• Journal of Advanced Navigation Technology
• /
• v.22 no.6
• /
• pp.610-615
• /
• 2018

Globally, global navigation satellite system (GNSS) is being developed and operated in advanced countries. China's Beidou is developing rapidly, starting with global positioning system (GPS), which is the most representative system. In this paper, we analyze the visibility of Beidou satellite in Korea at present time to utilize rapidly changing Beidou. In this analysis, it is compared with GPS which is stable service. The results of the visibility analysis are based on the results of the mask angle (the low elevation satellite exclusion angle) and the result of the skyplot (a visual representation of the position of the satellite at the user location). Visibility analysis shows that the high elevation angle of Beidou satellite is higher than that of GPS satellite in Korea. In addition, GPS and Beidou's availability and positioning accuracy analysis are performed to confirm the effect of increasing elevation angle satellites. According to the results, Beidou is more effective than GPS in using high elevation satellites in Korea.

• Proceedings of the Korean Society of Broadcast Engineers Conference
• /
• 2013.11a
• /
• pp.241-243
• /
• 2013

영상을 포함하여 다양한 방법으로 실내에서 위치를 확인하는 방법에 대한 연구가 진행되고 있다. 영상 기반의 측위 또한 여러 가지 방법이 있는데, 우리는 시스템 구축 비용이 많이 들지 않으면서도 많은 서비스에 활용 할 수 있는 영상 기반의 실용적 측위 시스템에 대한 연구를 하였다. 이 시스템은 실내에 미리 설치 된 간판이나 광고 등을 식별하고 이를 이용하여 실내에서 사용자의 위치를 구할 수 있다. 그러나, 영상 기반의 시스템이기 때문에 같은 영상이 서로 다른 참조 대상으로 등록 될 경우, 이것을 서로 구별 할 수 없다는 단점이 있다. 실내에서는 GPS 와 같은 위성 항법 신호 수신이 잘 되지 않기 때문에 GPS 를 위치를 확인하기 위한 목적으로 사용 할 수는 없다. 그러나, 특정 지점에서 수신되는 GPS 신호가 유사한 점을 이용하면, 서로 다른 위치에 설치 된 동일한 이미지의 참조 대상을 구별 할 수 있다. 이 방법은 추가적인 비용이 들지 않기 때문에, 영상 기반의 실용적 측위 시스템의 장점을 그대로 유지 하면서 측위 성능을 더 높 힐 수 있는 방법이다.

• Journal of Navigation and Port Research
• /
• v.38 no.4
• /
• pp.373-378
• /
• 2014

In order to prepare for recapitalization of differential GNSS (DGNSS) reference station and integrity monitor (RSIM) due to GNSS diversification, this paper focuses on differential correction algorithm using GPS/Galileo pesudorange. The technical standards on operation and broadcast of DGNSS RSIM are described as operation of differential GPS (DGPS) RSIM for conversion of DGNSS RSIM. Usually, in order to get the differential corrections of GNSS pesudorange, the system must know the real positions of satellites and user. Therefore, for calculating the position of Galileo satellites correctly, using the equation for calculating the SV position in Galileo ICD (Interface Control Document), it estimates the SV position based on Ephemeris data obtained from user receiver, and calculates the clock offset of satellite and user receiver, system time offset between GPS and Galileo, then determines the pseudorange corrections of GPS/Galileo. Based on a platform for performance verification connected with GPS/Galileo integrated signal simulator, it compared the PRC (pseudorange correction) errors of GPS and Galileo, analyzed the position errors of DGPS, DGalileo, and DGPS/DGalileo respectively. The proposed method was evaluated according to PRC errors and position accuracy at the simulation platform. When using the DGPS/DGalileo corrections, this paper could confirm that the results met the performance requirements of the RTCM.

• Korean Journal of Remote Sensing
• /
• v.39 no.6_2
• /
• pp.1529-1539
• /
• 2023

The data from Geostationary Ocean Color Imager-II (GOCI-II), which observes the color of the sea to monitor marine environments, undergoes various correction processes in the ground station system, producing data from Raw to Level-2 (L2). Quality issues arising at each processing stage accumulate step by step, leading to an amplification of errors in the satellite data. To address this, improvements were made to the GOCI-II ground station system to measure potential optical quality and geolocation accuracy errors in the Level-1A/B (L1A/B) data. A newly established Radiometric and Geometric Performance Assessment Module (RGPAM) now measures five optical quality factors and four geolocation accuracy factors in near real-time. Testing with GOCI-II data has shown that RGPAM's functions, including data processing, display and download of measurement results, work well. The performance metrics obtained through RGPAM are expected to serve as foundational data for real-time radiometric correction model enhancements, assessment of L1 data quality consistency, and the development of reprocessing strategies to address identified issues related to the GOCI-II detector's sensitivity degradation.

