• Journal of Satellite, Information and Communications
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• v.9 no.4
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• pp.117-126
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• 2014

The COSPAS-SARSAT Search-and-Rescue System detects and locates emergency beacons activated by aircraft, ships and individuals. In particular, when this system is used in wartime and the signal is leaked to the enemy, it can cause the loss of the rescuers and the survivors. This paper proposes an improved method which protects the COSPAS-SARSAT search-and-rescue signal itself from being disclosed during its operation. In addition, there is presented a new protocol which maintains the stabilized security status between survivors and rescuers, using the Galileo/SAR return link.

• Proceedings of the Korean Society of Surveying, Geodesy, Photogrammetry, and Cartography Conference
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• 2006.04a
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• pp.93-98
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• 2006

2008년 서비스 제공을 목표로 진행 중인 유럽의 Galileo 시스템은 최초의 순수 민간 목적으로 제작되는 광역위성항법시스템(GNSS: Global Navigation Satellite System)이다. 현재 GPS의 SA는 제거되었지만, 군사 목적뿐만 아니라 차량 및 항공 항법, 토목 건설 분야, 텔레메틱스를 통한 민간 활용의 증가로 인해 위성측위에 있어 미국의 의존도는 그 어느 때보다 높은 실정이다. 이에 따른 전략적, 기술적 의존은 절대적이며 잠재적인 위험 요소를 포함하고 있다 이에 본 논문에서는 자체 개발한 소프트웨어를 이용하여 향후 제공될 유럽의 Galileo 시스템을 국내 적용 시뮬레이션하였으며 그 결과를 바탕으로 GPS 단독 처리의 한계를 제시하며 이를 극복할 수 있는 대안으로 Galileo 시스템에 대하여 연구하였다. 이를 통하여 러시아의 GLONASS를 포함하여 다원화되어가는 광역위성항법시스템의 안정적인 측위 환경에 대한 연구가 그 목적이다.

• Proceedings of the IEEK Conference
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• 2008.06a
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• pp.421-422
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• 2008

In this paper, CMOS RF front-end circuits for an L1/L5 dual-band global positioning system (GPS)/Galileo receiver are designed in $0.13\;{\mu}m$ CMOS technology. The RF front-end circuits are composed of an RF single-to-differential low noise amplifier, an RF polyphase filter, two down-conversion mixers, two transimpedance amplifiers, a IF polyphase filter, four de-coupling capacitors. The CMOS RF front-end circuits provide gains of 43 dB and 44 dB, noise figures of 4 dB and 3 dB and consume 3.6 mW and 4.8 mW from 1.2 V supply voltage for L1 and L5, respectively.

• Current Industrial and Technological Trends in Aerospace
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• v.5 no.1
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• pp.65-74
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• 2007

현재 운용중인 전 세계적인 위성항법시스템(GNSS : Global Navigation Satellite System)은 미국의 GPS(Global Positioning System)와 러시아의 GLONASS(Global Navigation Satellite System)가 있다. 전 세계적으로 주로 사용되는 시스템은 GPS이며, GLONASS는 러시아의 경제사정 악화로 인하여 지속적인 위성발사가 이루어지지 못하고 있다. 추가적으로 추진되고 있는 위성항법시스템은 유럽의 갈릴레오(Galileo), 중국의 북두(Beidou), 일본의 JRANS(Japanese Regional Advanced Navigation System) 그리고 2006년 5월에 구축 프로젝트가 승인된 인도의 IRNSS(Indian Regional Navigation Satellite System)가 있다. 보강시스템의 경우, 미국 FAA(Federal Aviation Administration)는 광역오차보정시스템(WAAS)을 Raytheon사와 개발하였으며, 현재 착륙용 근거리오차보정시스템(LAAS)을 Raytheon사 및 Honeywell사와 함께 정부/산업체 공동개발 사업(GIP; Government Industry Partnership)으로 진행 중에 있다. 유럽은 EGNOS(European Geostationary Navigation Overlay Service)를 사용하고 있으며, 일본의 MSAT(MTSAT Satellite Based Augmentation System)와 인도의 GAGAN(GPS and GEO Augmented Navigation)은 추진 중이다. 이 글에서는 위성항법시스템과 위성항법 보강시스템의 현황을 살펴본다.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.39A no.6
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• pp.343-349
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• 2014

In this paper, we propose a three-stage unambiguous tracking scheme for CBOC signals. We evenly divide composite binary offset carrier (CBOC) signal, which was adopted in the Galileo system developed by the European Union (EU), by width of BOC(6,1) signal pulse, and then, generate 12 partial correlations. Then, we generate an unambiguous correlation function by recombining the partial correlations with two kinds of operation. The proposed correlation function is narrower and higher than the conventional correlation functions. From simulation result, it is shown that the proposed correlation function offers a better signal tracking performance over the conventional correlation functions.

