• The Proceeding of the Korean Institute of Electromagnetic Engineering and Science
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• v.14 no.2
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• pp.55-67
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• 2003

본 고에서는 차세대 무선통신용 초소형 단말기 구현에서 RF 시스템의 성능 개선에 크게 기여하게 될 RF 집적형 안테나 기술 현황과 향후 발전 방향이 제시된다. 고성능을 유지하면서 초소형 RF 전치단을 실현하기 위한 능동소자와 안테나가 결합하여 복합 기능을 하는 능동 집적 안테나(AIA, Active Integrated Antenna) 기술 현황, RF 시스템 단일 패키지(RF-SOP, System On Package) 형태에 집적 가능한 안테나 및 미래의 꿈인 RF 시스템 단일 칩 (RF-SOC, System On Chip)을 향한 단일 칩 안테나 (AOC, antenna on chip) 기술 동향 등이 기술된다.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.24 no.10
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• pp.994-1000
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• 2013

Conventional MIMO system is required to a number of RF chains as much as a number of antennas. If the number of antennas increased then the number of RF chains increased. Therefore, it is difficult to apply conventional MIMO system to mobile terminals with limited power. In this paper, we propose a TDM(time division multiplexing)-based single RF chain MIMO system. The outcome shows that performance of the proposed system is similar to conventional MIMO system using multiple RF chains when STO is corrected by phase angle estimation and the synchronizing signal of received signal. Therefore, it is possible to implement the MIMO-OFDM system of low power and complexity through a single RF chain.

• Proceedings of the Korean Vacuum Society Conference
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• 2010.08a
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• pp.133-133
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• 2010

중성입자빔 입사장치(neutral beam injection, NBI)의 중성빔 에너지 효율은 이온원의 수소 이온밀도 분율이 결정한다. 이온원에서 만들어진 $H^+$, $H_2^+$ 그리고 ${H_3}^+$는 중성화 과정(neutralization) 중 해리(dissociation) 때문에 각각 입사 에너지의 1, 1/2 그리고 1/3을 가진 중성입자가 된다. 중성빔 에너지 효율 제고하기 위해서는 이온원의 전체 이온 중 단원자 수소 이온 밀도 증가가 필요하다. 유도결합형 수소 플라즈마 이온원에서 RF 안테나 주파수에 따른 플라즈마 밀도와 단원자 수소 이온 밀도 비율 변화를 관찰하였다. RF 플라즈마에서 가스 압력이 결정하는 전자의 운동량 전달 충돌 주파수 대비 높은 RF 안테나 주파수(13.56 MHz)와 낮은 RF 안테나 주파수(수백 kHz)의 전력을 인가하였으며, Langmuir 탐침, 안테나 V-I 측정기 그리고 QMS(quadrupole mass spectrometer)을 이용하여 플라즈마 특성을 진단하였다. 플라즈마 밀도와 수소 이온 밀도 분율은 플라즈마 가열 메커니즘과 수소 플라즈마 내 반응 메커니즘에 의해 결정된다. 플라즈마 가열 메커니즘에 따른 실험 결과에 대한 RF 안테나 주파수 효과는 플라즈마 트랜스포머 회로 모델을 통해 해석하였으며, 수소 플라즈마 내 반응은 0-D 정상 상태의 입자 및 전력 평형 방정식 결과로 해석하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.5
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• pp.409-416
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• 2017

In order that multiple wideband RF transmitters which have mission to deliver essential information to aircraft operate at the same time, RF transmitter has a variable sub-carrier frequency to modulate the signal. In case of exposure to weak environment, Wide-band RF transmitter is designed to check component of transmitter that includes antenna BIT to increase system reliability. Normally, Antenna BIT measure the reflection RF power of antenna to check system condition. However, Antenna BIT has a difference that depends on testing frequency to use the long RF cable which is located between the power amp and the antenna. The periodic phenomenon of the reflected antenna power are theoretically explained about dependence on the RF cable length. Based on presented result, suggested measurement methods is effectively able to be applied to diagnosis system condition.

