• Journal of Positioning, Navigation, and Timing
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• 제12권3호
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• pp.215-228
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• 2023

The State Space Representation (SSR) method provides individual corrections for each Global Navigation Satellite System (GNSS) error components. This method can lead to less bandwidth for transmission and allows selective use of each correction. Precise Point Positioning (PPP) - Real-Time Kinematic (RTK) is one of the carrier-based precise positioning techniques using SSR correction. This technique enables high-precision positioning with a fast convergence time by providing atmospheric correction as well as satellite orbit and clock correction. Currently, the positioning service that supports PPP-RTK technology is the Quazi-Zenith Satellite System Centimeter Level Augmentation System (QZSS CLAS) in Japan. A system that provides correction for each GNSS error component, such as QZSS CLAS, requires monitoring of each error component to provide reliable correction and integrity information to the user. In this study, we conducted an analysis of the performance of residual error bounding for each error component. To assess this performance, we utilized the correction and quality indicators provided by QZSS CLAS. Performance analyses included the range domain, dispersive part, non-dispersive part, and satellite orbit/clock part. The residual root mean square (RMS) of CLAS correction for the range domain approximated 0.0369 m, and the residual RMS for both dispersive and non-dispersive components is around 0.0363 m. It has also been confirmed that the residual errors are properly bounded by the integrity parameters. However, the satellite orbit and clock part have a larger residual of about 0.6508 m, and it was confirmed that this residual was not bounded by the integrity parameters. Users who rely solely on satellite orbit and clock correction, particularly maritime users, thus should exercise caution when utilizing QZSS CLAS.

• 한국지역지리학회지
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• 제17권4호
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• pp.432-442
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• 2011

기온, 강수와 같은 기후관측 자료들은 공간과 더불어 시간적인 변이를 동시에 나타낸다. 따라서 신뢰성 높은 시계열 분포도 작성을 위해 공간적 자기상관성만을 고려하는 기존 공간 내삽 기법에 시공간적 자기상관성 정보를 반영할 필요가 있다. 이 연구에서는 시계열 기온 분포도 제작을 위해 1개월 동안 1시간 간격으로 획득된 기온 관측소 자료를 대상으로 시공간 크리깅을 적용하였다. 우선 기온자료를 결정론적 경향 성분과 확률론적 잔차 성분으로 분해한 후에, 경향 성분 모델링 과정에 기온과 연관성이 높은 고도 자료를 부가 자료로 통합하여 지형 효과를 반영하는 경향 성분을 모델링하였다. 잔차 성분에 대한 시공간 베리오그램 모델링에는 곱-합 모델을 적용하여 시간과 공간 베리오그램의 상호 연관성을 반영하도록 하였다. 이러한 시공간 베리오그램 모델을 이용하여 시공간 정규 크리깅을 적용한 결과, 기존 공간적 자기상관성만을 고려하는 정규 크리깅과 고도 자료를 부가 자료로 이용하는 회귀분석 크리깅에 비해 상대적으로 높은 예측 능력을 보였다. 이러한 결과는 고도 자료와 더불어 시공간 자기상관성 정보의 이용이 중요함을 지시한다. 따라서 공간적으로 가용할 수 있는 자료의 수가 한계가 있지만 시계열적으로 자료 획득이 가능한 변수를 분석할 때, 시공간 크리깅이 유용한 내삽 방법론으로 적용될 수 있을 것으로 기대된다.

• 상하수도학회지
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• 제20권1호
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• pp.86-93
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• 2006

In the drinking water treatment, the aesthetic and color problem are caused by the manganese which is occurring and present in the surface, lake and ground water. The most common treatment processes for removing manganese are known for oxidation followed by filtration. In this study, the manganese sand process was used for removing manganese with river bank filtrate as a source. In the manganese sand process, the residual chlorine and pH are important factors on the continuous manganese oxidation. In addition, space velocity (SV) and alum dosage are play a role of manganese removal. Even though manganese removal increased with increasing chlorine concentration, the control of residual chlorine is actually difficult in this process As the results of tests, the residual chlorine concentration as well as manganese removal were effectively achieved at pH 7.5. The optimum attached manganese concentration on manganese sand was confirmed to 0.3mg/L by the experimental result of a typical sand converting to manganese sand.

