• 제목/요약/키워드: International GNSS service

검색결과 73건 처리시간 0.027초

IGS 정밀궤도력을 이용한 SBAS 위성궤도 및 시계보정정보의 정확도 분석 (Accuracy Analysis of SBAS Satellite Orbit and Clock Corrections using IGS Precise Ephemeris)

  • 정명숙;김정래
    • 한국항행학회논문지
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    • 제13권2호
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    • pp.178-186
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    • 2009
  • SBAS(Satellite Based Augmentation System) 시스템에서는 GNSS 사용자들의 위치 정확도 향상을 위해 위성궤도 및 시계보정정보를 제공하고 있는데, 본 논문에서는 이러한 보정정보의 정확도에 대해 분석하였다. IGS(International GNSS Service)에서 제공하는 GPS 위성의 정밀궤도력을 참값으로 가정하고, 그에 대한 오차를 이용하여 정확도를 분석/수행하였다. 이때 IGS 정밀궤도력과의 정확한 비교를 위해 GPS 위성에 대한 안테나 위상중심 편차와 P1-C1 편이를 고려하였다. SBAS 위성궤도 및 시계보정 정보로는 미국의 WAAS와 일본의 MSAS 보정정보를 이용하였다. 정확도 분석을 통해 SBAS에서 제공하는 위성궤도 보정정보와 위성시계 보정정보가 상당한 상관관계를 가지고 있음을 확인하였다. 또한 보정정보의 정확도는 SBAS 시스템의 지상 네트워크 크기와 위성의 궤적에 영향을 받는 것을 확인하였다.

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저가형 측위장치에 RTS 보정정보의 실시간 LSTM 예측 기능 구현을 통한 PPP (Real-time LSTM Prediction of RTS Correction for PPP by a Low-cost Positioning Device)

  • 김범수;김민규;김정래;부성춘;이철수
    • 한국항행학회논문지
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    • 제26권2호
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    • pp.119-124
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    • 2022
  • IGS (international gnss service)에서는 GNSS (global navigation satellite system) 위성의 항법메시지에 적용할 수 있는 RTS (real-time service) 궤도 및 시계 보정정보를 제공한다. 하지만, 인터넷 단절이 발생하면 RTS 값을 수신할 수 없으므로, 안정적인 PPP (precise point positioning)를 수행하기 위해 신호 단절이 발생한 경우 RTS 보정정보를 예측해서 사용해야 한다. 본 논문에서는 실시간으로 신호 단절 구간에서 LSTM (long short-term memory) 알고리듬으로 궤도 및 시계 보정정보를 예측하여 PPP를 진행하였다. 연산 처리 속도가 빠르지 않은 Raspberry Pi (RPI)에 LSTM 알고리듬을 구현하여 예측성능을 분석하였다. 다항식 예측기법과 비교하여 LSTM은 장기간 예측에서 우수한 성능을 보였다.

Correction of Time and Coordinate Systems for Interoperability of Multi-GNSS

  • Kim, Lawoo;Lee, Yu Dam;Lee, Hyung Keun
    • 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.

Validation of GNSS TEC from NMSC GNSS Processing System

  • Lee, Jeong-Deok;Oh, Seung-Jun;Kil, Hyo-Sub;Shin, Dae-Yun
    • 천문학회보
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    • 제36권2호
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    • pp.101.1-101.1
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    • 2011
  • National Meteorological Satellite Center(NMSC) of Korea Meteorological Administration(KMA) is collecting GNSS data in near-real time for about 80 GNSS stations operated by multiple agencies. (eg. National Geographic Information Institute (NGII), Korea Astronomy and Space Science Institute (KASI), DGNSS Central Office) Using these GNSS data, NMSC developed automatic Total Electron Contents(TEC) derivation system over the Korean peninsular every 1-hour based on single station data processing. We present the TEC result and validation of TEC using International GNSS Service(IGS) global TEC data for the case of quiet time and storm time. The future plans for the system improvement will be discussed.

