• Journal of Positioning, Navigation, and Timing
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• 제10권4호
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• pp.353-361
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• 2021

This paper presents the jamming effect on the L5 band of Global Navigation Satellite System (GNSS) by analyzing real data collected via measurement campaigns in Korea region. In fact, the L5 band is one of the dedicated bands for various satellite navigation systems such as Global Positioning System (GPS), Galileo, BeiDou (BDS), and Quasi Zenith Satellite System (QZSS). And this band is also allocated along with various systems used for aeronautical radio navigation systems (ARNS). Among ARNS, the Distance Measuring Equipment (DME) and the Tactical Air Navigation System (TACAN) are systems that transmit and receive strong power pulse signals, which may cause unintentional jamming in the reception of GNSS signals. In this paper, signals in the main lobe of GPS L5, Galileo E5a, BDS B2a, and QZSS L5 are collected in Korean region to confirm whether the jamming effect exists in the band. And then, the pulse blanking technique, which is a simple signal processing technique capable of responding to pulsed jamming, is applied to analyze the jamming effect of DME/TACAN on the L5 band.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1991년도 한국자동제어학술회의논문집(국제학술편); KOEX, Seoul; 22-24 Oct. 1991
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• pp.1649-1654
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• 1991

In 1995 the VSOP satellite, which is called MUSES-B in Japan, will be launched under the VLBI Space Observatory Programme(VSOP) promoted by ISAS(Institute of Space and Astronautical Science) of Japan. We are now developing the GPS Receiver(GPSR) and On-board Orbit Determination System. This paper describes the GPS(Global Positioning System), VSOP, GPSR(GPS Receiver system) configuration and the results of the GPS system analysis. The GPSR consists of three GPS antennas and 5 channel receiver package. In the receiver package, there are two 16 bits microprocessing units. The power consumption is 25 Watts in average and the weight is 8.5 kg. Three GPS antennas on board enable GPSR to receive GPS signals from any NAVSTARs(GPS satellites) which are visible. NAVSATR's visibility is described as follows. The VSOP satellite flies from 1, 000 km to 20, 000 km in height on the elliptical orbit around the earth. On the other hand, the orbit of NAVSTARs are nearly circular and about 20, 000 km in height. GPSR can't receive the GPS signals near the apogee, because NAVSTARs transmit the GPS signals through the NAVSTAR's narrow beam antennas directed toward the earth. However near the perigee, GPSR can receive from 12 to 15 GPS signals. More than 4 GPS signals can be received for 40 minutes, which are related to GDOP(Geometric Dillusion Of Precision of selected NAVSTARs). Because there are a lot of visible NAVSTARs, GDOP is small near the perigee. This is a favorqble condition for GPSR. Orbit determination system onboard VSOP satellite consists of a Kalman filter and a precise orbit propagator. Near the perigee, the Kalman filter can eliminate the orbit propagation error using the observed data by GPSR. Except a perigee, precise onboard orbit propagator propagates the orbit, taking into account accelerations such as gravities of the earth, the sun, the moon, and other acceleration caused by the solar pressure. But there remain some amount of calculation and integration errors. When VSOP satellite returns to the perigee, the Kalman filter eliminates the error of the orbit determined by the propagator. After the error is eliminated, VSOP satellite flies out towards an apogee again. The analysis of the orbit determination is performed by the covariance analysis method. Number of the states of the onboard filter is 8. As for a true model, we assume that it is based on the actual error dynamics that include the Selective Availability of GPS called 'SA', having 17 states. Analytical results for position and velocity are tabulated and illustrated, in the sequel. These show that the position and the velocity error are about 40 m and 0.008 m/sec at the perigee, and are about 110 m and 0.012 m/sec at the apogee, respectively.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2005년도 Proceedings of ISRS 2005
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• pp.637-640
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• 2005

In the development of a electronic system for a optical payload comprising mainly EOS(Electro-Optical Sub-system) and PDTS(Payload Data Transmission Sub-system), many aspects should be investigated and discussed for the easy implementation, for th e higher reliability of operation and for the effective ness in cost, size and weight as well as for the secure interface with components of a satellite bus, etc. As important aspects the interfaces between a satellite bus and a payload, and some design features of the CEU(Camera Electronics Unit) inside the payload are described in this paper. Interfaces between a satellite bus and a payload depend considerably on whether t he payload carries the PMU(Payload Management Un it), which functions as main controller of the Payload, or not. With the PMU inside the payload, EOS and PDTS control is performed through the PMU keep ing the least interfaces of control signals and primary power lines, while the EOS and PDTS control is performed directly by the satellite bus components using relatively many control signals when no PMU exists inside the payload. For the CEU design the output channel configurations of panchromatic and multi-spectral bands including the video image data inter face between EOS and PDTS are described conceptually. The timing information control which is also important and necessary to interpret the received image data is described.

• 전기전자학회논문지
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• 제26권2호
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• pp.211-218
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• 2022

본 논문에서는 저궤도 위성 원격측정데이터 신호 수신을 위한 S-대역 위상배열안테나를 제안하였다. 제안된 안테나는 16개의 부배열 조립체, 16개의 능동회로모듈, 수직 급전회로망 및 제어/전원반으로 구성되며 고각 방향으로 빔틸트가 수행된다. 개발된 안테나는 고각 축과 위성 궤적을 일치시키고 개구 중심을 위성 궤적 상의 최대 고각을 바라보도록 하여 정밀한 위성 추적을 수행하였다. 저궤도 위성의 궤적은 위성점 계산을 통하여 정확하게 산출하였다. 위성 추적 시험은 최대 고각을 기준으로 ±30° 범위에서 수행되였다. 위성 추적 시험 결과 최대 고각에서의 S/N비는 16.5 dB이고 Eb/No는 13.3 dB를 얻었다. 수행된 위성 추적 결과는 사전 시스템 분석 결과와 잘 일치함을 확인하였다.

