• Title/Summary/Keyword: Ku Band Satellite

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Ku-Band Dielectric Resonator Bandpass Filter for Satellite Transponder (인공 위성 중계기용 Ku-Band 유전체 공진기 대역 통과 필터)

  • 김상철;이찬주;홍의석
    • Journal of the Korean Institute of Telematics and Electronics A
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    • v.29A no.11
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    • pp.49-56
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    • 1992
  • In this paper a band-pass filter using dielectric resonators with tuning screw and spacer at Ku-band is designed and constructed. For the filter design and construction, the coupling coefficient K between two resonators is numberically evaluated. The external quality factor Q$_{ex}$ is also calculated with a microstrip line which is necessary for the field excitation of dielectric resonator. The coupling between dielectric resonator and microstrip line depends mainly upon the magnetic field and is principal parameter in band-pass filter. The Q$_{ex}$ and K data which are evaluated by numberical analysis are practically applied to the filter construction. The theoretical Band-pass filter responses are given by Chebyshev approximation and they are nearly similar to the experimental results.

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Design of Direct Coupled Combline Filter With Tapped Line in/output For Ku-band Satellite Transponder Downconverter (직접 결합 방식의 Tapped Line 입/출력을 갖는 Ku 대역 위성 중계기 주파수 변환기용 Combline 필터의 설계)

  • 염인복;정근욱;박광량;김재명
    • Journal of the Korean Institute of Telematics and Electronics D
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    • v.34D no.12
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    • pp.22-30
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    • 1997
  • The design procedure for direct coupled combline filter with tapped line in/out was summarized on Ku-band satellite frequency downconverter for stellite application. We calculated the resonator dimensions, spacing between successive resonators, ground plane spacing and tapping position of in/output lines in accordance with the given procedure. Partitions wer eemployed between adjacent resonators by inserting irises to improve filter response characteristis. The designed filter was manufactued with aluminum alloy package to reduce mass, and resonators wer machined from the filter body and in/output lines wer fixed on resonators with epoxy to survive in vibration conditon during launch.

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Design and Fabrication of An LNA for The Reception of The Ku-Band Satellite Broadcast Signals (Ku-대역 위성 방송 수신 시스템을 위한 저잡음 증폭기의 설계 및 제작)

  • 주지한;이석곤;전병태;안병철
    • Proceedings of the IEEK Conference
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    • 2002.06a
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    • pp.451-454
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    • 2002
  • In this paper, a low-noise amplifier is designed and fabricated using the HJFET for the reception of the Ku-band satellite broadcast signals. The optimum input and output reflection coefficients of each amplifier stage are obtained by the trade-off between the stable gain and the noise figure circle. The amplifier performance is simulated and optimized using a microwave CAD software. The designed amplifier is fabricated and tested. Results of the test show a gain of 17.0 dB, a gain flatness of less than $\pm$2.BdB, the noise figure of less than 1.0 dB, and the input and output reflection coefficient of less than -10 dB.

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A Study on the Development of Ku-band Satellite Tracking Antenna System for Ship (선박용 Ku-Band 위성추적형 안테나시스템 개발에 관한 연구)

  • 배정철
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.7 no.6
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    • pp.1146-1152
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    • 2003
  • Satellite television receiving antenna is required for watching TV on the vehicles, ship and car. Recently TV is not only facility as getting information but one of utility in our life. In Korea, already on the service multi-channel satellite TV using excellent visibility and sound, and there are many users using now by fixing antenna. On this thesis, developed ship's satellite TV receiving antenna, the azimuth controlling is adopted azimuth information using gyro sensor and differential of receiving signal strength algorithm, and elevation controlling used gimbals. The result of this research is successfully implemented Korean satellite tracking antenna as performance until ${\pm}$30 degree roll and pitch of ship motion.

Multi-band directional antenna for satellite communications (위성 통신용 다대역 안테나)

  • Cheong, Chi-Hyun;Jeong, Hye-Mi;Kim, Kun-Woo;Bae, Ki-Hyoung;Tae, Hyun-Sik;Evtyushkin, Gennadiy
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.12
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    • pp.1223-1231
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    • 2010
  • The design is presented for a SATCOM antenna capable of simultaneous multi-band (X/Ku/Ka-Band) communications without replacement of feed horns or change of other parts in the application as a ground satellite terminal for large data transfer. The antenna is the offset configuration and consists of a dual-band(X/Ka-band) feed horn, a single-band(Ku-band) feed horn, a frequency selective surface(FSS) sub-reflector and a parabolic main-reflector. The antenna has a main reflector defining a prime focus and a frequency selective surface sub-reflector defining an image focus. A dual-band feed and a single-band feed are provided at each of the prime focus and image focus. The antenna is designed using 3D EM simulator and the gains measured in X/Ku/Ka-band of the complete antenna assembly is more than 31.6dBi, 36.8dBi, 40.8dBi, and the cross polarization is 21.7dB, 26.6dB, 25.2dB, respectively.

