• 한국컴퓨터정보학회논문지
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• 제28권2호
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• pp.121-129
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• 2023

이 논문에서 우리는 응급상황에 대응하여 일정 구간의 교통신호를 능동적으로 제어함으로써 재산과 인명 손실을 최소화할 수 있는 응급상황 대응 교통신호 제어 시스템을 개발하였다. 응급 차량 단말기에서 식별정보 및 GPS 정보를 포함한 응급신호를 송출하면 카메라에서 주위 영상을 획득하게 되고, 딥러닝 기반으로 객체를 분석하여 객체의 위치, 종류, 크기 등 정보를 가지는 객체정보를 출력한다. 이 객체를 트래킹한 정보를 생성하여 신호체계를 검출한 후 신호체계를 응급모드로 전환하여 수신받은 GPS 정보를 기준으로 응급 차량을 식별·추적하고 이 응급 차량의 진행 경로 기준으로 긴급 제어신호를 교통신호 제어기로 전송할 수 있는 체계이다. 이 시스템은 응급신호에 따라 우선 적용되는 긴급 제어신호에 의해 응급 차량의 진행이 저지되지 않도록 하여, 교통상 장애에 따른 인명과 재산의 손실을 최소화할 수 있다.

• 한국측량학회지
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• 제28권1호
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• pp.65-72
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• 2010

본 연구에서는 MMS인 경우 고성능의 중급 IMU가 사용되고 보행자 항법시스템에서는 MEMS형의 저급 IMU가 사용된다고 가정한 후 GPS 신호가 단절되었을 경우 IMU에 의해 생성되는 위치 및 자세 오차를 시뮬레이션을 통하여 계산하였다. 또한 GPS 신호 단절 시에 고도계, 전자나침반 및 2가지 센서를 동시에 이용하는 MultiSensor를 이용하여 중급 및 저급 IMU를 보정하였을 경우의 정확도 향상 효과를 분석하였다. 실험 결과 중급 IMU의 경우 MMS에서 요구되는 3차원 위치오차 정확도가 5m라고 가정할 경우 GPS 단절 시간이 30초가 넘으면 요구 정확도를 만족하지 못하였다. 하지만 GPS 단절 구간에서 고도계 전자나침반 그리고 MultiSensor를 이용하여 IMU 보정을 수행할 경우 약 60초까지 요구정확도를 만족하였다. 또한 고도계 및 전자나침반을 동시에 사용할 경우 고도계에 의한 영향이 더욱 큰 것으로 판단된다 MEMS IMU와 같은 저급 IMU가 사용되는 보행자 항법 시스템의 요구 위치 정확도가 약 20m라고 가정할 경우 4초 이후에는 요구 정확도를 만족하지 못하였으며 자세 오차도 매우 급증하였다. 하지만 GPS 신호 단절시 보조센서를 이용하여 저급 IMU 보정을 수행하였을 경우 약 15초까지 요구 정확도를 만족할수 있을 것으로 시뮬레이션 결과 예측되었으며 또한 중급 IMU 실험과는 반대로 보행자 항법과 같은 속도가 느린 시스템에서 고도계 및 전자나침반 2가지 센서를 동시에 사용할 경우 전자나침반에 의한 영향이 더욱 큰 것으로 나타났다. 본 연구는 GPS 신호 단절이 발생할 수 있는 지역에 대하여 MMS 또는 보행자 항법시스템을 운용할 경우 요구 정확도에 따른 보조센서 통합을 이용하여 정확도를 높이는 자료로써 사용될 수 있을 것으로 예상된다.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
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• pp.235-240
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• 2006

Ionospheric scintillation induces a rapid change in the amplitude and phase of radio wave signals. This is due to irregularities of electron density in the F-region of the ionosphere. It reduces the accuracy of both pseudorange and carrier phase measurements in GPS/satellite based Augmentation system (SBAS) receivers, and can cause loss of lock on the satellite signal. Scintillation is not as strong at mid-latitude regions such that positioning is not affected as much. Severe effects of scintillation occur mainly in a band approximately 20 degrees on either side of the magnetic equator and sometimes in the polar and auroral regions. Most scintillation occurs for a few hours after sunset during the peak years of the solar cycle. This paper focuses on estimation of the effects of ionospheric scintillation on GPS and SBAS signals using a software receiver. Software receivers have the advantage of flexibility over conventional receivers in examining performance. PC based receivers are especially effective in studying errors such as multipath and ionospheric scintillation. This is because it is possible to analyze IF signal data stored in host PC by the various processing algorithms. A L1 C/A software GPS receiver was developed consisting of a RF front-end module and a signal processing program on the PC. The RF front-end module consists of a down converter and a general purpose device for acquiring data. The signal processing program written in MATLAB implements signal acquisition, tracking, and pseudorange measurements. The receiver achieves standalone positioning with accuracy between 5 and 10 meters in 2drms. Typical phase locked loop (PLL) designs of GPS/SBAS receivers enable them to handle moderate amounts of scintillation. So the effects of ionospheric scintillation was estimated on the performance of GPS L1 C/A and SBAS receivers in terms of degradation of PLL accuracy considering the effect of various noise sources such as thermal noise jitter, ionospheric phase jitter and dynamic stress error.