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Accuracy Evaluation of KASS Augmented Navigation by Utilizing Commercial Receivers

  • Sung-Hyun Park;Yong-Hui Park;Jin-Ho Jeong;Jin-Mo Park
    • Journal of Positioning, Navigation, and Timing
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    • 제12권4호
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    • pp.349-358
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    • 2023
  • The Satellite-Based Augmentation System (SBAS) plays a significant role in the fields of aviation and navigation: it corrects signal errors of the Global Navigation Satellite System (GNSS) and provides integrity information to facilitate precise positioning. These SBAS systems have been adopted as international standards by the International Civil Aviation Organization (ICAO). In recent SBAS system design, the Minimum Operational Performance Standards (MOPS) defined by the Radio Technical Commission for Aeronautics (RTCA) must be followed. In October 2014, South Korea embarked on the development of a Korean GPS precision position correction system, referred to as Korea Augmentation Satellite System (KASS). The goal is to achieve APV-1 Standard of Service Level (SoL) service level and acquisition of CAT-1 test operating technology. The first satellite of KASS, KASS Prototype 1, was successfully launched from the Guiana Space Centre in South America on June 23, 2020. In December 2022 and June 2023, the first and second service signals of KASS were broadcasted, and full-scale KASS correction signal broadcasting is scheduled to start at the end of 2023. The aim of this study is to analyze the precision of both the GNSS system and KASS system by comparing them. KASS is also compared with Japan's Multi-functional Satellite Augmentation System (MSAS), which is available in Korea. The final objective of this work is to validate the usefulness of KASS correction navigation in the South Korean operational environment.

QZSS-CLAS의 Compact SSR을 이용한 다중 위성항법 기반의 Code-PPP 개발 (Development of Code-PPP Based on Multi-GNSS Using Compact SSR of QZSS-CLAS)

  • 이해창;박관동
    • 한국측량학회지
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    • 제38권6호
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    • pp.521-531
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    • 2020
  • QZSS (Quasi-Zenith Satellite System)는 위성의 L6 밴드를 통해서 CLAS (Centimeter Level Augmentation Service)를 제공한다. CLAS는 현재 GPS (Global Positioing System), Galileo 그리고, QZSS 위성군에 대한 보정정보를 제공하며, 이러한 보정정보를 C-SSR (Compact - Space State Representation)라고 한다. 본 연구에서는 L6 밴드를 수신할 수 있는 GPS 수신기인 Septentrio의 AsteRx4를 이용하여 CLAS 메시지를 수신하고, 그 메시지를 디코딩하여 C-SSR을 획득하였다. 그리고, GPS, Galileo, QZSS의 코드의사거리 관측치에 Compact SSR을 적용하여 GNSS (Global Navigation Satellite System) 오차를 보정하고, 비선형 최소제곱법으로 수신기의 3차원 위치 및 위성군의 시계오차들을 추정하는 다중 위성항법 기반의 Code-PPP (Precise Point Positioning)를 개발하였다. 개발한 알고리즘의 정확도를 평가하기 위해서 IGS (International GNSS Service) 사이트 중 하나인 TSK2 (Tsukuba)를 대상으로 정지측위를 수행하고, 일본의 가와니시(Kawanishi)시의 이나강(Ina river) 주변을 주행하며 이동측위를 수행하였다. 그 결과, 정지측위의 경우 모든 데이터셋의 평균 RMSE (Root Mean Squared Error)는 수평방향으로 0.35 m, 수직방향으로 0.57 m의 정확도를 나타냈다. 그리고 이동측위의 경우 VRS의 RTK-FIX 값과 비교해 봤을 때 수평방향은 약 0.82 m, 수직방향은 약 3.56 m의 정확도를 나타냈다.