• Spatial Information Research
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• v.14 no.2 s.37
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• pp.177-189
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• 2006

In the past several years there has been relying on USA fur the resource of global positioning data in the pluralistic GNSS environment(Galileo, Post GPS, Quasi-Zenith Satellite System). For this reason, we should make a decision which strategy for research is carried out. According to a diversity of resource for obtaining positioning data, well organized research support at government level for efficient using is required. Specially, it is very Important that subcommittee for research organized with National GIS Promotion Committee as a leader make counterplan strategy. We have obtained an conclusion that we can make a good decision by establishing Spatial Information Expert Group and selection of essential element of technology.

• Journal of Astronomy and Space Sciences
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• v.25 no.1
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• pp.43-52
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• 2008

As the next generation of global satellite navigation system, the Galileo project is about to witness an initial orbit validation stage as the successful test of navigation message transmission from Giove-A in 2007. The Space Geodesy division ana the Radio Astronomy division of the Korea Astronomy & Space Science Institute had collaborated on the field survey for the Galileo Sensor Station (GSS) RF environment of the proposed site near Jeju Tamla University from August 3rd to August 5th, 2006. The power spectrums were measured in full-band $(800{\sim}2000MHz)$ and in-band (E5, E6 and L1 band) in frequency domain for 24 hours respectively. Finally, we performed a time domain analysis to characterize strong in-band interference source based on the result of the previous step.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.21 no.4
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• pp.315-324
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• 2011

This paper presents a historical study on the derivation of the differential equation of motion for the single-degree-of-freedom m-k system with the harmonic excitation. It was Euler for the first time in the history of vibration theory who tackled the equation of motion for that system analytically, then gave the solution of the free vibration and described the resonance phenomena of the forced vibration in his famous paper E126 of 1739. As a result of the chronological progress in mechanics like pendulum condition from Galileo to Euler, the author asserts two conjectures that Euler could apply to obtain the equation of motion at that time.

• Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
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• v.38 no.6
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• pp.521-531
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• 2020

QZSS (Quasi-Zenith Satellite System) provides the CLAS (Centimeter Level Augmentation Service) through the satellite's L6 band. CLAS provides correction messages called C-SSR (Compact - State Space Representation) for GPS (Global Positioning System), Galileo and QZSS. In this study, CLAS messages were received by using the AsteRx4 of Septentrio which is a GPS receiver capable of receiving L6 bands, and the messages were decoded to acquire C-SSR. In addition, Multi-GNSS (Global Navigation Satellite System) Code-PPP (Precise Point Positioning) was developed to compensate for GNSS errors by using C-SSR to pseudo-range measurements of GPS, Galileo and QZSS. And non-linear least squares estimation was used to estimate the three-dimensional position of the receiver and the receiver time errors of the GNSS constellations. To evaluate the accuracy of the algorithms developed, static positioning was performed on TSK2 (Tsukuba), one of the IGS (International GNSS Service) sites, and kinematic positioning was performed while driving around the Ina River in Kawanishi. As a result, for the static positioning, the mean RMSE (Root Mean Square Error) for all data sets was 0.35 m in the horizontal direction ad 0.57 m in the vertical direction. And for the kinematic positioning, the accuracy was approximately 0.82 m in horizontal direction and 3.56 m in vertical direction compared o the RTK-FIX values of VRS.

• Journal of Satellite, Information and Communications
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• v.4 no.1
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• pp.36-44
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• 2009

The key technologies of GNSS receiver for GNSS sensor station are under development as a part of a GNSS ground station in ETRI. This paper presents the GNSS receiver implementation and signal processing result which is implemented based on FPGA to process the Galileo E1 and E5 signal. To verify the working and performance for GNSS receiver which is implemented based on FPGA, live signal received from GIOVE-B which is second test satellite is used. We gather GIOVE-B signal by using prototyping antenna and RF/IF units including IF-component. To verify Galileo E1 and E5 signal processing function from GIOVE-B, FPGA based signal processing module is implemented as a prototyping hardware board.