• 한국측량학회지
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• 제33권6호
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• pp.485-495
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• 2015

The Tohoku Earthquake, which hit Japan on March 11, 2011, was a massive magnitude 9.0 earthquake, with the earthquake itself causing damage and the resulting tsunami additionally causing enormous material and human damage. The crustal deformation at that time reached a maximum of 5.24 m in Japan, Neighboring countries South Korea and China as well as the Southeast Asian region also witnessed crustal deformation ranging from a few centimeters to a few meters. The detailed analysis in this study based on data from 72 of the sites in South Korea where GNSS CORS was installed showed that South Korea underwent heterogeneous crustal deformation from the Tohoku earthquake, with a maximum of 55.5 mm, a minimum of 9.2 mm, and an average of 22.42 mm. A crustal deformation model was developed, applied, and evaluated for accuracy in this study for a prompt revision of the survey results of the control points that were changed by the crustal deformation. The survey results were revised by applying a crustal deformation model to the 1,195 unified control points installed in South Korea prior to the Tohoku earthquake. The comparison of these 1,195 points with their new survey results showed that the RMSE decreased from 14.1 to 3.4 mm and that the maximum result difference declined from 39 to 10 mm. Revision of the survey results of the control points using the crustal deformation model is deemed very useful considering that the accuracy of the survey results of the unified control points in South Korea is 3 cm.

• 제어로봇시스템학회논문지
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• 제20권8호
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• pp.890-894
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• 2014

In this paper, we derive the CRLB (Cramer-Rao Lower Bound) of effective carrier-to-noise power ratio ($C/N_0$) estimation for a GPS (Global Positioning System) L1 C/A (Coarse/Acquisition) signal under band-limited white noise jamming environments. The quality of a received GPS signal is commonly described in terms of its $C/N_0$, implying that the noise is white and thus can be described by scalar noise density. However, if some intentional interference is received to a victim GPS receiver, then the $C/N_0$ is no longer the efficacious performance indicator. The correct and straightforward measurement to analyze the receiving situation is the effective $C/N_0$. In this paper, we consider a band-limited white noise jamming whose bandwidth is 2MHz and is the same as one of the first null-to-null bandwidth of the GPS L1 C/A signal.

• 한국측량학회지
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• 제37권5호
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• pp.367-377
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• 2019

As an alternative navigation system for the non-GNSS (Global Navigation Satellite System) environment, a new type of DBRN (DataBase Referenced Navigation) which applies both gravity gradient and terrain, and combines filter-based algorithm with profile matching was suggested. To improve the stability of the performance compared to the previous study, both centralized and decentralized EKF (Extended Kalman Filter) were constructed based on gravity gradient and terrain data, and one of filters was selected in a timely manner. Then, the final position of a moving vehicle was determined by combining a position from the filter with the one from a profile matching. In the simulation test, it was found that the overall performance was improved to the 19.957m by combining centralized and decentralized EKF compared to the centralized EKF that of 20.779m. Especially, the divergence of centralized EKF in two trajectories located in the plain area disappeared. In addition, the average horizontal error decreased to the 16.704m by re-determining the final position using both filter-based and profile matching solutions. Of course, not all trajectories generated improved performance but there is not a large difference in terms of their horizontal errors. Among nine trajectories, eights show smaller than 20m and only one has 21.654m error. Thus, it would be concluded that the endemic problem of performance inconsistency in the single geophysical DB or algorithm-based DBRN was resolved because the combination of geophysical data and algorithms determined the position with a consistent level of error.

• 한국측량학회지
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• 제39권5호
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• pp.343-349
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• 2021

In The process from design to construction in the existing construction work was less efficient due to the contradictory approach of identifying the 3D state in the plan view and the repeated generation of surveys, floor plans, drawings. Accurate 3D design data is essential for smart construction. However, most of the existing related studies have focused on explaining the development method and main functions of equipment or improving the productivity of smart construction. Therefore, in this study, the utility of 3D design model generation for smart construction and construction survey using 3D laser scanner was evaluated. Plane and vertical road alignment were created using the specifications of the road. The generated road alignment was created as a three-dimensional corridor design using cross-sections at intervals of 20m. In addition, it was possible to create a DTM (Digital Terrain Model) using a digital map and effectively create a 3D design model for the study area through overlapping. Construction survey using a 3D laser scanner showed accuracy within 10cm as a result of the accuracy evaluation. These results proved that construction surveying using a 3D laser scanner is possible because it satisfies the acceptable accuracy of the relevant regulations modeling of target areas using 3D design and construction survey using 3D laser scanner can be a way to address shortcomings of existing GNSS (Global Navigation Satellite System) methods. And accurate 3D data will be used as essential data as basic data for smart construction.

