• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.6
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• pp.481-487
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• 2013

In GPS(Global Positioning System)/INS(Inertial Navigation System) integrated navigation systems, GPS antennas and an inertial measurement units are usually installed outside and inside of the vehicle, respectively. By the difference of installed locations, performance of GPS/INS integrated navigation systems is affected by lever arm errors. For more accurate navigation, lever arm errors need to be compensated correctly since it directly affects the accuracy of navigation states. This paper proposes an effective lever arm error compensation method that utilizes velocity measurements of GPS and INS. By an experiment, feasibility of the proposed algorithm is verified. It is also shown that lever arm compensation is especially important when vehicles are experiencing rotational movements.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2014.10a
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• pp.189-191
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• 2014

보다 편리하고 안전한 항해를 위해 GPS 뿐만 아니라 GLONASS 등 다양한 위성항법시스템이 항해장비 및 통신장비에 이용되고 있다. 특히 항만을 포함한 연안에서는 위성항법시스템 단독으로 제공하는 위치 항법 시각정보 보다 더 정확하고 신뢰할 수 있는 정보를 얻기 위해 보강시스템 개념의 DGPS 서비스를 제공하고 있다. 위성항법시스템의 다원화는 현재 연근해는 물론이고 육상에서도 제공하고 있는 DGPS 서비스를 DGNSS 서비스로 확장해야 하는 필요를 낳았다. 본 논문은 현재 구축된 해양보정시스템에 대해서 살펴보고, 해양 DGPS 인프라가 다중 위성항법시스템을 위한 서비스를 위해서 고려해야 할 사항에 대해 분석한다.

• Journal of Advanced Navigation Technology
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• v.18 no.4
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• pp.312-318
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• 2014

The altitudes of GEO satellites are higher than those of GPS satellites. Therefore the visibility and the received power of GPS signals are totally different from those of the users near the Earth's surface. In this study, we analyzed the visibility of GPS signals received on GEO satellites. And we also developed a software GPS receiver that works on GEO satellites using CCMDB algorithm which is a weak signal receiver algorithm. GPS signals received on a GEO satellite are generated by a commercial hardware GPS simulator and used for the verification of the developed software GPS receiver. The mean 3D position and velocity error are calculated as 165.636 m and 0.5081 m/s.

• Journal of Satellite, Information and Communications
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• v.7 no.1
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• pp.128-133
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• 2012

In this paper, we analysis the effect of error of code tracking and frequency tracking according to the chip delay of spoofing signal through the simulation. Firstly, we investigate the type of spoofing signal and defense technical of spoofing attack. For simulation, we generated the intermediate spoofing signal using the software GNSS signal generator simulator(SGGS), the intermediate spoofers synchronize its counterfeit GPS signals with the current broadcast GPS signals. The software GPS receiver simulator(SGRS) received the spoofing signal and normal signal from SGGS, and process the signals. In paper, we can check that the DLL and PLL tracking loop error are generated and pseudo-range is changed non-linear according to chip delay of spoofing signal when the spoofing signal is entered. As a result, we can check that navigation solution is incorrectly effected by spoofing signal.

• Journal of the Institute of Electronics Engineers of Korea SC
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• v.41 no.1
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• pp.1-8
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• 2004

The INS(Inertial Navigation System) provides high rate position, velocity and attitude data with good short-term stability while the GPS(Global Position System) provides position and velocity data with long-term stability. By integrating the INS with GPS, a navigation system can be achieved to Provide highly accurate navigation Performance. For the best performance, time synchronization of GPS and INS data is very important in GPS/INS integrated system But, it is impossible to synchronize them exactly due to the communication and computation time-delay. In this paper, to reduce the error caused by the measurement time-delay in GPS/INS integrated systems, error compensation methods using separate bias Kalman filter are suggested for both the loosely-coupled and the tightly-coupled GPS/INS integration systems. Linearized error models for the position and velocity matching GPS/INS integrated systems are Int derived by linearizing with respect to its time-delay and augmenting the delay-state into the conventional state equations for each case. And then separate bias Kalman Inter is introduced to estimate the time-delay during only initial navigation stage. The simulation results show that the present method is effective enough resulting in considerably less position error.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2013.10a
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• pp.145-146
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• 2013

