• Journal of Positioning, Navigation, and Timing
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• 제12권2호
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• pp.113-119
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• 2023

Satellite navigation systems, with the exception of the GLObal NAvigation Satellite System (GLONASS), adopt ionosphere models and provide ionospheric coefficients to single-frequency users via navigation messages to correct ionospheric delay, the main source of positioning errors. A Global Navigation Satellite System (GNSS) mostly has its own ionospheric models: the Klobuchar model for Global Positioning System (GPS), the NeQuick-G model for Galileo, and the BeiDou Global Ionospheric delay correction Model (BDGIM) for BeiDou satellite navigation System (BDS)-3. On the other hand, a Regional Navigation Satellite System (RNSS) such as the Quasi-Zenith Satellite System (QZSS) and BDS-2 uses the Klobuchar Model rather than developing a new model. QZSS provides its own coefficients that are customized for its service area while BDS-2 slightly modifies the Klobuchar model to improve accuracy in the Asia-Pacific region. In addition, BDS broadcasts multiple ionospheric parameters depending on the satellites, unlike other systems. In this paper, we analyzed the different ionospheric models of GPS, QZSS, and BDS in Korea. The ionospheric models of QZSS and BDS-2, which are based in Asia, reduced error by at least 25.6% compared to GPS. However, QZSS was less accurate than GPS during geomagnetic storms or at low latitude. The accuracy of the models according to the BDS satellite orbit was also analyzed. The BDS-2 ionospheric model showed an error reduction of more than 5.9% when using GEO coefficients, while in BDS-3, the difference between satellites was within 0.01 m.

• 항공우주산업기술동향
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• 제8권2호
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• pp.46-53
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• 2010

이 논문에서는 위성항법시스템의 운영 현황과 개발 계획에 대하여 기술하였다. 미국의 GPS(Global Positioning System)와 러시아의 GLONASS(Global Navigation Satellite System), 유럽의 Galileo, 중국의 Beidou/Compsss, 그리고 일본의 QZSS(Quasi-Zenith Satellite System) 에 대하여 시스템의 구성과 운영 위성 상태에 대하여 기술하였으며, 각 시스템의 개발 계획과 현대화에 대하여 기술하였다.

• International Journal of Aeronautical and Space Sciences
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• 제6권1호
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• pp.61-70
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• 2005

The currently developed propulsion system(PS) is composed of propellant tank, valves, thrusters, interconnecting line assembly and thermal hardwares to prevent propellant freezing in the space environment. Comprehensive engineering analyses in the structure, thermal, flow and plume fields are performed to evaluate main design parameters and to verify their suitabilities concurrently at the design phase. The integrated PS has undergone a series of acceptance tests to verify workmanship, performance, and functionality prior to spacecraft level integration. After all the processes of assembly, integration and test are completed, the PS is integrated with the satellite bus system successfully. At present, the severe environmental tests have been carried out to evaluate functionality performances of satellite bus system. This paper summarizes an overall development process of monopropellant propulsion system for the attitude and orbit control of LEO(Low Earth Orbit) observation satellite from the design engineering up to the integration and test.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2004년도 한국우주과학회보 제13권2호
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• pp.351-355
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• 2004

A multibeam switching satellite system technology have started localized development to overcome the limitation of the frequency resource and geostationary orbit existing relay type satellite transponder and the required performance of the spot beam, and looked around the configuration and functions of the multibeam switching satellite communication system. This paper proposed that operation scheme and network control features for service definition, network architecture, transmission method of the natural disaster service network and public communication service network using this system.

• 한국정보처리학회논문지
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• 제7권3호
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• pp.901-908
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• 2000

Satellite communication in the 21 century's high tech information world is developing rapidly, marked by high levels of applications and functions. For example, satellite communication can process and switch the speed of the service provided by a broad and vast digital multimedia system such as a long-distance all between nations or broadcasting transfer service, which is supplied by a contemporary satellite system. So, it bring about problems which lack of satellite orbit and gibes out frequency resource by increment of satellite universally. To support this, an OBP satellite system is need, which includes an on-board IF/RF switch, baseband signal processing, multi-beam antenna technology, as well as a simple transponder system. In this paper, we have outlined the next generation of satellite communication; satellite OBP transport network architecture, which offers multimedia service and applied frequency reuse method for multi-spot beam. The satellite B-ISDN transport network architecture is also analyzed.

