• Journal of Positioning, Navigation, and Timing
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• 제11권4호
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• pp.287-295
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• 2022

The GNSS coordinate time series is used as important data for geophysical analysis such as terrestrial reference frame establishment, crustal deformation, Earth orientation parameter estimation, etc. However, various factors may cause discontinuity in the coordinate time series, which may lead to errors in the interpretation. In this paper, we describe the discontinuity in the coordinate time series due to the equipment replacement for domestic GNSS stations and discuss the change in movement magnitude and velocity vector difference in each direction before and after discontinuity correction. To do this, we used three years (2017-2019) of data from 40 GNSS stations. The average magnitude of the velocity vector in the north-south, east-west, and vertical directions before correction is -12.9±1.5, 28.0±1.9, and 4.2±7.6 mm/yr, respectively. After correction, the average moving speed in each direction was -13.0±1.0, 28.2±0.8, and 0.7±2.1 mm/yr, respectively. The average magnitudes of the horizontal GNSS velocity vectors before and after discontinuous correction was similar, but the deviation in movement size of stations decreased after correction. After equipment replacement, the change in the vertical movement occurred more than the horizontal movement variation. Moreover, the change in the magnitude of movement in each direction may also cause a change in the velocity vector, which may lead to errors in geophysical analysis.

• Geomechanics and Engineering
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• 제30권6호
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• pp.539-549
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• 2022

Accidental anchor drop can cause disturbances to seabed materials and pose significant threats to the safety and serviceability of submarine structures such as pipelines. In this study, a series of anchor drop tests was carried out to investigate the penetration mechanism of a Hall anchor in sand and clay. A special anchor drop apparatus was designed to model the inflight drop of a Hall anchor. Results indicate that Coriolis acceleration was the primary cause of large horizontal offsets in sand, and earth gravity had negligible impact on the lateral movement of dropped anchors. The indued final horizontal offset was shown to increase with the elevated drop height of an anchor, and the existence of water can slow down the landing velocity of an anchor. It is also observed that water conditions had a significant effect on the influence zone caused by anchors. The vertical influence depth was over 5 m, and the influence radius was more than 3 m if the anchor had a drop height of 25 m in dry sand. In comparison, the vertical influence depth and radius reduced to less than 3 m and 2 m, respectively, when the anchor was released from 10 m height and fell into the seabed with a water depth of 15 m. It is also found that the dynamically penetrating anchors could significantly influence the earth pressure in clay. There is a non-linear increase in the measured penetration depth with kinematic energy, and the resulted maximum earth pressure increased dramatically with an increase in kinematic energy. Results from centrifuge model tests in this study provide useful insights into the penetration mechanism of a dropped anchor, which provides valuable data for design and planning of future submarine structures.

• 지구물리와물리탐사
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• 제16권3호
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• pp.163-170
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• 2013

탄성파 탐사자료의 진폭변화를 분석하면 지층의 유체를 탐지하고 석유 가스 저류층의 정밀한 물성 도출이 가능하다. 본 연구는 동해 울릉분지의 심해 탄성파 탐사자료에 대하여 진폭변화를 분석하고 정리하였다. 중합단면에서 반사신호가 강하게 기록된 영역의 탄성파 공통깊이점-벌림 모음과 공통깊이점-반사각 모음을 관찰하여 진폭변화가 뚜렷한 영역을 선별하였다. 울릉분지의 중앙부 탄성파 탐사 반사각 모음의 주시 3200과 3300 ms 구간 탄성파 신호에 대한 종축절편과 진폭구배 속성을 계산하여 벌림에 따른 진폭 증가 및 감소를 확인하였다. 종축절편과 진폭구배를 곱한 속성과 합한 속성을 도출하여 울릉분지 퇴적층의 가스부존 가능 영역 상부와 하부 경계를 구분하였다. 가스로 포화된 퇴적층의 탄성파 진폭변화 특성을 보이는 영역은 탄성파주시 3 s 인근에서 간헐적으로 나타났다. 교차도표를 이용하여 울릉분지 탄성파자료의 진폭변화를 유형별로 확인할 수 있었다. 배경매질의 종축절편과 진폭구배는 함수 퇴적층의 일반적인 특징인 반비례관계를 보였고 가스함유 퇴적층의 진폭변화를 보이는 표본은 교차도표 단면상에서 1사분면과 3사분면에 위치하였다. 교차도표에서 선택된 표본들을 중합단면에서 추적한 결과 울릉분지 중앙부의 심해 퇴적지층 중 진폭변화 유형 3에 해당하는 영역이 수평연장 150 m 내로 분포함을 유추할 수 있었다.