• 대한토목학회논문집
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• 제30권4A호
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• pp.375-382
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• 2010

본 논문은 GNSS 데이터를 이용한 사장교의 고유진동수와 모드형상 추출을 다루고 있다. 서해대교 사장교에 설치된 6개의 GNSS 측정점으로부터 응답신호를 얻어 동특성 분석에 사용하였다. 측정된 GNSS 신호에 대해 정규화 과정과 버터워스 필터를 사용하여 관심영역의 신호를 분리한 뒤, 이중 미분을 수행하여 가속도 데이터로 변환하였다. 변환된 가속도에 대한 FFT 분석을 통해 5개의 고유진동수를 추출하였으며, 이를 기존 연구결과와 비교 검증하였다. 또한 TDD기법을 이용하여 GNSS 데이터로부터 교량의 모드형상까지 추출할 수 있었다.

• Journal of Electrical Engineering and Technology
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• 제13권5호
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• pp.2004-2010
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• 2018

We propose a small active antenna to receive Global Navigation Satellite System (GNSS) signals, i.e., Global Positioning System (GPS) L1 (1,575MHz) and Russian Global Navigation Satellite System (GLONASS) L1 (1,600 MHz) signals. A two-stage low-noise amplifier (LNA) with more than 27 dB gain is implemented in the bottom layer of a three-layer antenna package. In addition, a hybrid coupler is used to combine signals from pair of proximately coupled orthogonal feeds with $90^{\circ}$ phase difference to achieve the circular polarization (CP) characteristic. Three layers of high permittivity (${\varepsilon}_r=10$) substrates are stacked and effectively integrated to have a small dimension of $64mm{\times}64mm{\times}7.42mm$ (including both circuit and antenna). The reflection coefficient of the fabricated antenna at the target frequency is below -10 dB, the measured antenna gain is above 26 dBic and the measured noise figure is less than 1.4 dB.

• 한국전자파학회논문지
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• 제17권9호
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• pp.795-803
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• 2006

본 논문에서는 Ka 대역 초고속 위성 방송 시스템에서 강우 감쇠에 대처하면서 가입자에게 지속적으로 방송을 제공하기 위해 unequal error protection(UEP) 방식을 이용한 계층적 부호화 방식에 대한 연구를 하였다. 신호의 중요도에 따라 변조 방식 및 채널 코딩 방식을 달리하는 time sharing 방식과 달리 하나의 변조 방식을 이용하여 성상도 위치에서 신호의 중요도에 따라 신호간의 최소 거리를 다르게 배치하는 UEP 방식에 대한 구조 및 성능을 분석하였으며, 성능 분석을 토대로 최적의 방식을 제시하였다.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 2002년도 하계종합학술대회 논문집(2)
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• pp.337-340
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• 2002

In data transmission at the digital satellite broadcasting systems, the delay and spread are caused whit receiving original signals from the transmitter in the receiver. So, there are some problems in data fast transmission. Also, transmitted signals ate received in stale of the combination of transmission delay and noise of channel. The affect of channel noise is reduced when increasing transmission power, but as signal interference due to the transmission delay and spread of channel increase in proportion to the transmission power, there is a problem in spite of increasing the transmission power. And there is the problem to add ISI(inter symbol interference) because the property of the channel is limo-varying due to relative moving in the transceiver Therefore, in this paper, a pulse shaping filter for the high-speed service in digital satellite broadcasting systems was designed and reduced the ISI.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.1015-1017
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• 2003

Recently, DGPS or RTK-GPS techniques enable us to use satellite based positioning systems with high accuracy. But in urban area, navigation systems suffer from problems such as signal blockage by high-rise buildings, multi-path problems, and so on. So we have to know numbers of visible satellites and quality of signals received at the ground level in urban area as accurate as possible. In this paper, we developed a simulation system called LoQAS [Location service Quality Assessment System, 2002, the University of Tokyo] which can simulate numbers of visible satellites and DOP values using accurate satellite orbital data and 3-D digital map. In this time, we evaluated this system and extended it to deal with reflected signals to assess multi-path problems.

• 한국위성정보통신학회논문지
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• 제11권2호
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• pp.18-22
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• 2016

본 논문에서는 백스캐터 통신 주파수의 검파한 에너지의 평균을 이용하여 신호를 판단하는 법을 제안한다. Bistatic scatter radio 구조에 해당 모델을 적용시켜 Radio Frequency(RF) 에너지 하베스팅을 수행한다. RF 에너지 전송 시 태그가 모든 RF 신호를 하나의 Frequency Shift Keying(FSK) 대역폭으로 모두 반사하여, 수신기에서 하베스팅 신호와 백스캐터 신호의 차이를 판별할 수 있게 된다. 수신기는 이를 이용해 최적의 안테나 선택을 할 수 있다. 시뮬레이션을 통해 적절한 파라미터 설정을 통해 효과적으로 신호를 검출할 수 있는 것을 확인하였다.