• Title/Summary/Keyword: Dual-offset Gregorian

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Design of Offset Dual-Shaped Reflector Systems for Compact Antenna Test Range (콤팩트 안테나 테스트 레인지용 경면수정 오프셋 복반사경 시스템의 설계)

  • Noh, Sung-Min;Choi, Hak-Keun;Lim, Sung-Bin
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.19 no.4
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    • pp.451-460
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    • 2008
  • Gregorian offset dual-shaped reflector antennas have been widely used in the satellite communication systems for their high gain and low sidelobe characteristics. However, in this paper, it is designed as the CATR(Compact Antenna Test Range) reflector system, and its near-field characteristics are investigated. The CATR facility needs to provide an uniform plane wave with the minimum amplitude and phase ripple and the low cross polarization to the test region. Therefore, the reflector near-field patterns are calculated and presented with the variations of the aperture power distribution, the feed horn pattern, and the distance from the aperture to the test zone. Also, the offset dual-shaped reflector is fabricated at 30 GHz, and its near-field patterns are measured. The measured results are in good agreement with the calculated results. From theses results, we confirm that the designed offset dual-shaped reflector can be used as the reflector system for the compact antenna test range.

The Design of Elliptical Dual Offset Gregorian Antenna for Satellite Communication on Ka-band (Ka대역 위성통신용 타원형 이중옵셋 그레고리안 안테나 설계)

  • Kim, Chun-Won;Cheong, Chi-Hyun;Kim, Kun-Woo;Lee, Seong-Jae
    • Journal of the Korea Institute of Military Science and Technology
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    • v.16 no.6
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    • pp.811-818
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    • 2013
  • In this paper, we have designed the elliptical dual offset gregorian antenna which can use Ka band earth station antennas in the fixed-satellite service. The structure of antenna is increasing the antenna gain by decreasing blockage areas and decreasing wind effects by shortening height of the antenna. The corrugate horn antenna for this antenna has symmetric radiation patterns and low side lobe levels that can meet ITU-R envelope. The distribution of electric field on a aperture of main reflector is calculated by an ray-tracing method that use the radiation pattern of the feed horn. The final geometric of antena is decided by choosing the distribution that comply with antenna requirement. The FEKO analysed electrical performance of this antenna. The fabricated antenna has 45.0dBi(@30.0GHz)/41.7dBi(@20.2GHz), high efficiency and low side lobe level that meet ITU-R S. 580-6 envelope.

Analysis of a Shaped Dual Offset Reflector Antenna-I : Subreflector Analysis (수정곡면 옵셉 복 반사판 안테나의 복사특성 해석-I : 부반사판 해석)

  • 임규태;이상설
    • Journal of the Korean Institute of Telematics and Electronics A
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    • v.32A no.9
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    • pp.106-113
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    • 1995
  • The radiation characteristics of the subreflector of a shaped dual offset reflector antenna are analyzed by the uniform theory of diffraction(UTD). The discrete shaped subreflector profile is transformed into an analytic function by the global interpolation. To obtain the first and the second derivative terms on the surface, the local interpolation method is used. The reflection point needed for the geometrical optics(GO) is found by using the multi-dimensional function minimizing algorithm. The radiation pattern of a Gregorian type shaped subreflector is presented. The characteristics of the radiation patterns for various feed edge taperings and frequencies are examined.

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An Antenna & RF System for Fly-away Satcom Terminal Application on Ka-band (Ka대역 위성통신용 fly-away 터미널 안테나 & RF 시스템 설계)

  • Park, Byungjun;Kim, Chunwon;Yoon, Wonsang;Lee, SeongJae
    • Journal of the Korea Institute of Military Science and Technology
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    • v.17 no.4
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    • pp.485-491
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    • 2014
  • An Antenna & RF system for a fly-away satcom terminal application on ka-band is presented in this paper. The Fly-away satellite terminal can be moved and operated by two person and adapt automatic satellite tracking system in order to decrease the tracking time. Additionally, for low-power consumption, compact size and light-weight, a dual reflector antenna is constructed using dual-offset gregorian antenna structure. For minimize weight, the reflector of the antenna is made of Magnesium. For low-power consumption and light-weight, the pHEMT MMIC compound devices is utilized. The Electronic Band-Gap(EBG) Low-Pass Filter(LPF) is designed for harmonic rejection. In the receiving part, Low-Noise Block converter(LNB) structure is designed for compact and lightweight. In this paper, fly-away satcom terminal with low-power consumption, compact size and light-weight is described with antenna system and RF system performances. Through the experimentation, fly-away terminal's EIRP is more than 50dBW, G/T is more than $17dB/^{\circ}K$.

The Antenna Design for Korea SAT-5 Satellite Communication in Ka-band (무궁화 5호 위성통신용 Ka대역 안테나 설계)

  • Kim, Chun-Won;Cheong, Chi-Hyun;Kim, Kun-Woo;Lee, Seong-Jae
    • 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.

Transmitter Design for Earth Station Terminal Operating with Military Geostationary Satellites on Ka-band (Ka 대역 군위성통신 지상단말 송신기 설계)

  • Kim, Chun-Won;Park, Byung-Jun;Yoon, Won-Sang;Lee, Seong-Jae
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.25 no.4
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    • pp.393-400
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    • 2014
  • In this paper, we have designed the transmitter for earth station terminal operating with military geostationary satellite on Ka-band that is complied with MIL-STD-188-164A. The designed antenna of this terminal is dual-offset gregorian reflector which is consist of corrugated horn and iris polarizer, othermode transducer. This antenna meets radiation pattern and transmit EIRP spectral density requirements in this standard. The designed RF systems of this terminal are consist of Block Up Converter(BUC) converting frequency band from IF to Ka band and SSPA having low-power consumption and compact light-weight using the pHEMT MMIC compound devices. This RF systems applied with VSWR, spurious/harmonic suppression, output flatness and phase noise requirement in this standard.