• 대한토목학회논문집
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• 제26권3D호
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• pp.453-459
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• 2006

본 연구는 차량의 주행경로를 정확하게 측정하는 수단을 개발하고 이를 현장계측에 적용하여 주행차량의 횡방향 이격에 의한 아스팔트 콘크리트 포장(이후 아스팔트 포장)의 주요 응답 특성을 규명하고자 하였다. 개발된 주행이격 측정 시스템은 두 개의 레이저 센서로부터 전송된 신호가 차량의 타이어로부터 반사되어오는 물리적 현상을 실시간으로 분석함으로서 도로 포장위의 임의의 기준으로부터 실제 차량이 주행한 경로를 정확하게 관측 할 수 있다. 다양한 주행이격에 의한 아스팔트 포장의 횡방향 수평 변형률과 하부 포장층의 수직응력 변화를 실측하기 위하여 시험도로상의 아스팔트 포장의 일부 구간을 선정, 덤프트럭에 의한 동하중 재하시험을 시행하였다. 차량의 횡방향 이격거리는 주행차로(2차)의 차륜부에 매설된 횡방향 수평 변형률 계측기의 중심을 기준으로 추월차로 방향으로 20cm 간격으로 조수석 차륜에 의한 하중중첩의 영향을 최대한 배재하도록 설정하였다. 현장시험 결과 표층과 중간층에서는 하중재하 위치에서 발생한 압축변형이 이격거리 약 40cm에서부터 점차 인장으로 변화하고 있음을 알 수 있었다. 또한, 보조기층상부와 동상방지층상부에 작용하는 수직응력은 하중재하 위치에서 치대로 발생하였으며 이격거리 50cm 이상부터는 하중에 의한 영향이 상대적으로 미비하였다.

• 한국실내디자인학회논문집
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• 제17권6호
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• pp.188-196
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• 2008

The study aims to find out the changing aspects of contemporary Korean libraries so called public in terms of their spatial configuration. In so doing, it analysed 14 recently built libraries by investigation of user's behavior. Interview and observation were conducted as a method of investigation. The method of analysis was based on statistics by mapping spatial data. As the result, it could be said that most users have a clear goal in Korea. In some libraries, the distinct characteristics of behavior show that users visit other functional rooms including functional rooms for the purpose. It could be said that the configuration of space in recently public libraries become more public as a place. In view of domestic affairs, in terms of users need, the reading room for personal study have features of the most private room and a static activity. so that the reading room separate from the other functional rooms in floor, but it adjoin other functional rooms in the horizontal configuration. so its location make offset a role of functional rooms can be interactive with each other, except reading room.

• Ocean Systems Engineering
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• 제4권3호
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• pp.215-241
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• 2014

Steel catenary riser (SCR) is a popular/economical solution for the oil/gas production in deep and ultra-deep water. The behavioral characteristics of SCR have a high correlation with the motion of floating production facility at its survival and operational environments. When large motions of surface floaters occur, such as FPSO in 100-yr storm case, they can cause unacceptable negative tension on SCR near TDZ (touch down zone) and the corresponding elastic deflection can be large due to local dynamic buckling. The generation, propagation, and decay of the elastic wave are also affected by SCR and seabed soil interaction effects. The temporary local dynamic buckling vanishes with the recovery of tension on SCR with the upheaval motion of surface floater. Unlike larger-scale, an-order-of-magnitude longer period global buckling driven by heat and pressure variations in subsea pipelines, the sub-critical local dynamic buckling of SCR is motion-driven and short cycled, which, however, can lead to permanent structural damage when the resulting stress is greatly amplified beyond the elastic limit. The phenomenon is extensively investigated in this paper by using the vessel-mooring-riser coupled dynamic analysis program. It is found that the moment of large downward heave motion at the farthest-horizontal-offset position is the most dangerous for the local dynamic buckling.