외삽기법을 이용한 전리층 보정정보 영역 확장 (Extending Ionospheric Correction Coverage Area by using Extrapolation Methods)

  • 김정래;김민규
    • 한국항공운항학회지
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    • 제22권3호
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    • pp.74-81
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    • 2014
  • The coverage area of GNSS regional ionospheric correction model is mainly determined by the disribution of GNSS ground monitoring stations. Outside the coverage area, GNSS users may receive ionospheric correction signals but the correction does not contain valid correction information. Extrapolation of the correction information can extend the coverage area to some extent. Three interpolation methods, Kriging, biharmonic spline and cubic spline, are tested to evaluate the extrapolation accuracy of the ionospheric delay corrections outside the correction coverage area. IGS (International GNSS Service) ionosphere map data is used to simulate the corrections and to compute the extrapolation error statistics. Among the three methods, biharmonic method yields the best accuracy. The estimation error has a high value during Spring and Fall. The error has a high value in South and East sides and has a low value in North side.

KASI 연구원 인터뷰-한국천문연구원 선임연구부장 박필호 박사

  • 한국천문연구원
    • KASI NEWSLETTER
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    • 통권55호
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    • pp.14-15
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    • 2006
  • 지난 해 한국천문연구원은 세계 4번째,아시아에서는 첫 번째로 IGS(International GNSS Service)국제 글로벌 테이터 센터(Global Data center)를 유치하였다.이번 사업을 진두 지휘한 이는 1989년부터 GPS와 동고동락한 박필호박사이다.

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Generation of Klobuchar Ionospheric Error Model Coefficients Using Fourier Series and Accuracy Analysis

  • Lee, Chang-Moon;Park, Kwan-Dong
    • Journal of Astronomy and Space Sciences
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    • 제28권1호
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    • pp.71-77
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    • 2011
  • Ionospheric error modeling is necessary to create reliable global navigation satellite system (GNSS) signals using a GNSS simulator. In this paper we developed algorithms to generate Klobuchar coefficients ${\alpha}_n$, ${\beta}_n$ (n = 1, 2, 3, 4) for a GNSS simulator and verified accuracy of the algorithm. The eight Klobuchar coefficients were extracted from three years of global positioning system broadcast (BRDC) messages provided by International GNSS service from 2006 through 2008 and were fitted with Fourier series. The generated coefficients from our developed algorithms are referred to as Fourier Klobuchar model (FOKM) coefficients, while those coefficients from BRDC massages are named as BRDC coefficients. The correlation coefficient values between FOKM and BRDC were higher than 0.97. We estimated total electron content using the Klobuchar model with FOKM coefficients and compared the result with that from the BRDC model. As a result, the maximum root mean square was 1.6 total electron content unit.

State of the Art on Terrestrial Radionavigation System and Its Applications for Maritime PNT Service

  • Seo, Kiyeol;Fang, Tae Hyun;Park, Sang Hyun
    • Journal of Positioning, Navigation, and Timing
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    • 제11권4호
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    • pp.229-238
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    • 2022
  • This paper addresses on the International technical trends, standards, and development status of terrestrial radionavigation system to provide more accurate and fail-safe Positioning, Navigation, and Timing (PNT) Information available in maritime navigation environment. We analyze the performance result of pilot service in enhanced Long range navigation (eLoran) testbed environment using Low Frequency (LF) signal, and describe the development status of Ranging-Mode (R-Mode) system using Medium Frequency (MF) and Very High Frequency (VHF) to meet the Harbor Entrances and Approaches (HEA) requirement of International Maritime Organization (IMO) within 10m position accuracy. Furthermore, we present an architecture for integrated service of satellite-terrestrial navigation system and future maritime applicable fields. As the core information infrastructure of future navigation for 4th industrial revolution, this paper will be contributed to determining the direction of present and future to provide fail-safe PNT service with Global Navigation Satellite System (GNSS) based on the technical enhancement of terrestrial integrated navigation system.