• 대한공간정보학회지
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• 제19권4호
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• pp.119-126
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• 2011

초고층 건물이나 고가 구조물 상부의 정위치 측설에 주로 사용되어 왔던 광학식 TS장비는 시준선 확보의 어려움, 장거리 관측에 따른 오차의 증가 및 동적관측의 어려움 등으로 인하여 사용성이 많이 떨어지므로 최근에는 GPS를 이용한 측량방법이 제시되고 있다. 그러나 기존의 GPS측량방법들은 대부분 후처리 방법으로서 측설, 검측, 위치조정 및 확인측량 등 일련의 과정에서 시간이 과다 소요되는 문제점이 있다. 따라서 본 논문에서는 RTK측위 기법을 적용하여 실시간으로 구조물의 위치를 검측하고 조정함으로써 측량으로 인한 공사의 중단을 최소화 하고, 준스태틱 RTK기법에 의한 고정밀의 측정값을 기반으로 망조정을 통해 수 mm 이내의 높은 정확도로 시공좌표를 결정함으로써 공정관리와 품질관리를 모두 충족시킬 수 있는 방법에 대해 실험 하였다. 실험결과 130m 이상 높이의 고가 구조물 상층부에서 사변망을 이루는 4점의 준스태틱 RTK 관측점을 최소제곱법으로 망조정 하면 약 2mm 내외의 정확도로 구조물 측설이 가능하므로 향후 초고층 건물이나 고가 교량등의 시공측량에 널리 적용될 수 있을 것으로 사료된다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2003년도 춘계학술대회 논문집
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• pp.158-161
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• 2003

Recently, the evolution in production techniques (e.g. high-speed milling), the complex shapes involved in modem production design, and the ever increasing pressure for higher productivity demand a drastic improvement of the dynamic behavior of the machine tool axes used in production machinery. And also machine tools of multi functional and minimized parts are increasingly required as demand of higher accurate in some fields such as electronic and optical components etc. The accuracy and the productivity of machined parts are natural to depend on the linear system of machine tools. The complex workpiece surfaces encountered in present-day products and generated by CAD systems are to be transformed into tool paths for machine tools. The more complex these tool paths and the higher the speed requirements, the higher the acceleration requirements are needed to the machine tool axes and the motion control system, and the more difficult it is to meet the requirements. The traditional indirect drive design for high speed machine tools, which consists of a rotary motor with a ball-screw transmission to the slide, is limited in speed, acceleration, and accuracy. The direct drive design of machine tool axes. which is based on linear motors and which recently appeared on the market. is a viable candidate to meet the ever increasing demands, because of these advantages such as no backlash, less friction, no mechanical limitations on acceleration and velocity and mechanical simplicity. Therefore performance tests were carried out to machine tool axes based on linear motor. Especially, dynamic characteristics were investigated through circular test.

• 한국해양학회지:바다
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• 제24권1호
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• pp.30-48
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• 2019

2018년은 해양 과학시추가 시작된 지 50년이 되는 해이다. 그럼에도 불구하고 우리는 지구의 대양저보다 달의 표면을 더 많이 알고 있을 정도로 지구내부에 대한 정보가 많지 않다. 대양저에 관한 연구는 해양 과학시추로부터 얻어진 시료를 통해서 알 수 있다. 이러한 심해의 시료획득은 50년 전인 1968년 8월 11일 미연방차원에서 지원된 심해저시추계획(DSDP: Deep Sea Drilling Project)에서 글로마 챌린저(Glomar Challenger)호를 이용한 멕시코 만 시추로부터 시작되었다. 이후 해저지각시추프로그램(ODP: Ocean Drilling Program), 통합해저지각시추프로그램(old IODP: Integrated Ocean Drilling Program), 그리고 국제해양시추탐사프로그램 (new IODP: International Ocean Discovery Program)으로 이어져 오고 있다. 해양 과학시추로부터 얻어진 가장 큰 성과는 두 가지 기술적인 성과와 다양한 과학적인 성과로 나눠진다. 첫 번째 기술적인 성과는 시추선이 시추위치를 벗어나지 않고 연속적으로 시추코어를 획득할 수 있도록 위치를 유지시켜주는 동적위치유지 시스템(dynamic positioning system)이다. 다른 하나는 시추동안 드릴 비트를 교체한 후 동일한 시추공에 드릴비트가 쉽게 투입될 수 있도록 해주는 재투입 콘(re-entry cone)의 개발이다. 이러한 기술적인 혁신 외에도 다양한 과학적 성과 즉 판구조론 증명, 지구의 역사 규명, 그리고 심해 퇴적물 내 생명체의 발견 등이 있다. 2013년 10월 시작된 국제해양시추탐사프로그램(new IODP)은 2023년까지 계속될 예정이고, 2023년 이후 다음 단계를 위해 참여 회원국들은 새로운 과학계획 수립과 더불어 미래의 해양 과학시추 50년을 준비하고 있다. 우리나라도 이러한 국제적인 동향에 발맞추어 회원국가로서 지속적인 참여와 다음단계를 위한 준비가 필요한 시점이다.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2008년도 한국우주과학회보 제17권2호
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• pp.34.3-34.3
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• 2008

