• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.1
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• pp.191-196
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• 2006

In GPS Positioning, the error of satellite orbit will affect user's position accuracy directly, it is important to determine the satellite orbit precise. The real-time orbit is needed in kinematic GPS positioning, the precise GPS orbit from IGS would be delayed long time, so orbit prediction is key to real-time kinematic positioning. We analyze the GPS predicted ephemeris, on the base of comparison of EKF and UKF, a new orbit prediction method is put forward based on UKF in this paper, the result shows that UKF improves the orbit predicted precision and stability. It offers a new method for others satellites orbit determination as Galileo, and so on.

• ETRI Journal
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• 제30권1호
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• pp.59-67
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• 2008

The necessity for the precise time synchronization of measurement data from multiple sensors is widely recognized in the field of global positioning system/inertial navigation system (GPS/INS) integration. Having precise time synchronization is critical for achieving high data fusion performance. The limitations and advantages of various time synchronization scenarios and existing solutions are investigated in this paper. A criterion for evaluating synchronization accuracy requirements is derived on the basis of a comparison of the Kalman filter innovation series and the platform dynamics. An innovative time synchronization solution using a counter and two latching registers is proposed. The proposed solution has been implemented with off-the-shelf components and tested. The resolution and accuracy analysis shows that the proposed solution can achieve a time synchronization accuracy of 0.1 ms if INS can provide a hard-wired timing signal. A synchronization accuracy of 2 ms was achieved when the test system was used to synchronize a low-grade micro-electromechanical inertial measurement unit (IMU), which has only an RS-232 data output interface.

• 한국정보통신학회논문지
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• 제19권5호
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• pp.1055-1062
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• 2015

본 논문에서는 GPS 위치 정보를 이용한 파고계측시스템을 제안한다. 제안한 시스템은 이중주파수 측정치 및 GPS 정밀위성정보를 이용하여 위치를 추정하는 PPP 기반 항법 알고리즘을 사용한다. 이를 이용하여 기준국으로부터 보정정보를 받는 RTK나 DGPS 기반 파고계와 달리 기준국과의 거리에 관계없이 높은 정확도로 위치 추정이 가능하다. 그리고 GPS 단독으로 운용되는 간단한 시스템이므로, 가속도계 기반 파고 계측 시스템처럼 다른 센서를 이용하여 누적되는 위치 오차를 보정할 필요가 없다. 제안한 파고계측시스템을 테스트하기 위하여 경북 울진 죽변항 인근 해역에 제안한 시스템과 기상청에서 활용하는 상용 파고계를 탑재한 부표를 설치하고, 시험 운용하였다. 그리고 부표로부터 전송된 두 가지 파고 데이터를 상호 비교함으로써 제안한 시스템의 성능을 평가하였다.

• Korean Journal of Geomatics
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• 제2권1호
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• pp.65-73
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• 2002

GPS in the United States and GLONASS of the old Soviet Union are used currently as satellite navigation systems. Plans are being made to use the Galileo satellite system in Europe, and these plans focus on a combined application of the satellite navigation systems. In this study, we examined the possibility of effective application of a combination of GPS/GLONASS in urban areas, where 3-dimensional positioning is impossible with GPS alone. We analyzed the 3-D coordinate deviation of a GLONASS satellite by integration interval and compared it with GLONASS satellite coordinates in precise ephmerides by transforming it into WGS84. We also programmed GPS/GLONASS, analyzed 3-D positioning accuracy by static surveying and kinematic surveying with Ashtech Z18 receivers and Legacy receivers, and then compared the results to those of GPS surveying. As a result, we are able to decide the integration interval for producing GLONASS satellite coordinates in navigation and geographical information and construct a GPS/GLONASS data processing system by developing a DGPS/DGLONASS positioning program. If more than four GLONASS satellites are observed, the accuracy of GPS/GLONASS is better than that of GPS positioning. As a result of kinematic surveying in a congested urban area with skyscrapers, we discovered that the GPS/LONASS combination is very effective.

• Journal of Astronomy and Space Sciences
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• 제14권2호
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• pp.375-380
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• 1997

GPS(Global Positioning System)에 있어서 궤도의 정밀도는 응용분야의 결과에 영향을 미치는 매우 중요한 파라미터이다. 따라서 GPS 사용자가 얻는 자료의 정밀도는 기준으로 삼고 있는 위성의 위치 자료를 얼마만큼 신뢰할 수 있느냐에 달려 있는데 이들 위성의 위치 자료는 실시간으로 제공되는 항법메세지에 포함된 방송궤도력에 의존할 경우 실제위치와 약 3~10m의 차이가 난다. 그러나 GPS를 이용하여 100km의 기선거리를 수mm의 오차로 측정하기 위해서는 방송궤도력보다 실제 궤도에 매우 가까운 정밀 궤도력을 사용하여야 하는데 이 정밀 궤도력은 오차가 수cm정도로서 현재 이러한 수준의 정밀 궤도력을 계산할 수 있는 능력을 보유한 곳은 전 세계 약 7개 기관이다. 이번 연구에서는 정밀 궤도 결정에 필요한 궤도 모델링과 위상자료 처리 방법을 연구하였고, 직접 전세계 28개 관측소로부터 관측된 위상 관측 자료들을 최소자추정(Least Square Estimation) 하여 국제 GPS 관측망에서 발표하는 궤도자료에 비길 수 있는 정밀 궤도력을 산출하였다.

