• 한국정보통신학회:학술대회논문집
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• 한국정보통신학회 2015년도 추계학술대회
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• pp.270-271
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• 2015

최근 사물 사이의 정보 소통을 가능하게 하는 사물 인터넷 기술을 이용한 지능형 실내 위치 인식서비스에 대한 관심이 증대되고 있다. 특히 스마트 기기를 이용한 실내 위치 기반 서비스에 대한 수요와 적용 사례가 활발히 이루어지고 있다. 이를 위해 실내 위치 측위 기술로서 BLE (Bluetooth Low Energy) 기술에 많은 관심이 증가되고 있다. 그러나 iBeacon이 제공하는 신호만을 이용하여 측위를 하게 되면 신호 간섭 등의 이유로 실내 위치 정보의 신뢰도는 떨어지게 된다. 본 논문에서는 iBeacon의 신호 정보로 부터 신뢰성 있는 위치 정보를 얻기 위한 데이터 수집 방법과 신뢰도 높은 위치 정보 연산 기법을 제안한다.

• 대한기계학회논문집A
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• 제21권6호
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• pp.918-924
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• 1997

A method for measuring the accuracy of rotating objects was studied. Rotating axis errors are significant; such as the spindle error of a manufacturing machine which results in the surface roughness of machined work pieces. Three capacitance type displacement sensors were used to measure the rotating master ball position. The sensors were mounted to the three orthogonal points on the spindle axis. The measurement data were analyzed and shown for rotating spindle accuracy, not only for average roundness error but also for spindle volumetric positional error during the revolutions. This method is simple and economical for industrial field use with regular inspection of rotating machines using portable equipment. Measuring and analyzing time using this method takes only a couple of hours. This method can also measure microscopic amplitude and 3-dimensional direction of vibrating objects.

• 한국전자통신학회논문지
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• 제14권3호
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• pp.601-606
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• 2019

렌티큘러 위치기반 시스템은 지상 및 실외중심의 지역, 건물, 선박, 지하 등 실내에 있는 사용자가 스스로 자신의 위치를 실시간으로 알릴 수 있는 위치정보 기술이다. 본 논문에서는 이전의 실내 위치 인식기술의 한계성과 문제점을 분석하고, 이용자 중심의 위치서비스 방법을 제안한다. 제안된 방법은 렌티큘러 스티커, 데이터베이스(DB) 수집 및 분석기술, 측위시스템으로 구성되어 있고, 측위오차기반 서비스를 실행하기 위한 기반 인프라로 활용될 수 있을 것이며, 실내 렌티큘러를 이용한 위치기반시스템 개발을 통하여 사용자 중심의 측위 정확도 향상뿐만 아니라, 각종 재난안전 상황에서 신속한 구조활동에 사용자 중심의 위치기반 시스템으로 활용할 수 있을 것이다.

• Journal of Positioning, Navigation, and Timing
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• 제11권4호
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• pp.317-325
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• 2022

In this paper, we developed a single frequency-based RRAIM to monitor integrity of the UAM landing vertically in urban area with only low-cost single-frequency GPS receiver. Conventional dual-frequency RRAIM eliminates ionospheric delay through a combination of frequencies. In this study, ionospheric delay was directly modeled. Drift error of residual ionospheric delay is modeled using the previously studied result on ionospheric rates of change. To verify the performance of the proposed RRAIM algorithm, a simulation of vertical landing UAM in urban area was conducted. It was assumed that the protection level at the initial position was calculated through SBAS correction data. During vertical landing, integrity monitored by receiver alone without external correction data. In the 60 sec simulation, the protection level of the proposed RRAIM compared to the conventional RRAIM was calculated to be 140% due to the accumulated ionospheric delay error. Nevertheless, it was confirmed that the final vertical protection level meeting the requirements of LPV-200, which cannot be achieved with single frequency GPS receiver alone.

• Journal of Positioning, Navigation, and Timing
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• 제9권4호
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• pp.357-366
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• 2020

This paper addressed a relative navigation method for autonomous rendezvous and docking of cube-satellites using single frequency Differential GPS (DGPS) under the intermittent communication between satellites. Since the ionospheric error of GPS measurement is variable depending on the visible satellites, a few meters error of relative navigation is occurred in the Low-Earth Orbit (LEO) environment. Therefore, it is essential to remove the ionospheric error to perform relative navigation. Besides, an intermittent communication period for receiving GPS measurements of the target satellite is limited for getting information every sampling time. To solve this problem, a method combining range domain DGPS and orbit propagation is proposed in this paper. The proposed method improves the performance of DGPS by using Hatch filter and solves an intermittent communication problem by estimating the relative position and velocity using Hill-Clohessy-Wiltshire Equation. Through the simulation, it is verified that the suggested algorithm provides the relative position error within RMS 0.5 m and the relative velocity error within RMS 3 cm/s. Furthermore, it has the advantage that it is suitable for real-time implementation using single-frequency GPS measurements and is computationally efficient.

• Journal of Positioning, Navigation, and Timing
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• 제11권3호
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• pp.147-156
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• 2022

In this paper, we propose Time-Division-Multiplexing Tertiary Offset Carrier (TDMTOC), a novel GNSS modulation based on Tertiary Offset Carrier (TOC) modulation. The TDMTOC modulation multiplexes two three-level signals (i.e., -1, 0, and 1) while crossing over time, and is a type of TOC modulation designed specifically for signal multiplexing. The proposed modulation generates TDMTOC subcarriers of two different phases by simply combining two Binary Offset Carrier (BOC) subcarriers by addition or subtraction. TDMTOC has better correlation and spectral properties than conventional BPSK, BOC, and MBOC modulation techniques, and has good power and spectral efficiency since it can multiplex signals without power loss similar to time division multiplexing. To prove this, we introduce the multiplexing process of TDMTOC, and compare TDMTOC with Binary Phase Shift Keying (BPSK), BOC, Composite BOC (CBOC), and Time Multiplexed BOC (TMBOC) that are currently serviced in GNSS by simulations of various aspects. Through the simulation results, we prove that TDMTOC has better correlation property than modulations currently used in GNSS, less intersystem interference due to its wide spectrum property, and robustness in multipath and noise channel environments.