• The Journal of the Institute of Internet, Broadcasting and Communication
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• v.11 no.3
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• pp.1-8
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• 2011

In this paper, data transmission corrugated horn antenna for RF sensor satellite system and its radiation characteristic are presented. The proposed antenna is designed, fabricated and measured to obtain the maximum gain at ${\pm}60^{\circ}$ of its radiation patterns. The result of the proposed antenna is that the return loss is less than -15 dB and the gain is over 5 dBi at ${\pm}60^{\circ}$ of its radiation patterns. From these results, it is confirmed that the proposed can be used as data transmission corrugated horn antenna for RF sensor satellite system.

• The Journal of Korean Institute of Communications and Information Sciences
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• v.39A no.2
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• pp.69-76
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• 2014

Multiple-input and multiple-output (MIMO) technique is used in many communication fields in order to increase the channel capacity. However, this MIMO system has difficulty of miniaturization of antenna size due to the multiple RF chains Also, multiple RF chain raises some problems which increase power consumption at RF circuit and degrade the system performance due to the interference between RF chains. Because of these reasons, beamspace MIMO (BS-MIMO) technique with only single RF chain was proposed for MIMO transmission. This BS-MIMO system basically uses electronically steerable parasitic array radiator (ESPAR) antenna. Existing ESPAR antenna has a 5-element structure. So, it is possible to do only $3{\times}3$ MIMO transmission. Therefore, in order to extend BS-MIMO dimension, extension of ESPAR antenna structure is essential. In this paper, we show that BS-MIMO dimension can be increased according to the extension of structure of the ESPAR antenna, as in the conventional MIMO techniques. For example, we show that it is possible to design the $7{\times}7$ BS-MIMO transmissions with the 13-element ESPAR antenna. Also, when the number of parasitic elements of ESPAR antenna increases by two elements, MIMO dimension is expanded by 1.

• 전자공학회논문지 IE
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• v.47 no.1
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• pp.34-40
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• 2010

Even if use ICS repeater in radio communication system, distance between Donor antenna and Service antenna though do much isolation degree must that shortcoming have. Proposed IP antenna to supplement this shortcoming in this paper. Result Doner antenna and isolation of Service antenna that measure through examination do 1.5m and when did direction 180 degree, Isolation confirmed that is measured 110dB. Confirmed that can unuse ICS repeater through this result and service by general RF repeater.

• Journal of the Korean Vacuum Society
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• v.15 no.3
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• pp.314-324
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• 2006

The vacuum characteristics of the KSTAR ICRF antenna were experimentally investigated. The fabricated antenna was installed in the RF Test Chamber(RFTC) which has a vacuum system with an effective pumping speed of 1015 l/s. The time variations of RFTC pressure, total gas load and ultimate pressure were measured before the RF test. RF conditioning effect was studied by repeating RF pulses at low power level. A time variation of the RFTC pressure was measured during a RF power was applied to the antenna. Threshold pressure at which a RF breakdown occurs was investigated. Whenever the pressure was higher than $10^{-4}$ mbar, the RF breakdown occurred. During a long pulse testing, the temperature of the antenna and RFTC pressure were measured to investigate long pulse limitation of the maximum available voltage without any cooling, which were compared with testing results with a water cooling of the antenna.

• Journal of Space Technology and Applications
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• v.1 no.3
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• pp.364-374
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• 2021

This research discusses the change in radio frequency (RF) characteristics according to the number of Gores on the deployable mesh antennas for potential micro-satellite applications. The deployable type of lightweight mesh antenna can be used for various space missions such as communication/SAR/ SIGINT. In order to implement an ideal curvature of antenna surface, sufficient number of antenna rib structures are required. However, the increase in antenna ribs affects various design factors of the antenna system, especially total system mass, complexity of deployable mechanism and reliability. In this paper, the proper number of ribs for the mesh antenna were derived by comparison of electro-magnetic (EM) simulation results of example of antenna model in accordance with the various number of ribs.

• 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.