separate module. These modules are linked with two external modules-the aircraft and the runway characteristics-to carry out dynamic analysis and numerical simulation of the aircraft motion on the ground. Three sets of coordinate system associated with strut, wheel/tire and runway are defined, and external loads to each component and response characteristics are examined. Lagrangian formulation is used to derive the undercarriage equations of motion relative to the moving aircraft, and the resultant forces and moments from the undercarriage are transformed to aircraft body axes.

• 대한산업공학회지
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• 제25권2호
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• pp.282-289
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• 1999

To minimize a real world test of underwater guided vehicle, it is necessary to perform a test on ground by using closed loop test techniques. This paper describes implementation of HILS(Hardware In the Loop Simulation) system for ground test and test methodologies for performance evaluation of a guided weapon. HILS system uses a real time distributed computer and a real time processing technique. Ground test results of underwater vehicle are presented for moving and stationary targets by using HILS system.