• 제어로봇시스템학회논문지
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• 제14권7호
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• pp.702-710
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• 2008

In this paper, the observability of the INS/GPS integrated system for a land vehicle is analyzed on measurements and different filters with respect to the measurements are designed. In the stationary case, it is shown that horizontal accelerometer biases and vertical attitude errors and gyro biases are unobservable. An 8-state filter is designed based on the observability analysis. When GPS signal is available, a 15-state filter is used with position and velocity measurements. To estimate the INS errors even in the case that GPS signal is blocked a filter is designed in consideration of the non-holonomic constraints of a land vehicle. In this case, the horizontal position and velocity errors and vertical attitude error are unobservable. However, a 12-state filter including the velocity states is designed to estimate the accelerometer biases. When GPS signal recovers, a 9-state filter is used excluding the sensor biases. This paper presents a multi-dimensional filter that switches the four filters according to the usable measurements and maneuver environments. A simulation is carried out to verify the performance of the proposed filter.

• Journal of Positioning, Navigation, and Timing
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• 제4권4호
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• pp.173-180
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• 2015

In this study, an algorithm that detects a spoofing signal for a GPS L1 signal was proposed, and the performance was verified through RF spoofing signal simulation. The proposed algorithm determines the reception of a spoofing signal by detecting a correlation distortion of GPS L1 C/A code caused by the spoofing signal. To detect the correlation distortion, a detection criterion of a spoofing signal was derived from the relationship among the Early, Prompt, and Late tap correlation values of a receiver correlator; and a detection threshold was calculated from the false alarm probability of spoofing signal detection. In this study, an RF spoofing environment was built using the GSS 8000 simulator (Spirent). For the RF spoofing signal generated from the simulator, the RF spoofing environment was verified using the commercial receiver DL-V3 (Novatel Inc.). To verify the performance of the proposed algorithm, the RF signal was stored as IF band data using a USRP signal collector (NI) so that the data could be processed by a CNU software receiver (software defined radio). For the performance of the proposed algorithm, results were obtained using the correlation value of the software receiver, and the performance was verified through the detection of a spoofing signal and the detection time of a spoofing signal.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2005년도 ICCAS
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• pp.1234-1238
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• 2005

As the low power GPS signal is susceptible to interference, interference can seriously degrade the performance of GPS receiver. This paper designs a ANIEF(Adaptive Narrowband Interference Excision in Frequency domain) filter that removes narrow band interferences with low signal loss. This filter uses the pre-correlation technique and attempts to filter out the interference in the frequency domain. The interference excision performance of the designed filter is evaluated for various interferences using the ANIEF filter inserted GPS software receiver and the interference generator. Interferences considered in this paper are single-tone CWI(Continuous Wave Interference), multi-tones CWI, pulsed CWI, and swept CWI. The narrowband interference excision filter in frequency domain is very effective against various interferences and the strong interference with a simple structure. However, the signal power loss is unavoidable while transforming. In this paper, the hamming window and overlap technique are adopted to reduce the signal power loss. Finally, the interference excision performance and the reduced signal power loss of the ANIEF filter are shown.