• Proceedings of the KIEE Conference
• /
• 2011.07a
• /
• pp.1254-1255
• /
• 2011

최근 무선통신기반 열차제어시스템의 국산화 개발이 진행 중에 있으며, 이동폐색 및 열차간격의 효율적인 제어를 위해서는 열차에 서 직접 열차의 이동위치와 속도를 정확하게 실시간으로 파악할 수 있어야 한다. 하지만 기존 철도시스템에서는 열차의 위치 및 속도확인을 위해 궤도회로와 타코메터를 이용하고 있으며, 효율적인 열차제어를 위해 지상설비의 도움없이 안전하고 정확한 열차위치정보의 확보가 필요하다. 따라서 본 논문에서는 위성항법수신기, 관성센서, 도플러레이더센서, 타코메터와 같이 열차에 탑재 가능한 위치 및 속도센서를 통합 적용하여 단독으로 열차 위치 및 속도파악이 가능한 차상기반 열차위치검지 장치를 구성하고, 한국형 틸팅열차 탑재시험을 통해 위치정확성을 평가하고 철도운영 환경에서의 적용성을 확인한다.

• Journal of Advanced Navigation Technology
• /
• v.13 no.2
• /
• pp.178-186
• /
• 2009

SBAS(Satellite Based Augmentation System) provides GNSS satellite orbit and clock corrections for positioning accuracy improvement of GNSS users. In this paper, the accuracy of SBAS satellite orbit and clock corrections were analyzed by comparing with the IGS(International GNSS Service) precise ephemeris. The GPS antenna phase center offsets and the P1-C1 bias are considered for the analysis. The correction data of the US WAAS and the Japanese MSAS were analyzed. The analysis results showed that the SBAS satellite orbit and clock corrections are highly correlated. The correction data accuracy depends on the SBAS ground network size and orbit trajectories.

• Journal of IKEEE
• /
• v.1 no.1 s.1
• /
• pp.19-30
• /
• 1997

In this paper we design the optimal satellite-tracking antenna $H{\infty}$ control system using genetic algorithms. To do this, we give gain and dynamics parameters to the weighting functions and apply genetic algorithms with reference model to the optimal determination of weighting functions and design parameter ${\gamma}$ that are given by Glover-Doyle algorithm which can design $H{\infty}$ controller in the state space. These weighting functions and design parameter ${\gamma}$ are optimized simultaneously in the search domain guaranteeing the robust stability of closed-loop system. The effectiveness of this satellite-tracking antenna $H{\infty}$ control system is verified by computer simulation.

• 정보화사회
• /
• s.179
• /
• pp.10-14
• /
• 2006

LBS가 기본적으로 이동통신 기지국과 위성위치확인시스템(GPS:Global Positioning System)을 통해 개인이나 차량의 위치 정보를 파악하고, 이를 기반으로 각종 첨단 서비스를 제공하다보니, 이통사의 핵심 서비스로 발전되고 있는 것은 틀림없다. 특히 과거 국방.교통.물료 및 환경 분야에서 사용되던 GPS기반의 LBS기술이 이동통신망과 연결되면서 대중적이고 일반적인 서비스로 발전해 나가고 있어 향후 이통사들의 먹거리로 손색없다는 평가를 받고 있다.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
• /
• 2008.05a
• /
• pp.197-200
• /
• 2008

A GNSS augmentation system provides precise position information using corrected GNSS pseudorange measurements. Common bias errors are corrected by PRC (Pseudorange Correction) between reference stations and a rover. However non-common errors (Ionospheric and Tropospheric noise error) are not corrected. Using position error variance this paper analyzes non-common errors (noise errors) of ionosphere and troposphere wet vapor.

• Journal of Advanced Navigation Technology
• /
• v.23 no.3
• /
• pp.221-227
• /
• 2019

In this paper, interacting multiple model (IMM) filter was designed that guarantees a stable navigation performance even in the unstable satellite navigation position. In order to design IMM filter in INS / GPS integrated navigation system, sub filter of the IMM filter is defined as Kalman filter. In the IMM filter configuration, two subfilters are determined. Each Kalman filter defines the six-teenth state composed of position, velocity, attitude, and sensor error from the INS error equation and the states additionally derived in case of the coloured measurement noise. In order to verify the performance of the proposed filter, we compared the performance how the filter works in the presence of arbitrary error in GPS navigation solution. The Monte Carlo simulation was performed 100 times and the results were compared with the root mean square(RMS). The results show that the proposed method is stable against errors and show fast convergence.