Design of Ku-Band BiCMOS Low Noise Amplifier (Ku-대역 BiCMOS 저잡음 증폭기 설계)

  • Chang, Dong-Pil;Yom, In-Bok
    • The Journal of Korean Institute of Electromagnetic Engineering and Science
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    • v.22 no.2
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    • pp.199-207
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    • 2011
  • A Ku-band low noise amplifier has been designed and fabricated by using 0.25 um SiGe BiCMOS process. The developed Ku-band LNA RFIC which has been designed with hetero-junction bipolar transistor(HBT) in the BiCMOS process have noise figure about 2.0 dB and linear gain over 19 dB in the frequency range from 9 GHz to 14 GHz. Optimization technique for p-tap value and electro-magnetic(EM) simulation technique had been used to overcome the inaccuracy in the PDK provided from the foundry service company and to supply the insufficient inductor library. The finally fabricated low noise amplifier of two fabrication runs has been implemented with the size of $0.65\;mm{\times}0.55\;mm$. The pure amplifier circuit layout with the reduced size of $0.4\;mm{\times}0.4\;mm$ without the input and output RF pads and DC bais pads has been incorporated as low noise amplication stages in the multi-function RFIC for the active phased array antenna of Ku-band satellite VSAT.

Development of a Vertical polarized Leaky-wave Waveguide Slot Array Antenna for Receiving the Ku-band Direct Broadcasting Satellite Signals

  • Lim, Gye-Jae
    • Journal of Satellite, Information and Communications
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    • v.2 no.2
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    • pp.10-15
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    • 2007
  • Small size and low profile antenna for mobile vehicular-top-mounted is needed in satellite communication services such as DBS, Satellite Internet and VSAT. In middle latitudes, the development of an array antenna which has the conformal, low profile and 45 degree beam tilted configuration, and has the high gain with sharp beamwidth, low sidelobe and low loss is required for Ku-band satellite communication. In this paper, in order to meet with these performances, an array antenna consisting of the vertical polarized waveguide longitudinal slots based on the leaky-wave mode of traveling wave antenna is proposed. An array antenna consisting of 16 leaky-wave elements is showing 30 dBi of gain, 4.9 degree of beamwidth, below than -20 dB of sidelobe level, 45 degree of beam tilt angle in center frequency. Feed network designed by waveguide cooperated feed shows good performance of wideband and low loss.

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A study on GEO satellite signals in L - to Ka-band affected by Asian Sand Dust

  • Hong Wan-Pyo
    • Journal of information and communication convergence engineering
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    • v.3 no.3
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    • pp.146-151
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    • 2005
  • This paper represents an attempt to bring together and analyses the measurement data measured by the Satellite Signal Monitoring Center in Korea and the Korea Meteorological Administration/Korea Meteorological Research Institute in close cooperation with this study team. This paper presents the signal characteristic of GEO satellite operating in frequency range 1 to 20GHz associated with Asian Sand Dust (the so-called Yellow Sand Dust). The downlink signal power (dBm) for L-, S-, C-, Ku-, and Ka-band frequencies from GEO satellites were measured in a clear weather and in Asian Sand Dust weather by the Satellite Signal Monitoring Center. The measured signal power(dBm) were compared to the total number concentration and size distribution of Sand Dust that were measured by the Korea Meteorological Administration/Korea Meteorological Research Institute and the possible correlation between these sets data were analyzed. The results demonstrate that the downlink signal level (dBm) of GEO satellite is attenuated by Asian Sand Dust. Hitherto, merger information has been reported as to the influence of sand dust on satellite communications operating in regions affected by sand dust.

Design of a Novel low Pass Filler will Low Spurious Response for Satellite Transponder (위성중계기를 위한 낮은 불요 특성을 갖는 새로운 형태의 저역통과 필터 설계)

  • 이문규;류근관;염인복;이성팔
    • Proceedings of the Korea Electromagnetic Engineering Society Conference
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    • 2001.11a
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    • pp.172-175
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    • 2001
  • A novel microstrip type low-pass filter using thin or thick film resistors is proposed to efficiently eliminate harmonic spurious response in stop-band. The proposed low-pass filter shows the spurious suppression enhancement of 20 dB over a conventional one. The designed low-pass filter could be used as a harmonic rejection filter of a local oscillator for Ku-band satellite payload system.

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Frequency Sharing between Multi-beam Mobile Satellite Communication System and Mobile Communication System in 2.1 GHz Band (2.1 GHz 대역 다중빔 이동위성통신 시스템과 이동통신 시스템간 주파수 공유)

  • Jeong, Nam-Ho;Kim, Hee-Wook;Oh, Dae-Sub;Ku, Bon-Jun
    • Journal of Satellite, Information and Communications
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    • v.7 no.1
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    • pp.102-107
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    • 2012
  • In this paper, we presented interference scenarios and an evaluation methodology for the co-frequency radio interference between a multi-beam mobile satellite communication system and a mobile communication system in 2.1 GHz band. Radio interferences between these systems are calculated using a minimum coupling loss method and an assesment for minimum separation distances was conducted for coexistence of a mobile satellite system and a mobile system in the same geographical area.