• Journal of Advanced Navigation Technology
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• v.20 no.5
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• pp.394-400
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• 2016

It is well known that the encrypted ranging signal, such as GPS P(Y) code, is immune to spoofing attack. However, in order for users to use the signal, there needs permission from the operator. And also there are many restrictions for use because of security issues. In this paper, a ground reference station equipped with high-gain directional antenna and a user receiver were simulated. In the reference station, the encrypted code can be demodulated from the high-gain signal. And then the code can be used to detect spoofing attack in the user receiver. This paper proposes the spoofing detection method using the encrypted signal and deals with simulation results.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2019.05a
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• pp.210-212
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• 2019

위성항법시스템의 취약성에 따른 보완 시스템의 필요가 높아지면서, eLoran 시스템이 가장 현실적인 대안으로 인정받고 있다. 우리나라도 서해 일부 지역에서 eLoran 시스템의 테스트베드 구축 사업을 진행 중에 있다. 전 해양지역에 안정적인 서비스를 제공하기 위해서는 추가적인 송신국 설치가 필요하지만. 여러가지 현실적인 이유로 인해 추진되기 어렵다. 이런 문제를 해결하기 위해 기존의 NDGNSS 기준국을 활용한 측위기술이 개발되고 있다. 이미 운영 중인 NDGNSS 기준국을 활용하면 전 해상에서 탄력적 항법시스템 운용이 가능해질 수 있다. 본 논문에서는 eLoran 시스템과 NDGNSS의 기준국을 활용한 지상파 통합항법시스템의 성능을 예측할 수 있는 시뮬레이션 툴을 제작 하였다. ITU에서 배포한 송출 주파수와 거리에 따른 신호 세기, 대기잡음 등을 고려해 Cramer-Rao Lower Bound로 수신 신호의 측정 거리 오차를 계산하였다. 또한 한빛호가 항해하면서 수집한 DGPS 신호를 통해 실질적인 대기잡음을 추정하는 방법을 사용해 기존보다 정확한 SNR 계산이 가능해졌다. 해당 결과는 추후 진행될 지상파통합항법시스템 개발에 유용하게 활용될 것으로 기대된다.

• Journal of Astronomy and Space Sciences
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• v.25 no.2
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• pp.227-238
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• 2008

GNSS (Global Navigation Satellite System) Ground Station monitors navigation satellite signal, analyzes navigation result, and uploads correction information to satellite. GNSS Ground Station is considered as a main object for constructing GNSS infra-structure and applied in various fields. ETRI (Electronics and Telecommunications Research Institute) is developing Monitoring and Control subsystem, which is subsystem of GNSS Ground Station. Monitoring and Control subsystem acquires GPS and Galileo satellite signal and provides signal monitoring data to GNSS control center. In this paper, the configurations of GNSS Ground Station and Monitoring and Control subsystem are introduced and the preliminary design of Monitoring and Control subsystem is performed. Monitoring and Control subsystem consists of data acquisition module, data formatting and archiving module, data error correction module, navigation solution determination module, independent quality monitoring module, and system operation and maintenance module. The design process uses UML (Unified Modeling Language) method which is a standard for developing software and consists of use-case modeling, domain design, software structure design, and user interface structure design. The preliminary design of Monitoring and Control subsystem enhances operation capability of GNSS Ground Station and is used as basic material for detail design of Monitoring and Control subsystem.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2013.10a
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• pp.366-369
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• 2013

위치, 항법 및 시각정보가 육상, 해상, 항공 등 지구상 거의 모든 공간에서 다양한 목적으로 활용되고 있는 위성항법시스템(GNSS, Global Navigation Satelite System)은 그 중요성이 더욱 높아지고 있으며 미국이 제공해 주는 GPS의 고의잡음(SA)제거 및 성능 향상을 통하여 GNSS를 이용한 응용분야의 발전은 더욱 확대되고 있는 실정이다. 이러한 위성항법시스템의 P.N.T(Position, Navigation and Timing) 서비스 기능을 사회의 전박적인 주요 인프라 시설에 기초적인 원리의 정확성을 더하고 지속성과 무결함성을 제공할 수 있기 때문에 신뢰성을 가지고 여러분야에 활용되고 있으나 지상에서 약20,200km 고도에 위치한 인공위성에서 미약한 신호를 송신함으로써 GNSS 수신기가 의도적이든 비의도적이든 동일한 주파수 밴드의 신호에 영향을 받을 경우 정상적인 역할을 할 수 없다. 우리나라의 경우 P.N.T 서비스 기반 자체가 GPS에 전적으로 의존하고 있으며 유사시 이를 대체할 항법 시스템을 별도로 갖추고 있지 않고 있어 미국의 고의적인 GPS 서비스의 중단이나 주변국가의 방해전파 송신으로 인한 GPS 신호 중단사태가 발생할 경우에는 우리나라 국가 주요 인프라에 치명적인 피해를 입힐 수 있기 때문에 대체항법을 시스템을 구축하여 독자적인 P.N.T 서비스를 제공할 수 있는 시스템 구축이 국가적인 차원에서 절실하게 필요하다.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.18 no.1
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• pp.11-18
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• 2010