보다 편리하고 안전한 항해를 위해 GPS 뿐만 아니라 GLONASS 등 다양한 위성항법시스템이 항해장비 및 통신장비에 이용되고 있다. 특히 항만을 포함한 연안에서는 위성항법시스템 단독으로 제공하는 위치 항법 시각정보 보다 더 정확하고 신뢰할 수 있는 정보를 얻기 위해 보강시스템 개념의 DGPS 서비스를 제공하고 있다. 위성항법시스템의 다원화는 현재 연근해는 물론이고 육상에서도 제공하고 있는 DGPS 서비스를 DGNSS 서비스로 확장해야 하는 필요를 낳았다. 본 논문은 현재 국제기구가 제정한 기술표준과 권고서를 분석하고, 이들이 가지고 있는 다원화의 한계성과 유연성, 확장성의 부족을 제시한다. 그리고 현재 논의되고 있는 차세대 DGNSS 관련 국제표준과 제시한 문제와의 상관관계를 보인다. 마지막으로 본 논문은 DGNSS 서비스를 위한 국제표준의 변화가 미치게 될 영향에 대해 전망한다.

• Journal of the Korean Society of Surveying, Geodesy, Photogrammetry and Cartography
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• v.32 no.2
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• pp.163-171
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• 2014

Based on the GPS/IMU integration, the car navigation has unstable conditions as well as drastically reduces accuracies in urban region. Nowadays, many cars mounted the camera to record driving states. If the ground coordinates of street furniture are known, the position and attitude of camera can be determined through SPR(Single Photo Resection). Therefore, an estimated position and attitude from SPR can be applied measurements in Kalman filter for updating errors of navigation solutions from GPS/IMU integration. In this study, the GPS/IMU/SPR integration algorithm was developed in loosely coupled modes through extended Kalman filters. Also, in order to analyze performances of GPS/IMU/SPR, simulation tests were conducted in GPS signal reception environments and the GCPs (Ground Control Points) distributions. In fact, the position and attitude gathered from GPS/IMU/SPR integration are more precise than the position and attitude from GPS/IMU integration. When IPs (image points), corresponded to GCPs, were concentrated in the center of image, the position error in the optical axis respectively increased. To understand effects from SPR, we plan to carry additional test on the magnitude of GCP, IP and initial exterior orientation errors.

• Journal of Satellite, Information and Communications
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• v.8 no.2
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• pp.29-35
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• 2013

In this paper, we investigate the type and detection methode of spoofing attack, and then analyze the performance of spoofing detection algorithm in GPS L1 signal through the simulation. Generally spoofer is different from the jammer, because the receiver can be operated and not. In case of spoofing the GPS receiver is hard to recognize the spoofing attack and can be operated normally without stopping because the spoofing signal is the mimic GPS signal. To evaluate the performance of spoofing detection algorithm, both the software based spoofing and GPS signal generator and the software based GPS receiver are implemented. In paper, we can check that spoofing signal can affect to the DLL and PLL tracking loop because code delay and doppler frequency of spoofing. The spoofing detection algorithm has been implemented using the pseudorange, signal strength and navigation solution of GPS receiver and proposed algorithm can effectively detect the spoofing signal.

• Proceedings of the Korean Institute of Navigation and Port Research Conference
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• 2015.10a
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• pp.270-272
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• 2015

선박의 항해 도중 GPS 위성을 이용하여 위치를 추정하는 방법이 널리 사용되고 있다. 본 연구에서는 재밍으로 인하여 항해 중에 간헐적인 GPS 신호의 획득은 가능하나 지속적인 신호 추적이 불가하여 GPS 위성의 코드 위상 측정치만 얻을 수 있는 상황을 가정하였다. 동 시간대의 기준국에서 수신한 항법 메시지와 신호 획득 과정에서 측정된 코드 위상 만을 이용하여 GPS C/A 코드의 반복 횟수를 정확히 추정하고 대략적인 위치 해를 계산하는 알고리즘을 개발하였다.

• Journal of the Korea Institute of Information and Communication Engineering
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• v.21 no.6
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• pp.1243-1251
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• 2017

When a Ship sails in the ocean, it is significant to find one's position for safe navigation. Most of ships have been using GPS navigation since its development after 1990's. The celestial navigation was used as the navigation method when sailing in the ocean, but time-consuming process such as complicated calculation and plotting the result on chart diminished its utilization. The thesis explains convenience and utilization of existing celestial navigation by resolving challenges it has. As a way of enhancing the celestial navigation, the author developed a software which incudes a numerical formula based on the previous calculation process. When a navigator inputs the altitude of sun, GHA and dec into computer while sailing, the position of the ship will be displayed as the coordinates. The improved method thus reaffirmed the usefulness of the celestial navigation and will greatly serve as means of navigation in the occurrence of distress. Abstract should be placed here.