• 항공우주산업기술동향
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• 제7권2호
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• pp.115-120
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• 2009

본 논문에서는 원형마크를 이용한 항공기와 활주로간의 새로운 거리측정시스템에 관한 내용이다. 이 시스템은 항공기에 카메라와 고도계를 장착하고 활주로에 원형마크가 있어야 한다. 항공기에 장착된 카메라는 반드시 항공기의 진행방향을 향하면서 원형마크를 영상이미지형태로 간파하여 이미 장착한 고도계의 고도값과 함께 비행조종컴퓨터가 항공기와 지상간의 각도, 항공기와 원형마크간의 지상거리, 그리고 기울기거리를 계산하여야 한다. 이 시스템은 무인기의 자동착륙에 사용될 수 있다.

• 한국산학기술학회논문지
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• 제20권9호
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• pp.474-480
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• 2019

본 연구에서는 무인항공영상의 품질 평가를 위해 공간해상도 검정 방법 중 하나인 MTF(Modulation Transfer Function)를 Circular target을 이용하여 평가하는 방안을 제시하고, MATLAB GUI 기반 해상도 분석 Tool을 제작하여 무인항공영상 품질의 신뢰도와 작업의 효율성을 높이고자 하였다. 이를 위해 무인항공기체인 DJI Phantom 4 Pro(FC 6310)기체는 80m, 120m, 150m, Matrice 600(iXM-100)기체는 150m, 200m, 400m의 서로 다른 고도에서 촬영하였으며, 유인항공영상과 비교를 위해 UltraCAM Eagle Mark 2 센서로 비행고도 1000m에서 영상을 촬영하여 MTF를 비교하였다. 연구 결과 DJI Phantom 4 Pro(FC 6310)기체의 ${\sigma}MTFs$ 수치는 촬영고도에 따라 0.431, 0.524, 0.699, Matrice 600(iXM-100)기체의 ${\sigma}MTFs$ 수치는 촬영고도에 따라 0.332, 0.393, 0.631의 결과를 나타내어 촬영고도가 높아질수록 영상의 품질이 낮아짐을 알 수 있었다. 동일한 고도인 150m의 경우 탑재된 카메라의 성능이 높은 Matrice 600(iXM-100)기체의 영상품질이 매우 높은 결과를 나타내어 카메라의 성능이 영상의 품질에 미치는 영향을 확인할 수 있었다. 또한, UltraCAM Eagle Mark 2 센서를 탑재한 유인항공영상의 ${\sigma}MTF$ 수치는 높은 비행고도로 인하여 0.711의 결과를 나타내어 모든 무인항공영상의 품질보다 낮은 결과를 나타내었다. 하지만 DJI Phantom 4 Pro(FC 6310)기체의 150m 고도에서 촬영한 무인항공영상에서 ${\sigma}MTF$ 수치는 0.699의 결과를 나타내어 유인항공영상의 품질과 거의 비슷한 결과를 나타내었다.

• 한국해양공학회지
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• 제15권1호
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• pp.12-18
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• 2001

This study concentrates on the second-order diffraction problem around circular cylinders in multi-frequency waves. The method of solution is a time-domain Rankine panel method which adopts a higher-order approximation for the velocity potential and wave elevation. In the present study, the multiple second-order quadratic transfer functions are extracted from the second-order time signal generated in random waves, and the comparison with other bench-mark test results shows a good agreement. This approach is directly applicable to prediction of nonlinear forces on offshore structures in random ocean.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2004년도 추계학술대회 논문집
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• pp.127-130
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• 2004