GNSS(Global Navigation Satellite System) Ground Station performs GNSS signal acquisition and processing. This system generates error correction information and distributes them to GNSS users. GNSS Ground Station consists of sensor station which contains receiver and meteorological sensor, monitoring and control subsystem which monitors and controls sensor station, control center which generates error correction information, and uplink station which transmits correction information to navigation satellites. Monitoring and control subsystem acquires and processes navigation data from sensor station. The processed data is transmitted to GNSS control center. Monitoring and control subsystem consists of data acquisition module, data formatting and archiving module, data error correction module, navigation determination module, independent quality monitoring module, and system maintenance and management module. The independent quality monitoring module inspects navigation signal, data, and measurement. This paper introduces independent quality monitoring and performs the analysis using measurement data.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.12
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• pp.1232-1237
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• 2009

The ICAO and FAA are developing and verifying of GBAS for civil aircraft landing and take-off. The guarantee of aircraft integrity issue is the important part of GBAS. To guarantee integrity, the GBAS ground facility broadcasts various informations to aircraft. The informations are related to the estimated accuracy of each pseudorange correction and the estimated error terms, for example B-value and standard deviation of the ground facility error. These parameters are used to calculate position error (estimated value of the user). If estimated position errors don't satisfy requirements, aircraft use alternate navigation means. In this paper, GBAS reference stations's real data, which operated by KARI (Korea Aerospace Research Institute) in Jeju international airport, are used to development of new ground facility error standard deviation model. We verify improvement of GBAS availability, with respected to vertical protection level, using B-value based a new ground facility error standard deviation model and a sigma inflation factor.

• 한국항공운항학회:학술대회논문집
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• 2007.06a
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• pp.125-128
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• 2007

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• v.2
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• pp.163-166
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• 2006

본 논문에서는 지상송신국 기반의 로란-C 전파항법시스템이 위성항법시스템(GNSS)의 등장이후 급속한 이용자 감소로 운영의 효율성이 떨어짐에 따라 다양한 각도의 로란-C 성능평가를 실시하여 활용능률 향상방안을 제안하였으며, 국가항법시스템의체계인 관리를 위해 DGPS시스템과 로란-C를 연계한 GNSS 정보센터를 운영하여 GPS는 물론 Galileo, GLONASS 등 위성항법시템 전반의 상황을 모니터링하고 GNSS 불능 시 로란-C를 BACK-UP시스템으로 활용한다면 GNSS 장애로 인한 국가적대혼란의 예방함께 체계적인 전파항법시스템 관리가 가능할 것으로 결론하였다.

• Journal of Navigation and Port Research
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• v.43 no.6
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• pp.429-436
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• 2019

The eLoran system is considered the best alternative because the vulnerability of satellite navigation systems cannot be resolved as perfect. Thus, South Korea is in the process of establishing a testbed of the eLoran system in the West Sea. To provide resilient navigation services to all waters, additional eLoran transmitters are required. However, it is difficult to establish eLoran transmitters because of various practical reasons. Instead, the positioning with NDGNSS/AIS source can expand the coverage and its algorithm with applying continuous waves is under development. Using the already operating NDGNSS reference station and the AIS base station, it is possible to operate the navigation system with higher accuracy than before. Thus, it is crucial to predict the performance when each system is integrated. In this paper, we have developed a simulation tool that can predict the performance of terrestrial integrated navigation system using the eLoran system, maritime NDGNSS station and the AIS station. The esitmated phase error of the received signal is calculated with the Cramer-Rao Lower Bound factoring the transmission power and the atmospheric noise according to the transmission frequency distributed by the ITU. Additionally, the simulation results are more accurate by estimating the annual mean atmospheric noise of the 300 kHz signal through the DGPS signal information collected from the maritime NDGNSS station. This approach can further increase the reliability of simulation results.

• Journal of Advanced Navigation Technology
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• v.27 no.4
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• pp.396-409
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• 2023

In the field of autonomous vehicles, where high accuracy and reliability are critical, various satellite navigation augmentation systems have been developed to improve system performance. These systems generate correction and integrity information based on measurements and navigation data collected from ground reference stations, enhancing user positioning accuracy. Thus, the performance of the system heavily relies on the deployment and spacing of reference stations. To construct an effective satellite navigation augmentation system, careful consideration must be given to the installation points of reference stations. This paper presents a user positioning performance modeling formula and proposes a method for selecting the installation points of new reference stations. The proposed method involves selecting a candidate group area that can optimize the user's positioning performance. By utilizing this method, the system's performance can be improved, ensuring high accuracy and reliability for autonomous vehicle applications.