• 대한공간정보학회지
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• 제22권1호
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• pp.47-54
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• 2014

휴대용 단말에 간편하게 구현 가능하도록 GPS의 코드의사거리 관측치 기반의 정밀단독측위(PPP; Precise Point Positioning) 알고리즘을 개발하고 그 성능을 검증하였다. PPP에 필요한 기본 모델로 그룹 딜레이, 상대성 효과, 위성안테나 위상중심오프셋 보정모델을 적용하였다. 위성 궤도와 시계오차는 IGS(International GNSS Service) 공식 산출물에 최적의 알고리즘을 통해 보간하고, 대류권과 전리층 오차는 각각 과학기술용 GPS 자료처리 소프트웨어로 산출한 참값과 GIM(Global Ionosphere Model)을 사상함수를 적용해 시선방향 오차로 변환해 적용하였다. 개발된 알고리즘을 4일간 테스트한 결과 수평오차는 0.8~1.6m, 수직오차는 1.6~2.2m 수준으로 나타났다. 이는 DGPS 측위결과와 유사한 성능으로 향후 PPP 알고리즘의 추가개선이 이루어질 경우 다양한 측량 및 위치기반서비스 분야에 활용 가능할 것으로 기대된다.

• 한국정보통신학회논문지
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• 제22권6호
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• pp.910-915
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• 2018

미국의 GPS, 러시아의 GLONASS, 유럽의 Galileo, 중국의 Beidou 등과 같은 GNSS(Global Navigation Satellite System)의 핵심요소인 정밀 시각은 전 세계에서 다양한 경제적 활동의 중요한 근간이 되어 있다. 통신시스템, 전력 그리드, 금융 네트워크 등은 기본적인 작동 원리의 근간뿐만 아니라 작업들 간의 동기와 운영적 효율을 위해 정밀 시각을 기반으로 동작한다. 본 논문에서는 GNSS 신호 관측을 통해 클럭의 오류(클럭 솔루션)를 계산하는 방법인 정밀 절대측위 기법을 구현한 벨기에의 아토미움을 국내에서 처음으로 소개하고 한국표준과학연구원 관측 데이터를 적용하여 클럭 솔루션을 추출한 결과를 제시한다.

• 한국위성정보통신학회논문지
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• 제8권2호
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• pp.22-28
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• 2013

In this paper, new LBS (location based service) are proposed using conventional DMB (digital multimedia/mobile broadcasting) system. LBS applications are proposed that can be suitable for the subway and ground transportation based on S-DMB (satellite-DMB) and T-DMB (terrestrial-DMB) respectively. In the shaded area such as subway, the broadcasting signal transmitted from the satellite of S-DMB system should be retransmitted by the earth repeater called the gap filler and each gap filler has its own identification value called the gap filler ID which introduces the area in which the gap filler was installed. Therefore, the LBS can be implemented by using the gap filler ID of S-DMB on the subway in which the GPS (global positioning system) can't be received. Unlike the LBS on the subway, the combination of T-DMB and DGPS (differential GPS) will be introduced as a way for ground transportation. Generally, DGPS has been designed to compensate the position value calculated from the GPS signal so that positioning error of about 1 meter can be obtained by using DGPS information. T-DMB system transmitting DGPS signal will be expected to be commercial in Korea and, if using DGPS information transmitted through T-DMB network, LBS with more precise positioning than GPS alone can be implemented in the ground vehicles.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2002년도 Proceedings of International Symposium on Remote Sensing
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• pp.751-756
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• 2002

Since the operation of the first satellite-based navigation services, satellite positioning has played an increasing role in both surveying and navigation, and has become an indispensable tool for precise relative positioning. However, in some situations, e.g. at a low angle of elevation, the use of satellites for navigation is seriously restricted because obstacles like buildings and mountains can block signals. As a mean to resolve this problem, the quasi-zenith satellite system has been proposed as a next-generation satellite navigation system. Quasi-zenith satellite is a system which simultaneously deploys several satellites in a quasi-zenith geostationary orbit so that one of the satellites always stay close to the zenith if viewed from a specific point on the ground of East Asia. Thus, if a position measurement function compatible with GPS is installed in the quasi-zenith and stationary satellites, and these satellites are utilized together with the GPS, four satellites can be accessed simultaneously nearly all day long and a substantial improvement in position measurement, especially in metropolitan areas, can be achieved. The purpose of this paper is to evaluate the effectiveness of quasi-zenith satellite system on positioning accuracy improvement through simulation by using precise orbital information of the satellites and a three-Dimensional digital map. Through this simulation system, it is possible to calculate the number of simultaneously visible satellites and available area of the positioning without the need of actual observation.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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• pp.87-90
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• 2005

The FORMOSAT-3/COSMIC mission is a micro satellite mission to deploy a constellation of six micro satellites at low Earth orbits. The final mission orbit is of an altitude of 750-800 lan. It is a collaborative Taiwan-USA science experiment. Each satellite consists of three science payloads in which the GPS occultation experiment (GOX) payload will collect the GPS signals for the studies of meteorology, climate, space weather, and geodesy. The GOX onboard FORMOSAT -3 is designed as a GPS receiver with 4 antennas. The fore and aft limb antennas are installed on the front and back sides, respectively, and as well as the two precise orbit determination (POD) antennas. The precise orbit information is needed for both the occultation inversion and geodetic research. However, the instrument associated errors, such as the antenna phase center offset and even the different cable delay due to the geometric configuration of fore- and aft-positions of the POD antennas produce error on the orbit. Thus, the focus of this study is to investigate the impact of POD antenna parameter on the determination of precise satellite orbit. Furthermore, the effect of the accuracy of the determined satellite orbit on the retrieved atmospheric and ionospheric parameters is also examined. The CHAMP data, the FORMOSAT-3 satellite and orbit parameters, the Bernese 5.0 software, and the occultation data processing system are used in this work. The results show that 8 cm error on the POD antenna phase center can result in ~8 cm bias on the determined orbit and subsequently cause 0.2 K deviation on the retrieved atmospheric temperature at altitudes above 10 lan.