Relative navigation system is presented using measurements from a single-channel global positioning system (GPS) simulator. The objective of this study is to provide real-time relative navigation results as well as absolute navigation results for two formation flying satellites separated about 1km in low earth orbit. To improve the performance, more accurate dynamic model and modified relative measurement model are developed. This modified method prevents non-linearity of the measurement model from degrading precision by applying linearization about the states from absolute navigation algorithm not about a priori states. Furthermore, absolute states are obtained using ion-free GRAPHIC pseudo-ranges and precise relative states are provided using double differential carrier-phase data based on Extended Kalman Filter. The software-based simulation is performed and achieved meter-level precision for absolute navigation and millimeter-level precision for relative navigation. The absolute and relative accuracies at steady state are about 0.77m and 4mm respectively (3D, r.m.s.). In addition, Integer ambiguity algorithm (LAMBDA method) improves simulation performances.

• Ocean and Polar Research
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• 제37권3호
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• pp.235-247
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• 2015

The main purpose of procuring the oceanographic research vessel with state-of-the-art technology is to provide a floating laboratory to conduct field work on the global oceans. The vessel should be properly utilized to locate and evaluate unexplored natural resources as well as to contribute international efforts to better understand and manage global environmental issues. Top priorities in the vessel design are high safety standards, noise and vibration control efficiency, and effective application of research equipment. For the accomplishment of all activities, the vessel length over all should be extended ~100 m with a gross tonnage of ~5,900 ton. In particular, the dynamic positioning system II will essentially operate at sea state 6. The high efficiency emissions reduction system will also be adopted in preparation for entry into force of 3rd exhaust emission control (Tier III). About 130 navigational and scientific instruments will be installed. The final design and model test of the new research vessel were reviewed and completed, respectively, in 2014. Currently, the ship is being built on schedule and expected to be delivered in December 2015. Within the near future, the new vessel will assume the role of carrying out multidisciplinary oceanographic researches of the highest standards in a technologically advanced and environment friendly manner.

• 대한기계학회논문집
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• 제19권7호
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• pp.1604-1618
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• 1995

In the process of mechanical assembly design, assembly modeling systems have been used mainly for the design verification before manufacturing by enabling to check the interference and/ or the dynamic and kinematic performance. However, the conventional assembly modeling systems have a shortcoming that they can not be used in the initial design stage but can be used only after the design is fully completed. In other words conventional assembly modeling systems provide bottom-up modeling which means that the detailed modeling of components must precede the definition of relationships between them. To resolve this problem, an assembly modeling system is proposed to provide a top-down modeling environment in which components and assembly can be modeled simultaneously. To this end, an assembly data structure suitable for top-down assembly modeling has been established. Feature positioning Module(FPM) using geometric constraints has been also developed. The Sekective Solving Method proposed for FPM is based on the priority between the constraint equations and enables the designer's intent expressed by geometric constraints to be maintained throughout the whole modeling process. Finally, the feature based modeling technique using two-level features has been developed. Two-level features include an abstract model and a detailed model in a merged form in non-manifold data frame.