• 도시과학
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• 제7권2호
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• pp.53-60
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• 2018

Digital Twin is a technology that creates a photocopy of real-world objects on a computer and analyzes the past and present operational status by fusing the structure, context, and operation of various physical systems with property information, and predicts the future society's countermeasures. In particular, 3D rendering technology (UAS, LiDAR, GNSS, etc.) is a core technology in digital twin. so, the research and application are actively performed in the industry in recent years. However, UAS (Unmanned Aerial System) and LiDAR (Light Detection And Ranging) have to be solved by compensating blind spot which is not reconstructed according to the object shape. In addition, the terrestrial LiDAR can acquire the point cloud of the object more precisely and quickly at a short distance, but a blind spot is generated at the upper part of the object, thereby imposing restrictions on the forward digital twin modeling. The UAS is capable of modeling a specific range of objects with high accuracy by using high resolution images at low altitudes, and has the advantage of generating a high density point group based on SfM (Structure-from-Motion) image analysis technology. However, It is relatively far from the target LiDAR than the terrestrial LiDAR, and it takes time to analyze the image. In particular, it is necessary to reduce the accuracy of the side part and compensate the blind spot. By re-optimizing it after fusion with UAS and Terrestrial LiDAR, the residual error of each modeling method was compensated and the mutual correction result was obtained. The accuracy of fusion-based 3D model is less than 1cm and it is expected to be useful for digital twin construction.

• 한국산학기술학회논문지
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• 제21권1호
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• pp.14-19
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• 2020

본 논문은 차등 위성항법 보정 시스템을 이용한 측위 오차 보정을 통해 소형 드론의 위치를 정밀하게 계측할 수 있는 시스템 구현에 대해 서술하고 있다. 본 시스템은 고정된 위치에 자리하는 기준국과 실시간으로 움직이는 이동국(드론)으로 이루어져 있다. 자체 기준국 위치 정보와 국가에서 제공하는 관측 정보를 함께 후처리하여 기준국의 정밀 좌표를 획득하는 과정에 대해 서술하고, 이동국을 정밀 추적하기 위한 차등 위성 항법 시스템의 하드웨어 및 소프트웨어 구성에 대해 설명한다. 기준국 및 이동국 구현에 있어 저가의 경량 위성 항법 수신기 및 오픈소스 소프트웨어 코드와 라이브러리를 활용하여 범용성과 경제성을 극대화 하였으며, 오차 보정 정보 송수신에는 비 면허 주파수 대역 무선통신인 지그비(Zigbee)를 사용하였다. 본 시스템을 이용하여 소형 드론 위치 추적 시험 결과, 평균 측위 오차가 0.8m 및 최대 측위 오차가 1.2m로, 단일 위성 항법 수신기를 사용했을 경우 대비 오차가 86% 개선됨을 확인할 수 있었다.

• 한국정보통신학회논문지
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• 제19권8호
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• pp.1959-1964
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• 2015

본 논문은 미국정부의 SA정책 및 GPS 현대화 정책 추진으로 진화 해 온 민간용 GPS 수신신호의 항법파라미터 분석에 중점을 둔 연구로서, 향후 GPS 신호를 포함하거나 또는 포함하지 않는 복합 위성항법시스템에 대한 종합분석을 하기 위한 연구이다. 특히, 본 논문에서는 위성의 기하학적 행렬을 기초로 한 GDOP 이론에 대한 체계적 정립과, 위성배열의 변화 및 반송파대 잡음비의 변화에 따른 L1, C/A 수신 신호를 수집하여 통계적 분석을 하였다. HDOP 0.5, PDOP 1.2, VDOP 1.1의 GDOP 편차에 대응하는 항법 정밀도에 대하여 회전타원체 및 ECEF 좌표계를 기준하여 분석하였다. 본 연구에서 얻은 항법 파라미터의 정보들은 향후 다국적 및 다중위성항법에 대한 종합분석에 활용될 것으로 예상한다.

