• Composites Research
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• v.14 no.5
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• pp.20-25
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• 2001

This paper deals with finite element analysis for free vibration and forced sinusoidal vibration of Ka- and Ku- band antenna structures using MSC/NASTRAN. The structures are designed to satisfy minimum resonance frequency requirement in order to decouple the dynamic interaction of the satellite antenna with the spacecraft bus structure. The large mass method was utilized to analyze output acceleration according to the forced sinusoidal vibration inputs in X-, Y- and Z- directions. The analysis results can also be used thor verification experimental planning of satellite antenna.

• Journal of Satellite, Information and Communications
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• v.1 no.2
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• pp.38-44
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• 2006

The COMS(Communication, Ocean & Meteorological Satellite) is the geostationary satellite which will be performing three main objectives such as meteorological service, ocean monitoring and Ka-band satellite communications. In order to accomplish these missions, the COMS system needs to implement a specific electrical/mechanical interface functions which are requested by each payload units. This paper describes a on-board interface hardware design for COMS Meteorological Imager(MI). The Meteorological Imager Interface Unit(MI2U) achieves, through MIL-STD-15533 system bus, the interface between the Spacecraft Computer Unit(SCU) and the instrument which is dedicated to MI. MI2U provides a necessary power input to MI from +50V Power Supply Regulator(PSR), and allows adaptation of the specific payload interfaces and protocol to COMS spacecraft.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2011.05a
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• pp.499-501
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• 2011

The phase noise spectrum distribution of COMS Communication transponder was measured and analyzed in the view point of transmission scheme. The effects of phase noise are also analyzed according to the transmission methods. The phase noise of COMS communication transponder may be increased because of utilization of ka-band. So the effects of phase noise will be increased in conditions of high-order transmission mode. The phase noise characteritics are measured for COMS communication transponder with MSM function and the effects for phase noise are analyzed in this paper.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.23 no.6
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• pp.756-759
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• 2012

This paper presents the multibeam service coverage of GEO(Geostationary Orbit) satellite and the practical antenna scheme scenarios to provide the universal communication services on the Korean peninsula. The proposed antenna systems consist of the simplest scheme and feed network so that they can be mounted on satellites. The feed networks are effectively organized according to the frequency and polarization plan. Despite simple structure, all scenarios meet the electrical performance by the optimization of feed allocation and feed excitation.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.11 no.3
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• pp.345-351
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• 2000

In this paper, we design and analyze a Ka-band microstrip line to rectangular waveguide transition using the expanding-cell FDTD method. The transition under investigation consists of a ridged waveguide, microstrip line, and $\lambda$/4 Chebyshev impedance transformer. To improve the accuracyand efficiency, the expanding-cell FDTD method is applied to analyze the characteristics of a ridged waveguide impedance transformer. To verify the accuracy of the expanding-cell FDTD method, S parameters of the analyzed transition are compared with those of experimental data. The efficiency of the present approach is verified by comparing the computational time for expanding-cell and that for fine cell. The relation between the number of step and operation bandwidth is analyzed by comparing the characteristics of four and three step Chebyshev waveguide impedance transformer.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.19 no.8
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• pp.826-831
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• 2008

This paper presents hybrid antenna(HA) design based on shaped reflector for mobile satellite communication. HA is composed of a shaped reflector and a feeder having $1{\times}8$ linear phased array, and reflector shaping method is applied for the performance optimization with minimum aperture size. And, in the feeder design, HA has another merit to minimize the manufacturing cost by optimizing the number of element. Proposed HA is designed at Ka-band and can electrically control a beam pattern within ${\pm}3^{\circ}$ in the basic angle of $+45^{\circ}$ in elevation. This antenna is designed to meet ITU-R S.465-5 for beam pattern including side-lobe level.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.39 no.3
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• pp.279-288
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• 2011

This paper will discuss the alignment techniques and measurement results of geostationary satellite communication antennas for correct antenna pointing and also the fixtures. To get the best performance in terms of antenna pointing and fixtures, zero G condition have been simulated and laser tracker and theodolite system have been applied. As a result, alignment stability was verified within the tolerance, ${\pm}\;0.25mm$ and ${\pm}\;0.013^{\circ}$ and finally Ka-band deployable antenna alignment has been accomplished within the tolerance, ${\pm}\;0.5mm$ and ${\pm}\;0.015^{\circ}$.