For the quality control of the industrial products, an automatic hole measuring system has been developed. The measurement device allows X-Y movement due to contact forces between a hole and its own circular cone and the device is attached to an industrial robot. Its measurement accuracy is about 0.04mm. This movement of the plate is measured by two LVDT sensor system. But this system using the LVDT sensors is restricted by high cost and precision of measurement and correspondence of environment so particularly, a vision system with CCD-Camera is discussed in this paper for the above mentioned purpose. The device consists of two of two links jointed with hinge pins basically and, they guarantee free movement of the touch prove attached on the second link in the same plane. These links are returned to home position by the spring plungers automatically after each process for the next one. On the surface of the touch prove, it has a circular white mark for camera recognition. The system detect and notify the center coordinate of capture mark image through the image processing. Its measuring accuracy has been proved to be about $\pm$0.01mm through the repeated implementation over 200 times. This technique will shows the advantage of touch-indirect image capture idea using cone-shaped touch prove in various symmetrical shaped holes particulary, like tapped holes, chamfered holes, etc As a result, we attained our object in a view of the accuracy, economical efficiency, and functionality

• Korean Chemical Engineering Research
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• 제53권5호
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• pp.609-613
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• 2015

The onset of instability induced by impulsive spin-down of the rigid-body flow placed in the gap between two coaxial cylinders is analyzed by using the energy method. In the present stability analysis the growth rate of the kinetic energy of the base state and also that of disturbances are taken into consideration. In the present system the primary flow is a transient, laminar one. But for the Reynolds number equal or larger than a certain one, i.e. $Re{\geq}Re_G$ secondary motion sets in, starting at a certain time. For $Re{\geq}Re_G$ the dimensionless critical time to mark the onset of vortex instabilities, ${\tau}_c$, is here presented as a function of the Reynolds number Re and the radius ratio ${\eta}$. For the wide gap case of small ${\eta}$, the transient instability is possible in the range of $Re_G{\leq}Re{\leq}Re_S$. It is found that the predicted ${\tau}_c$-value is much smaller than experimental detection time of first observable secondary motion. It seems evident that small disturbances initiated at ${\tau}_c$ require some growth period until they are detected experimentally.

• Nuclear Engineering and Technology
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• 제34권6호
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• pp.553-565
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• 2002

In this paper, the robust control scheme with the improved control performance within the boundary layer is proposed. In the control scheme, the robust controller based on the traditional variable structure control method is modified to have the adaptation within the boundary layer. From this controller, the width of the boundary layer where the robust control input is smoothened out can be given by an appropriate value. But the improved control performance within the boundary layer can be achieved without the so-called control chattering because the role of adaptive control is to compensate for the uncovered portions of the robust control occurred from the continuous approximation within the boundary layer Simulation tests for circular navigation of an underwater wall-ranging robot developed for inspection of wall surfaces in the research reactor, TRIGA MARK III, confirm the performance improvement. Notational Conventions Vectors are written in boldface roman lower-case letters, e.g., x and y. Matrices are written in upper-case roman letters, e.g., G and B. And ∥.∥ means the Euclidean norm.

• Structural Engineering and Mechanics
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• 제53권1호
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• pp.73-87
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• 2015

In case of aircraft impact on nuclear containment structures, the initial kinetic energy of the aircraft is transferred and absorbed by the outer containment, may causing either complete or partial failure of containment structure. In the present study safety analysis of BWR Mark III type containment has been performed. The total height of containment is 67 m. It has a circular wall with monolithic dome of 21m diameter. Crash analysis has been performed for fighter jet Phantom F4. A normal hit at the crown of containment dome has been considered. Numerical simulations have been carried out using finite element code ABAQUS/Explicit. Concrete Damage Plasticity model have been incorporated to simulate the behaviour of concrete at high strain rate, while Johnson-Cook elasto-visco model of ductile metals have been used for steel reinforcement. Maximum deformation in the containment building has reported as 33.35 mm against crash of Phantom F4. Deformations in concrete and reinforcements have been localised to the impact region. Moreover, no significant global damage has been observed in structure. It may be concluded from the present study that at higher velocity of aircraft perforation of the structure may happen.