• 한국위성정보통신학회논문지
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• 제11권3호
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• pp.12-17
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• 2016

정지궤도 위성들을 이용하여 사용자들에게 GNSS (Global Navigation Satellite System) 정정 데이터 및 레인징 신호를 제공하는 SBAS (Satellite Based Augmentation System)는 국제민간항공기구에 의해 2025년까지 도입되도록 권고되고 있다. 본 논문에서는 현재 개발/구축 사업으로 진행중인 한국형 SBAS 시스템인 KASS (Korea Augmentation Satellite System)의 위성통신시스템 RF 링크를 기본 설계하여 그 결과를 제시한다. C 대역 상향링크와 Ku 대역 상향링크를 모두 고려하여 SBAS 시스템에 대한 국제 표준 요구사항을 만족하도록 RF 링크를 설계하였고, 각 주파수 대역에 따른 요구되는 위성통신국의 최소 EIRP 및 G/T 성능 규모를 파악하였다. 이러한 RF 링크 설계 분석 결과를 이용하여 KASS 위성통신시스템의 하위 시스템 규격 선정시 효과적인 설계가 될 수 있도록 활용할 예정이다.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2004년도 한국우주과학회보 제13권2호
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• pp.58-58
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• 2004

• 한국항행학회논문지
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• 제20권4호
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• pp.305-313
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• 2016

ICAO (International Civil Aviation Organization)는 GNSS (global navigation satellite system)를 이용하는 PBN (performance based navigation) 도입을 권고하였다. 우리나라도 PBN 로드맵을 수립하여 항공분야에서 GNSS를 이용할 수 있는 환경을 갖추려 시도하고 있으며, 2014년 10월 한국형 SBAS (satellite-based augmentation system) 개발을 위해 KASS (Korea augmentation satellite system) 사업을 본격적으로 착수하였다. 항공기가 GNSS를 이용하기 위해서는 수신기와 같은 항법장비를 탑재해야 한다. GNSS 항법장비는 항로, 이륙 도착, 접근 등 비행 단계에서 사용되기 때문에 장비의 규격은 다양하고 각각 별도로 그 기능과 성능을 규정하고 있다. 이 논문에서는 현재까지 제정된 항공용 GNSS 장비 표준안과 규정된 항법장비 및 인터페이스 규격에 대해 분석하여 정리하였다. KASS 개발 구축 시 비행시험 및 비행절차 개발 등 항공용 GNSS 탑재장비 등이 요구되는 곳에 활용성이 있을 것으로 기대한다.

• 한국위성정보통신학회논문지
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• 제3권2호
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• pp.32-37
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• 2008

Global Navigation Satellite System (GNSS) is been developing in many countries. The satellite navigation system has the importance in economic and military fields. For utilizing satellite navigation system properly, the technology of GNSS Ground Station is needed. GNSS Ground Station monitors the signal of navigation satellite and analyzes navigation solution. This study deals with the navigation software for GNSS Ground Station. This paper will introduce the navigation solution algorithm for GNSS Ground Station. The navigation solution can be calculated by the code-carrier smoothing method, the Kalman-filter method, the least-square method, and the weight least square method. The performance of each navigation algorithm in this paper is presented.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.31-33
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• 2003

Recently, KARI developed in-house meteorological sensor processing system named MESIS for GOES GVAR 5-CH Imager for better KOMPSAT EOC mission operation. MESIS consists of antenna system, receiver, serial telemetry card, processing and mapping software, and 2 NT PC systems. This paper shows system requirement, system design, characteristic and test results of processing system. System operation concept and sample image are also provided. Implemented system was proven to be fully operational through lots of operations covering from RF signal reception to web publishing.