• 제어로봇시스템학회논문지
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• 제12권8호
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• pp.729-738
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• 2006

In recent days, navigation technology becomes more important as location based service (LBS) such as E911 and telematics are considered as attractive business fields. Commercial LBS requires that navigation system should be inexpensive and available anytime and anywhere - indoors and outdoors. If we consider these requirements, it is out of question that GPS is the most favorite system in the world. However, GPS has a serious problem. The one is that GPS does not operate indoors well. This is because GPS satellites are about 20,000km above the ground so that indoor signals are too weak to be tracked in GPS receiver. And the other is that vertical accuracy is less than horizontal accuracy, because of GPS satellites' geometry. To solve these problems, many researches have been done around the world since 1990s. This paper is also one of them and we will introduce an excellent solution by use of pseudolite. Pseudolite is a kind of signal generator, which transmits GPS-like signal. So it is same as GPS satellite in ground. In this paper, we will propose the integrated navigation system of GPS and pseudolite and show the flight test results using RC airplane to proof our navigation system. As a result, we could improve the vertical accuracy of airplane into the horizontal accuracy.

• 한국전자통신학회논문지
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• 제12권1호
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• pp.61-68
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• 2017

본 논문에서는 민간용으로 사용되는 GPS 시스템의 C/A 부호(Coarse Acquisition Code)를 연구, 모의실험하고, 분석하였다. 모의실험은 Matlab을 사용하였다. 실제의 GPS 신호를 해석하는 문제를 모의실험을 한 결과, 이 부호 문제의 융통성과 정확성을 확인할 수 있었다. 이의 방법의 응용으로 위성신호를 정확하게 추적할 수 있게 할 수 있고, 위성수신기의 성능을 향상시키는데 도움이 될 것이다.

• 한국항해항만학회:학술대회논문집
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• 한국항해항만학회 2015년도 추계학술대회
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• pp.279-282
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• 2015

해양수산발전 기본법 제 15조(해양안전관리 등)에 의거 해양안전 및 해양교통시설의 하나인 위성항법 보정서비스(DGPS) 전국망 구축에 따라 국가 인프라 활용도를 극대화하고 대국민 편익 개선을 위해 원천기술개발이 꾸준히 제기 되고 있다. 특히 해양용 중파수신기 공급제품 유형을 살펴보면 국제해사기구(IMO) 권고에 만족하는 성능 제품 대부분 안테나와 수신기가 분리되는 구조 공급되고 있고 일부 통합모델의 경우 매우 고가모델로 해양용 수신기 보다는 휴대가 쉬운(Portable) 측위용으로 일부 활용되고 있어 저렴한 통합모델 개발이 요구되고 있다. 현재 해양용 위성항법 보정정보 수신기 중 GPS모듈, 중파모듈 각각은 저가 개발이 가능하나 독립적 운용 환경에서 통합모델 개발 이루어지지 않아 어떠한 문제가 있는지 살펴보고, 285kHz~315kHz 중파(medium wave or Beacon)를 이용한 DGPS Beacon 수신기 구조에서 중파안테나와 GPS수신기가 중파대역 폭당 신호대 잡음비(SNR: Signal to Noise Ratio)가 GPS 수신기에 미치는 영향에 대해 중점 연구하였다. 본 연구는 중파와 GPS 통합과정에서 중파안테나 및 수신부와 GPS안테나와 수신부가 어떤 영향을 미치고 GPS 신호감쇄가 DGPS 성능에 미치는 특성을 GPS 제조사별로 살펴보았고 중파 정규화 신호대 잡음비가 GPS제조사별 미치는 영향과 중파신호 영향에 대해 GPS 대역 폭당 잡음 전력비 성능개선을 위한 제안을 하였다.

• International Journal of Aeronautical and Space Sciences
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• 제9권2호
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• pp.121-128
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• 2008

Modularized GPS software defined radio (SDR) has many advantages of applying and modifying algorithm. Hardware based GPS receiver uses many hardware parts (such as RF front, correlators, CPU and other peripherals) that process tracked signal and navigation data to calculate user position, while SDR uses software modules, which run on general purpose CPU platform or embedded DSP. SDR does not have to change hardware part and is not limited by hardware capability when new processing algorithm is applied. The weakness of SDR is that software correlation takes lots of processing time. However, in these days the evolution of processing power of MPU and DSP leads the competitiveness of SDR against the hardware GPS receiver. This paper shows a study of modulization of GPS software platform and it presents development of the GNSS software platform using MATLAB Simulink™. We focus on post processing SDR platform which is usually adapted in research area. The main functions of SDR are GPS signal acquisition, signal tracking, decoding navigation data and calculating stand alone user position from stored data that was down converted and sampled intermediate frequency (IF) data. Each module of SDR platform is categorized by function for applicability for applying for other frequency and GPS signal easily. The developed software platform is tested using stored data which is down-converted and sampled IF data file. The test results present that the software platform calculates user position properly.