• 한국안전학회지
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• 제20권1호
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• pp.75-80
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• 2005

In this paper, when CF/EPOXY laminates for high efficiency space structure are subjected to FOD(Foreign Object Damage), the effects of temperature change on the impact damages(inter laminar separation and transverse crack) of CF/EPOXY laminates and the relationship between residual life and impact damages ale experimentally investigated. Composite laminates used in this experiment are CF/EPOXY orthotropic laminated plates, which have two-interfaces $[0^{\circ}_6/90^{\circ}_6]S$ and four-interfaces $[0^{\circ}_3/90^{\circ}_6/0^{\circ}_3]S$. CF/EPOXY specimens with impact damages caused by a steel ball launched from the air gun were observed by the scanning acoustic microscope under room and high temperatures. In this experimental results, various relations were experimentally observed including the delamination area vs. temperature change, the bending strength vs. impact energy and the residual bending strength vs. impact damage of CF/EPOXY laminates. And as the temperature of CF/PEEK laminates increases, the delaminaion areas of impact-induced damages decrease linearly. A linear relationship between the impact energy and the delamination areas were observed. As the temperature of CF/PEEK laminates increases, the delamination areas decrease because of higher initial delaminatin damage energy.

• 대한수학회보
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• 제42권3호
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• pp.631-638
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• 2005

we prove that, given any compact metric space X, there exists a residual subset R of H(X), the space of all homeomorphisms on X, such that if $\in$ R has a totally chain-transitive attractor A, then any g sufficiently close to f has a totally chain transitive attractor A$\_{g}$ which is convergent to A in the Hausdorff topology.

• 한국항공우주학회지
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• 제32권2호
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• pp.47-55
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• 2004

• 한국항공우주학회지
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• 제31권7호
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• pp.53-62
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• 2003

• 한국전산구조공학회:학술대회논문집
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• 한국전산구조공학회 2003년도 봄 학술발표회 논문집
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• pp.45-52
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• 2003

A finite element procedure to estimate ultimate strength of space frames considering spread of plasticity is presented. The improved displacement field is introduced based on inclusion of second order terms of finite rotations. All the nonlinear terms due to bending and torsional moment as well as axial force are precisely considered. The concept of plastic hinge is introduced and the incremental load/displacement method is applied for the elasto-plastic analysis. The initial yield surface is defined based on the residual stress and the full plastification surface is considered under the combined action of axial force, bending and torsional moments. The elasto-plastic stiffness matrices are derived using the flow rule and the normality condition of the limit function. Finite element solutions for ultimate strength of space frames are compared with available solutions and experimental results.

• 한국항공우주학회지
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• 제43권1호
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• pp.62-71
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• 2015

정지궤도위성은 궤도상에서 위치변화를 제어하기 위해 추력기를 사용하고 운용수명에 맞추어 적정한 양의 액체추진제를 탑재한다. 그러므로 정지궤도위성의 수명은 추진제 잔여량에 좌우되고 정확한 잔여추진제량 측정은 조기 수명종료로 야기되는 경제적 손실을 완화시킬 뿐만 아니라 후속위성의 대체나 위성망 운용계획 등에 매우 중요하다. 잔여추진제량을 측정하는 방법은 주로 PVT 방법, 열질량법, 회계식 방법이 사용된다. 본 논문에서는 회계식방법을 사용하기 위한 천리안위성 이원추진시스템의 모델링과 몬테카를로 방법을 이용하여 천리안위성의 궤도전이 소요 추진제량을 분석하였다.