• Current Industrial and Technological Trends in Aerospace
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• v.5 no.1
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• pp.39-55
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• 2007

인류는 달을 보며 우주개발에 대한 꿈을 꾸어왔다. 60년대에서 70년대 중반까지 미 소간의 우주경쟁으로 달 탐사에 큰 예산을 들여 마침내 인류를 달에 착륙시켜 달 탐사를 실현할 수 있었다. 이젠 화성에 인류를 보내기 위한 전초기지를 달에 구축하려고 다시금 미국이 달 탐사를 가동시켰다. 이에 따라 세계 여러 나라가 달에 대해 다시 관심을 고조 시키고 있다. 그래서 이 논문에서는 90년대와 최근에 재 시작된 달 탐사위성의 개발동향을 조사하여 기술하였다. 대상 위성 프로젝트는 미국의 클레멘타인과 루나 프로스펙터, 유럽연합의 스마트-1호, 일본의 셀레네, 중국의 창어-1호, 인도의 찬드라얀-1호, 미국의 LRO 달 탐사 궤도선, 러시아의 루나-글로브 위성들의 주요특성과 탑재체, 지상국, 임무궤적 및 달 임무 궤도에 대해 개괄적으로 기술하였다. 기술 특징으로는 위성 제작기술 발전에 따라 경량화에 중점을 두어 위성을 소형화 하였으며, 통신방식에 있어서는 X 및 Ka대역을 사용하여 데이터 전송속도를 현저히 증가 시켰으며, 위성 및 지상의 안테나의 크기를 줄일 수 있었으며, 전기추력기를 사용하여 소형위성으로도 달 탐사를 실현시켰다. 그리고 다른 나라에서 개발되는 달 탐사위성의 개발 예산을 살펴보면 약 1억불 정도이면 소형 급의 위성을 개발하여 달 궤도에 진입시켜 달 과학탐사 임무를 수행할 수 있다고 할 수 있겠다. 따라서 우리나라도 지난 15년 이상 지구궤도 위성을 성공적으로 개발하며 구축한 기술을 바탕으로 달 탐사 위성의 개발에 대한 가능성을 가지고 있다고 본다. 이제 우리나라도 인류의 미래우주개발의 일익을 담당하고자 달 탐사위성 프로젝트를 준비해야한다

• Journal of the Institute of Electronics Engineers of Korea SD
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• v.45 no.4
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• pp.131-136
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• 2008

Two Ka-band 3-stage power amplifiers were designed and fabricated using $0.18-{\mu}m$ CMOS technology. For low loss matching networks for the amplifiers, two substrate-shielded transmission line structures, having good modeling accuracy up to 40 GHz were used. The measured insertion loss of substrate-shielded microstrip-line (MSL) was 0.5 dB/mm at 27 GHz. A 3-stage CMOS amplifier using substrate-shielded MSL achieved a 14.7-dB small-signal gain and a 14.5-dBm output power at 27 GHz in a compact chip area of 0.83$mm^2$. The measured insertion loss of substrate-shielded coplanar waveguide (CPW) was 1.0 dB/mm at 27 GHz. A 3-stage amplifier using substrate-shielded CPW achieved a 12-dB small-signal gai and a 12.5-dBm output power at 26.5 GHz. This results shows a potential of CMOS technology for low cost short-range wireless communication components and system.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.14 no.12
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• pp.1292-1299
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• 2003

In this paper, we fabricated new GaAs-based dielectric-supported air gapped microstriplines(DAMLs) using the surface MEMS and the LPF for Ka-band using the fabricated DAMLs. We elevated the signal lines from the substrate, in order to reduce the substrate dielectric loss and obtain low losses at millimeter-wave frequency band with wide impedance range. We fabricated LPF with DAMLs for Ka-band. Due to reducing the dielectric loss of DAMLs, the insertion loss of LPF can be reduced. Miniature is essential to integrate LPF with active devices, so that we fabricated LPF with the slot on the ground to reduce the size of the LPF. We compared a characteristic to LPF with the slot and LPF without the slot.