• Journal of Positioning, Navigation, and Timing
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• 제12권4호
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• pp.335-342
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• 2023

Lunar Navigation Satellite System refers to a constellation of satellite providing PNT services on the moon. LNSS consists of main satellite and navigation satellites. Navigation satellites orbiting around the moon and a main satellite moves the area between the moon and the L2 point. The navigation satellite performs the same role as the Earth's GNSS satellite, and the main satellite communicates with the Earth for time synchronization. Due to the effect of the non-uniform shape of the moon, it is necessary to focus on the influence of the lunar gravitational field when designing the orbit simulation for navigation satellite. Since the main satellite is farther away from the moon than the navigation satellite, both the earth's gravity and the moon's gravity must be considered simultaneously when designing the orbit simulation for main satellite. Therefore, the main satellite orbit simulation must be designed through the three-body problem between the Earth, the moon, and the main satellite. In this paper, the orbit simulation tool for main satellite and navigation satellite required for LNSS was designed. The orbit simulation considers the environment characteristics of the moon. As a result of comparing long-term data (180 days) with the commercial program GMAT, it was confirmed that there was an error of about 1 m.

• Journal of Positioning, Navigation, and Timing
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• 제13권1호
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• pp.63-73
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• 2024

NeQuick G is the ionosphere model utilized by Galileo single-frequency users to estimate the ionospheric delay on each user-satellite link. The model is characterized by the effective ionization level (Az) index, determined by a modified dip latitude (MODIP) and broadcast coefficients derived from daily global space weather observations. However, globally fitted Az coefficients may not accurately represent ionosphere within local area. This study introduces a method for regional ionospheric modeling that searches for locally optimized Az coefficients. This approach involves fitting TEC output from NeQuick G to TEC data collected from GNSS stations around Korea under various ionospheric conditions including different seasons and both low and high solar activity phases. The optimized Az coefficients enable calculation of the Az index at any position within a region of interest, accounting for the spatial variability of the Az index in a polynomial function of MODIP. The results reveal reduced TEC estimation errors, particularly during high solar activity, with a maximum reduction in the RMS error by 85.95%. This indicates that the proposed method for NeQuick G can effectively model various ionospheric conditions in local areas, offering potential applications in GNSS performance analyses for local areas by generating various ionospheric scenarios.

• 한국산학기술학회논문지
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• 제14권5호
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• pp.2481-2486
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• 2013

GPS에 대한 이해가 부족한 일반사용자가 정상적으로 GPS 자료를 처리하기 위해서는 많은 시간과 노력이 필요하다. 하지만 GPS 자료처리 분야는 외산 소프트웨어에 크게 의존하고 있으며, 사용자 위주의 기술 개발은 거의 이루어지지 않고 있다. 이에 본 연구에서는 비전문가도 상대측위 방법으로 고정밀 GPS 자료처리가 가능한 전문가 서비스를 구축하고자 하였다. 연구결과, GPS 자료처리에 필요한 최소 정보만을 입력함으로써 사용자의 편의성을 극대화시킬 수 있는 전문가 서비스를 개발하였으며, 국토지리정보원에서 제공하는 위성기준점의 관측자료와 실제 GPS측량으로 취득한 관측자료의 처리를 통해 전문가 서비스를 검증하였다. 전문가 서비스는 GPS 자료처리에 소요되는 노력과 시간을 크게 단축시킴으로써 정밀위치결정은 물론 다양한 학술연구에 기여할 것이다.

• 한국위성정보통신학회논문지
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• 제10권4호
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• pp.58-63
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• 2015

GPS(Global Positioning System는 지구상에서 약 2km 떨어진 위성으로부터 송신한 신호를 수신하므로 그 수신감도가 매우 낮아 재밍과 간섭에 매우 취약하다. 따라서 GPS 수신단에서 항재밍 능력에 대한 필요성은 점점 증가하고 있다. 이러한 GPS의 취약성을 이용하여 전시 상황에서 적군은 재밍 기법을 이용하여 수신단에서 아군의 GPS 신호를 이용한 정확한 측위를 방해한다. 따라서 전시상황에 대비하여 재밍 환경에 대응하고, 측위 정보를 획득할 수 있는 방법이 필요하다. 본 연구에서는 재밍 환경에서의 측위 정확도를 향상시키기 위해 BSS(Blind Source Separation) 기법을 사용하여 GPS 신호와 재밍 신호를 분리하는 방법을 제안한다. 또 재밍신호와 분리된 GPS 신호에는 여전히 잡음(noise)이 존재해 정확한 측위 정보를 획득하기 어렵다. 따라서 잡음을 효과적으로 제거하기 위해 웨이블릿 임계화 기법을 사용한다. 실험 결과는 본 연구실에서 수행한 GPS/QZSS/Wi-Fi 밀결합 측위기법의 테스트 결과를 이용하여 재밍 환경에서의 BSS 와 웨이블릿 임계화 기법을 통한 정확도 향상을 보이며 제안한 시스템 모델의 우수성을 입증한다.