• 한국지구과학회지
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• 제42권2호
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• pp.185-194
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• 2021

제주도 북서부인 애월 해안에는 평탄하게 흐른(판상) 용암류와 둥근 모양(원통)의 용암류가 관찰된다. 원통형 용암류의 치밀한 내부에는 동심원 구조와 방사상 절리가 발달한다. 구엄리 돌염전 주변의 판상 용암류 내부에는 상하부의 굵기가 다른 주상절리가 발달한다. 주상절리 상부는 다각형의 형태가 고르지 않으며 직경은 120-150 cm이다. 주상절리 하부는 육각형과 오각형으로 형태가 일정하고, 크기도 60 cm 내외이다. 원통형 로브는 크기와 형태에 따라 두 그룹으로 나눌 수 있다. 하나는 메가로브인데, 최대 직경이 30 m인 반원형이다. 또 하나는 원형의 로브로 직경이 10 m 이하이다. 원통형 용암류의 방사상 절리의 기둥 단면은 육각형과 오각형이며, 기둥의 직경은 중심에서 바깥쪽으로 증가하는데 바깥쪽 경계부에서는 80-120 cm 정도이다. 원통형 용암에서 관찰되는 동심원 구조는 4가지 요인이 복합된 것이다. 첫째는 원형의 균열로, 원통형 용암류 내에서 안쪽과 바깥쪽 사이의 온도차와 밀도차로 발생한 수축으로 생긴 틈새이다. 둘째는 방사상 절리의 마디층이 동심원을 이룬 것으로, 이 마디층은 방사상 절리와 동시에 만들어진 것이다. 셋째는 유동띠로서, 용암이 흐를 때 둥근 통로에 남긴 흔적이다. 네 번째는 용암에서 빠져나온 가스가 동굴에 형성된 기공 띠이다.

• Journal of Welding and Joining
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• 제32권6호
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• pp.1-7
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• 2014

For the resistance spot welds of CR1180 and GA1180 TRIP steels, the weld quality evaluation method using the digitalized X-ray transmission imaging apparatus was investigated in comparison with the crosssectional examination method. In the case of the resistance spot welding of CR1180, three circular regions, such as WZ(white zone), GZ(grey zone) and DZ(dark zone), appeared on X-ray image and they corresponded to the diameters of indentation mark, nugget and corona bond, respectively. The variation of X-ray transmission thickness due to the thickness variation of the weld seemed to be mainly responsible for the formation of those contrasts. The X-ray image contrast formed from the variation of transmission thickness at the outer border line of DZ could also enable the inspections of the notch shape, nonuniformity of the welding pressure and spatter from its sharpness, concentricity and the normal straight line, respectively. The X-ray image of the resistance spot weld of galvannealed GA1180 TRIP steel was very similar to that of CR1180 TRIP steel except the crown shaped outer border line of DZ which was considered to be due to the melting behavior of zinc having the boiling temperature even lower than the melting temperature of steel.

• Steel and Composite Structures
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• 제20권2호
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• pp.379-397
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• 2016

Due to creep and shrinkage of the concrete core, concrete-filled steel tubular (CFST) arches continue to deform in the long-term under sustained loads. This paper presents analytical investigations of the effects of geometric nonlinearity on the long-term in-plane structural performance and stability of three-pinned CFST circular arches under a sustained uniform radial load. Non-linear long-term analysis is conducted and compared with its linear counterpart. It is found that the linear analysis predicts long-term increases of deformations of the CFST arches, but does not predict any long-term changes of the internal actions. However, non-linear analysis predicts not only more significant long-term increases of deformations, but also significant long-term increases of internal actions under the same sustained load. As a result, a three-pinned CFST arch satisfying the serviceability limit state predicted by the linear analysis may violate the serviceability requirement when its geometric nonlinearity is considered. It is also shown that the geometric nonlinearity greatly reduces the long-term in-plane stability of three-pinned CFST arches under the sustained load. A three-pinned CFST arch satisfying the stability limit state predicted by linear analysis in the long-term may lose its stability because of its geometric nonlinearity. Hence, non-linear analysis is needed for correctly predicting the long-term structural behaviour and stability of three-pinned CFST arches under the sustained load. The non-linear long-term behaviour and stability of three-pinned CFST arches are compared with those of two-pinned counterparts. The linear and non-linear analyses for the long-term behaviour and stability are validated by the finite element method.