• JSTS:Journal of Semiconductor Technology and Science
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• 제13권3호
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• pp.198-206
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• 2013

This paper presents a wide band, fine-resolution digitally controlled oscillator (DCO) with an on-chip 3-D solenoid inductor using the 0.13 ${\mu}m$ digital CMOS process. The on-chip solenoid inductor is vertically constructed by using Metal and Via layers with a horizontal scalability. Compared to a spiral inductor, it has the advantage of occupying a small area and this is due to its 3-D structure. To control the frequency of the DCO, active capacitor and active inductor are tuned digitally. To cover the wide tuning range, a three-step coarse tuning scheme is used. In addition, the DCO gain needs to be calibrated digitally to compensate for gain variations. The DCO with solenoid inductor is fabricated in 0.13 ${\mu}m$ process and the die area of the solenoid inductor is 0.013 $mm^2$. The DCO tuning range is about 54 % at 4.1 GHz, and the power consumption is 6.6 mW from a 1.2 V supply voltage. An effective frequency resolution is 0.14 kHz. The measured phase noise of the DCO output at 5.195 GHz is -110.61 dBc/Hz at 1 MHz offset.

• 센서학회지
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• 제13권3호
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• pp.188-194
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• 2004

With a remarkable advance in CMOS (complimentary metal-oxide-semiconductor) process technology, a variety of vision sensors with signal processing circuits for complicated functions are actively being developed. Especially, as the principles of signal processing in human retina have been revealed, a series of vision chips imitating human retina have been reported. Human retina is able to detect the edge and motion of an object effectively. The edge detection among the several functions of the retina is accomplished by the cells called photoreceptor, horizontal cell and bipolar cell. We designed a CMOS vision chip by modeling cells of the retina as hardwares involved in edge and motion detection. The designed vision chip was fabricated using $0.6{\mu}m$ CMOS process and the characteristics were measured. Having reliable output characteristics, this chip can be used at the input stage for many applications, like targe tracking system, fingerprint recognition system, human-friendly robot system and etc.

• 복식문화연구
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• 제8권1호
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• pp.15-29
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• 2000

Nowadays every part no company continues to gain the upper hand of a competitive superiority. Strategic Alliances between companies have been rapidly increased to preoccupy a market. The purpose of this study is to find devices of strategic alliances for the competitive distribution environment of Korean fashion industries. This reseach has been done by the literature review of the related articles, books, and the case studies in domestic markets as well as foreign ones. Strategic alliances are business relationships established by tow or more companies which cooperate out of mutual need and share risk in achieving a common objective. Today the purpose of international strategic alliances is to be competitive in global markets by meeting of exceeding new standards for products and technology use. Various types of alliances are occurred and this situation will be more common and generalized since one parter's weakness is offset by the other's strength. Strategic alliances are characterized by being horizontal, collaborative, and mutually beneficial to all parties. When used in good faith, the strengths gained in a strategic alliance are great. Therefore retailer should find that to gain faithful partners is important and should effort positively to enrich alliances based on a mutual belief. Finally, to become a company for leading the global market, it is necessary that we operate strategic alliances mixed foreign investments and domestic technology with local distributions.

• Journal of Astronomy and Space Sciences
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• 제26권1호
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• pp.47-58
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• 2009

In this study, a Hardware-In-the-Loop (HIL) simulator using thrusters is developed to validate the spacecraft attitude system. To control the attitude of the simulator, eight cold gas thrusters are aligned with roll, pitch and yaw axis. Also linear actuators are applied to the HIL simulator for automatic mass balancing to compensate the center of mass offset from the center of rotation. The HIL simulator consists of an embedded computer (Onboard PC) for simulator system control, a wireless adapter for wireless network, a rate gyro sensor to measure 3-axis attitude of the simulator, an inclinometer to measure horizontal attitude, and a battery set to supply power for the simulator independently. For the performance test of the HIL simulator, a bang-bang controller and Pulse-Width Pulse-Frequency (PWPF) modulator are evaluated successfully. The maneuver of 68 deg. in yaw axis is tested for the comparison of the both controllers. The settling time of the bang -bang controller is faster than that of the PWPF modulator by six seconds in the experiment. The required fuel of the PWPF modulator is used as much as 51% of bang-bang controller in the experiment. Overall, the HIL simulator is appropriately developed to validate the control algorithms using thrusters.