• 한국항행학회논문지
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• 제15권6호
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• pp.953-961
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• 2011

IGS(Internation GNSS Service) 초신속궤도력에 포함된 예측궤도력은 실시간 혹은 준실시간 정밀 항법에 적합한 궤도력이다. 이 논문에서는 예측궤도력에서 발생할 수 있는 궤도 이상 발생 현황을 점검하고, NANU(Current Notice Advisories to NAVSTAR Users)와 IGS 방송궤도력(BRDC, Broadcast Ephemerides)를 이용하여 예측궤도력의 이상 검출 성능을 분석하였다. 그 결과 예측궤도력은 2010년 1년간 93회의 궤도 이상이 나타났으며, NANU를 이용할 경우 88%, NANU와 BRDC를 함께 사용할 경우 95%의 이상 검출이 가능함을 확인할 수 있었다.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
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• pp.267-270
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• 2006

The International GNSS Service (IGS) has managed the global GNSS network and provided the highest quality GNSS data and products, which are GPS ephemerides, clock information and Earth orientation parameter, as the standard for GNSS. An important part of its works is to provide the precise orbits of GPS satellites. GPS satellites send their orbit information (broadcast ephemerides) to users and their accuracies are approximately 1.6 meters level, but those accuracies are not sufficient for the high precise applications which require millimeters precision. The current accuracies of the IGS final orbits are within 5 centimeters level and they are used for Earth science, meteorology, space science, and they are made by the IGS analysis centers and combined by the IGS analysis center coordinator. The techniques making the products are very difficult and require the high technology. The Korea Astronomy and Space Science Institute (KASI) studies to make the IGS products. In this study, we developed our own processing strategy and made GPS ephemerides using Bernese GPS software Ver. 5.0. We used the broadcast ephemerides as the initial orbits and processed the globally distributed 150 IGS stations. The result shows about 6 to 8 centimeters in root-mean-squares related to IGS final orbits in each day during a week. We expect that this study can contribute to secure our own high technology.

• Journal of Positioning, Navigation, and Timing
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• 제10권4호
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• pp.279-289
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• 2021

GNSS receivers capable of tracking multiple Global Navigation Systems (GNSSs) simultaneously are widely used. In order to estimate accurate user position and velocity, it is necessary to consider the key elements that contribute to the interoperability of the different GNSSs. Typical examples are the time system and the coordinate system. Each GNSS is operated based on its own reference time system depending on when the system was developed and whether the leap seconds are applied. In addition, each GNSS is designed based on its own coordinate system based on earth model constant values. This paper addresses the interoperability issues from the viewpoint of Single Point Positioning (SPP) users utilizing multiple GNSS signals from GPS, GLONASS, BeiDou, and Galileo. Since the broadcast ephemerides of each GNSS are based on their own time and coordinate systems, the time and the coordinate systems should be unified for any user algorithm. For this purpose, this paper proposes a method of converting each GNSS coordinate system into the reference coordinate system through Helmert transformation. The error of the broadcast ephemerides was calculated with the precise ephemerides provided by the International GNSS Service (IGS). The effectiveness of the proposed multi-GNSS correction and transformation method is verified using the Multi-GNSS Experiment (MGEX) station data.

• 한국측량학회지
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• 제22권4호
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• pp.383-390
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• 2004

IGS는 13일 이후에 제공되는 매우 정확한 최종정밀궤도력을 제공하고 있으며, 보다 신속한 활용을 위해 신속정밀궤도력을 제공하고 있다. 그리고 실시간 활용을 위해 초신속정밀궤도력을 제공하고 있다. 본 연구에서는 최종정밀궤도력을 기준으로 신속정밀궤도력과 초신속정밀궤도력의 정확도를 분석하고, 위성의 위치결정에 필요한 Lagrange 보간법의 차수를 결정하고자 한다. 연구결과, 신속정밀궤도력의 x,y,z좌표의 평균제곱근오차는 $\pm$0.016m 정도였으며, 관측된 초신속정밀궤도력은 약 $\pm$0.024m의 오차를 나타내었다. 24시간동안의 예측 초신속정밀궤도력은 $\pm$0.07m, 6시간동안 예측된 초신속정밀궤도력은 $\pm$0.04m 정도의 오차를 나타내어 방송궤도력보다 매우 높은 정확도를 갖고 있음을 알 수 있었다. 또한, Lagrange 방법으로 위성의 위치를 계산하는 경우, 9차 다항식을 이용하는 것이 효율적임을 확인하였다.