• 대한공간정보학회지
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• 제3권2호
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• pp.221-225
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• 1995

단일 GPS위치 측정시 일반 사용자는 측정 오차들과 미국방성의 의도적인 오차들로 인해 항법이나 측지등의 응용분야에서 만족할만한 정확도를 얻을 수 없다. DGPS(Differential GPS)는 이러한 제약들을 해결할 수 있는 방법으로, 이는 이미 정확한 좌표를 알고 있는 기준국과 좌표를 알고자 원하는 지점간의 공통 오차를 제거하여 좌표를 구하는 방법으로 높은 정확도를 얻을 수 있다. 본 논문에서는 기지의 기준국 좌표와 GPS위성에서 수신한 자료들 사이에서 구한 기준국 좌표사이의 편차를 이용한 DGPS방법을 정적 실험 및 선박을 이용한 동적 실험등을 통하여 후처리 방법으로 구현하였다.

• Journal of Astronomy and Space Sciences
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• 제26권1호
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• pp.59-74
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• 2009

Relative navigation system is presented using GPS measurements from a single-channel global positioning system (GPS) simulator. The objective of this study is to provide the real-time inter-satellite relative positions as well as absolute positions for two formation flying satellites in low earth orbit. To improve the navigation performance, the absolute states are estimated using ion-free GRAPHIC (group and phase ionospheric correction) pseudo-ranges and the relative states are determined using double differential carrier-phase data and singled-differential C/A code data based on the extended Kalman filter and the unscented Kalman filter. Furthermore, pseudo-relative dynamic model and modified relative measurement model are developed. This modified EKF method prevents non-linearity of the measurement model from degrading precision by applying linearization about absolute navigation solutions not about the priori estimates. The LAMBDA method also has been used to improve the relative navigation performance by fixing ambiguities to integers for precise relative navigation. The software-based simulation has been performed and the steady state accuracies of 1 m and 6 mm ($1{\sigma}$ of 3-dimensional difference errors) are achieved for the absolute and relative navigation using EKF for a short baseline leader/follower formation. In addition, the navigation performances are compared for the EKF and the UKF for 10 hours simulation, and relative position errors are mm-level for the two filters showing the similar trends.

• Journal of Power Electronics
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• 제10권6호
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• pp.579-586
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• 2010

This paper presents the organisation and the technical structure of a remote controlled laboratory in the field of high dynamic drives and motion control. It is part of the PEMCWebLab project with the goal of providing students with practical experience on real systems in the field of power electronics and drives. The whole project is based on clear targets and leading ideas. A set of experiments can be remotely performed on a real system to stepwise identify a two axes positioning system and to design different cascaded control loops. Each single experiment is defined by its goals, the content of how to achieve them, and a verification of the results as well as the achieved learning outcomes. After a short description of the PEMCWebLab project, the structure of the remote control is presented together with the hardware applied. One important point is error handling as real machines and power electronics are applied. Finally, a selection of experiments is presented to show the graphical user interface and the sequence of the laboratory.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
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• pp.235-240
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• 2006

Ionospheric scintillation induces a rapid change in the amplitude and phase of radio wave signals. This is due to irregularities of electron density in the F-region of the ionosphere. It reduces the accuracy of both pseudorange and carrier phase measurements in GPS/satellite based Augmentation system (SBAS) receivers, and can cause loss of lock on the satellite signal. Scintillation is not as strong at mid-latitude regions such that positioning is not affected as much. Severe effects of scintillation occur mainly in a band approximately 20 degrees on either side of the magnetic equator and sometimes in the polar and auroral regions. Most scintillation occurs for a few hours after sunset during the peak years of the solar cycle. This paper focuses on estimation of the effects of ionospheric scintillation on GPS and SBAS signals using a software receiver. Software receivers have the advantage of flexibility over conventional receivers in examining performance. PC based receivers are especially effective in studying errors such as multipath and ionospheric scintillation. This is because it is possible to analyze IF signal data stored in host PC by the various processing algorithms. A L1 C/A software GPS receiver was developed consisting of a RF front-end module and a signal processing program on the PC. The RF front-end module consists of a down converter and a general purpose device for acquiring data. The signal processing program written in MATLAB implements signal acquisition, tracking, and pseudorange measurements. The receiver achieves standalone positioning with accuracy between 5 and 10 meters in 2drms. Typical phase locked loop (PLL) designs of GPS/SBAS receivers enable them to handle moderate amounts of scintillation. So the effects of ionospheric scintillation was estimated on the performance of GPS L1 C/A and SBAS receivers in terms of degradation of PLL accuracy considering the effect of various noise sources such as thermal noise jitter, ionospheric phase jitter and dynamic stress error.