• Satellite Communications and Space Industry
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• v.15 no.1
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• pp.94-100
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• 2008

• The Journal of the Korea institute of electronic communication sciences
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• v.13 no.1
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• pp.245-252
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• 2018

In this paper, the dual band circular polarization patch antenna was designed by using band rejection characteristics of CSRR structure for geostationary satellites. A quadrangular CSRR structure was etched on the ground at the rear of the patch antenna's feed to obtain band rejection characteristics in between the receiving frequency band(1525~1559MHz) and transmission band(1626.5~1660.5MHz), and the corner of the patch antenna was truncated to enable circular polarization. It was confirmed that the resonant frequency of the patch antenna differs according to the size anc location of the CSRR and cirular polarization characteristics with simulation and measurement results. Measurement results shows the gain of about 0.2dB and 1.5dB in the TX and RX band.

• Proceedings of the IEEK Conference
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• 2003.07a
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• pp.258-261
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• 2003

한반도와 그 주변 지역에 멀티미디어 서비스를 제공하기 위해 통신방송위성(CBS: Communications and Broadcastings Satellite) 탑재체의 Ku 대역 안테나가 개발되었다. Ku 대역 안테나는 성능 요구 조건을 만족하도록 설계 되었으며 일련의 시험을 통해 성능 검증이 이루어졌다. 일련의 시험은 초기 성능 시험(IFPT: Initial Functional Performance Test), 환경 시험, 최종 성능 시험(FFPT: Final Functional Performance Test)으로 구성되며 이를 통해 반사 손실, EOC(Edge Of Coverage) 이득, 사이드로브 레벨, 교차 편파 분리도등의 전기적 성능과 발사 및 우주 환경에서 강건함이 확인되었다.

• The Journal of the Korea institute of electronic communication sciences
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• v.14 no.5
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• pp.845-852
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• 2019

The main goal of Signal Intelligence (SIGNT) based on a satellite is to collect valid and accurate data without the topographical constraints, but, due to the characteristics of the satellite communication, the collected signals are greatly vulnerable to the influence of interference and jamming signals because their power are very low. Therefore, the high performance techniques of estimating the angle of arrivals (AOAs) of the collected signals and suppressing interference signals are required for collecting various signals on the ground employing the satellite. In addition, the high quality of the transmission beam-forming technique is required for accurately transmitting the collected information to a ground control center. In this paper, we present a beam-forming satellite system based on a circular array antenna, considering the above techniques, and evaluate and analysis the performance of the presented beam-forming system through the computer simulation. The circular array antenna structure is expected to effectively employ for the SIGINT system based on a satellite, because it is suitable to be installed in the satellite.

• Proceedings of the KAIS Fall Conference
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• 2006.05a
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• pp.291-293
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• 2006

본 논문에서는 휴대용 무선통신기기에 장착해서 사용가능한 소형 위성 DMB 안테나를 설계하였다. 안테나 디자인은 QHA(Quadrifilar Helical Antenna)이며 소형화를 위해 안테나 패턴을 유전체위에 감고 각 패턴의 가운데가 분리된 형상을 하고 있다. 시뮬레이션 결과에 따라 안테나가 실제 제작 되고 측정되었다.

• Aerospace Engineering and Technology
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• v.4 no.1
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• pp.103-107
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• 2005

There is an X-band transmission system in KOMPSAT-2 in order to downlink the acquired image data in high speed. KOMPSAT-2 employs a steerable high gain X-band antenna for that purpose. During the ground test, the X-band RF radiation is so strong that it has to be controlled for safety, while spacecraft needs to keep flight configuration. Also in a launch site of which all test facilities are the subjects of strict radiation control, the antenna system should be tested again without any change in the configuration. To limit the actual radiation of RF power, an antenna hat was manufactured and thoroughly tested to demonstrate the spacecraft safety when using it.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.42 no.1
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• pp.90-97
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• 2014

In this paper, we have designed the antenna for Korea SAT-5 Satellite Communication which can use Ka band in the earth station. The antenna structure consist of the the dual-offset gregorian reflector that has high gain and efficiency, the corrugated horn that has symmetric radiation patterns and low side lobe levels, the iris polarizer that make circular polarization and the OrthoMode Transducer that separate transmitting and receiving signals. The designed antenna gain is more than 45.7dBi in Tx-band which use LHCP and 42.0dBi in Rx-band which use RHCP. The co-polarized and cross-polarized radiation pattern comply with ITU-R S.580-6 and S.731-1 that are recommended by International Telecommunication Union in the geostationary satellite. The Axial ratio is less than 1.0dB in Tx-band and 1.5dB in Rx-band that meet MIL-STD-188-164A.

• Information and Communications Magazine
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• v.10 no.4
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• pp.53-62
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• 1993

정지궤도(Geo-Stationary Orbit)상의 통신위성의 정상운용 말미에 경제적 이유 또는 차세대 위성 발사지연등 기술적사유로 설계수명을 지난 후 경사궤도(Inclined Orbit)상의 위성 비정상운용을 개선하기 위하여 경사궤도의 개념, 도플러효과에 따른 지구국 설비 대책 및 INTELSAT 위성궤도 장기 운용계획 등을 조사 고찰한 것이다. 특히 경사궤도가 미치는 영향은 주파수, 안테나크기, 지구국 위도, 위성과 지구국과의 경도간격, 서비스의 디지틀과 애너로구등 다양한 요소를 수식화했다.

• Proceedings of the IEEK Conference
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• 2000.11a
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• pp.97-100
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• 2000

IMT-2000 지상 시스템에서는 순방향 링크의 용량을 증대하기 위하여 다중 전송 안테나를 이용하는 다양한 전송 다이버시티 기법들이 연구되고 있으며, 3GPP를 위한 표준 가운데 하나인 폐쇄루프 전송 다이버시티 기법은 단말기에서 순방향 채널의 상태에 따라 전송 안테나의 가중치를 결정하여 궤환함으로써 여타의 기법에 비해 우수한 성능을 보인다. 하지만 지상 시스템과는 달리 IMT-2000 위성 시스템에서는 현재 전송 다이버시티에 대한 표준이 없는 상황이며 이에 대한 연구 역시 미진하다. 본 논문에서는 폐쇄루프 전송 다이버시티를 IMT-2000 위성 시스템에 적용한 결과를 제시한다. IMT-2000 위성 채널 모델에 대한 모의 실험 결과 2개 안테나를 이용하는 폐쇄루프 전송 다이버시티를 통해 단일 안테나 혹은 2개 안테나 전송 신호의 단순한 다이버시티 결합에 비해 월등한 성능 향상이 가능함을 확인하였다.

• Journal of Satellite, Information and Communications
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• v.7 no.3
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• pp.105-109
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• 2012

In this paper, we developed an adoptable deployment method to the transmitting antennas of a ground based GPS system for aircraft. Aircraft generally uses satellite providing GPS signals for accurate position information, but transfers to ground based GPS signals time to time due to jamming signals or bad weather. The position accuracy of the ground based GPS system is highly dependent on the number and position of the GPS transmitting antennas. In this research, we found an algorism to predict the DOP due to the location of the GPS transmitting antennas and had an accurate DOP 2.5 area into 3-dimension from 0 to 10 km by 12 transmitting antennas.