• 한국공간정보시스템학회 논문지
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• 제3권1호
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• pp.37-48
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• 2001

지능형 교통 시스템(ITS)은 여행자에게 출발 전 또는 출발 후 도움이 되는 서비스와 유용한 데이터를 제공하는 여행자정보고급화 시스템을 포함하고 있다. 이 시스템은 출발전교통정보 안내 서브시스템, 운전중 교통정보제공 서브시스템, 동적주행안내 서브시스템들로 구성되어 있다. 여행자정보고급화 시스템은 표준화 작업을 총괄하는 기준 프레임워크인 국가 아키텍쳐에 따라 설계될 필요가 있다. 최근 소프트웨어 기술이 급속히 개선되고 안정화됨에 따라 미리 개발된 강력한 ITS 기술도 재사용 할 필요성이 있다. 컴포넌트와 개방형 인터페이스에 기반한 ITS 표준화는 현재 ITS 기술의 재사용성 문제를 해결하는 방법이 된다. 본 논문은 UML을 이용하여 컴포넌트에 기반한 여행자정보고급화 시스템을 설계한 결과를 제시하고 있으며 이 UML 방법은 새로 개발되는 ITS 컴포넌트를 위한 표준화된 모델을 제공할 것으로 기대된다.

• 한국전산구조공학회논문집
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• 제31권3호
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• pp.141-145
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• 2018

본 논문에서는 이단계 칼만필터를 활용한 구조물의 3 자유도 동적변위 계측 시스템을 소개한다. 개발 시스템은 센서 모듈, 베이스 모듈, 컴퓨테이션 모듈로 구성되어 있다. 센서 모듈은 100Hz 샘플주파수의 고정밀 가속도를 계측하는 포스피드백 가속도계와 10Hz의 샘플주파수의 저정밀도의 속도, 변위를 계측하는 저가의 RTK-GNSS로 구성되어 있다. 계측된 데이터는 LAN 케이블을 통하여 컴퓨테이션 모듈로 전송되고, 컴퓨테이션 모듈에서 이단계 칼만필터를 활용하여 100Hz 샘플주파수의 고정밀 변위를 실시간으로 산정한다. 개발 시스템의 변위 계측 정밀도를 검증하기 위해 미국, 캘리포니아에 위치한 San Francisco-Oaklmand Bay bridge 에서 현장 실험을 수행하였으며, 실험 결과 1.68mm RMS 오차를 보임을 확인하였다.

• 한국측량학회지
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• 제35권1호
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• pp.55-62
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• 2017

The SRP (Solar Radiation Pressure) model has always been an issue in the dynamic GPS (Global Positioning System) orbit determination. The widely used CODE (Center for Orbit Determination in Europe) model and its variants have nine parameters to estimate the solar radiation pressure from the Sun and to absorb the remaining forces. However, these parameters show a very high correlation with each other and, therefore, only several of them are estimated at most of the IGS (International GNSS Service) analysis centers. In this study, we attempted to numerically verify the correlation between the parameters. For this purpose, a bi-directional, multi-step numerical integrator was developed. The correlation between the SRP parameters was analyzed in terms of post-fit residuals of the orbit. The integrated orbit was fitted to the IGS final orbit as external observations. On top of the parametric analysis of the SRP parameters, we also verified the capabilities of orbit prediction at later time epochs. As a secondary criterion for orbit quality, the positional discontinuity of the daily arcs was also analyzed. The resulting post-fit RMSE (Root-Mean-Squared Error) shows a level of 4.8 mm on average and there is no significant difference between block types. Since the once-per-revolution parameters in the Y-axis are highly correlated with those in the B-axis, the periodic terms in the D- and Y-axis are constrained to zero in order to resolve the correlations. The 6-hr predicted orbit based on the previous day yields about 3 cm or less compared to the IGS final orbit for a week, and reaches up to 6 cm for 24 hours (except for one day). The mean positional discontinuity at the boundary of two 1-day arcs is on the level of 1.4 cm for all non-eclipsing satellites. The developed orbit integrator shows a high performance in statistics of RMSE and positional discontinuity, as well as the separations of the dynamic parameters. In further research, additional verification of the reference frame for the estimated orbit using SLR is necessary to confirm the consistency of the orbit frames.