• 한국전자파학회논문지
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• 제16권10호
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• pp.1043-1049
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• 2005

대용량 고속 광대역 전송에 적합한 OFDM(Orthogonal Frequency-Division Multiplexing) 통신 시스템에서 위상 잡음에 의해 발생하는 ICI(Inter-Sub-Carrier-Interference)는 부반송파 사이의 직교성을 깨뜨려 시스템 성능을 현저히 저하시킨다. 본 논문에서는 ICI 제거 기 법과 안테나, 시간, 주파수 다이버시티를 혼합한 새로운 STFBC(Space Time Frequency Block Coding) 방법을 이용하여 ICI를 효과적으로 제거한다. 먼저 위상잡음 선형 근사화 기법을 이용하여 제안한 STFBC OFDM 시스템에서 발생하는 CPE(Common Phase Error) 성분과 ICI 성분을 분석하고 PLL(Phase Locked Loop) 위상잡음에 의해 발생하는 시스템 성능 저하를 비교 분석하기 위하여 CIR(Carrier to Interference Ratio), PICR(Peak Interference to Carrier power Ratio) 그리고 BER(Bit Error Rate)을 토론한다. 분석 결과 제안한 STFBC 방법에서는 ICI를 뚜렷이 제거할 뿐만 아니라 기존의 STBC(Space Time Block Coding), SFBC(Space Frequency Block Coding) 등 다이버시티 코딩 기법에서 나타나는 SCI(Self Channel Interference)를 효과적으로 피면할 수 있다.

• 대한전자공학회:학술대회논문집
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• 대한전자공학회 1999년도 하계종합학술대회 논문집
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• pp.978-981
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• 1999

In this paper, an improved integer-N frequency synthesizer that can be synthesized into smaller channel space than input signal frequency is presented. The proposed frequency synthesizer also has an characteristics of fast phase locking time. The frequency synthesizer performed in the manner that it divides various outputs of different phases in VCO by means of dividers that have different control signals respectively and then add the divided signal. In order to confirm the characteristics of proposed frequency synthesizer, behavioral and SPICE simulations are performed using C-language and HSPICE respectively.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2003년도 한국우주과학회보 제12권2호
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• pp.48-48
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• 2003

A precision orbit determination (POD) system of low Earth orbiter using the GPS dual frequency measurements has been developed. It is an option of KOMPSAT-2 POD process system. In this research, the orbit determination using the real dual frequency carrier phase measurements of the SAC-C satellite was conducted to verify KOMPSAT-2 POD system reliability. The SAC-C satellite is an international cooperative mission between NASA, the Argentine Commission on Space Activities (CONAE), Centre National d'Etudes Spatiales (CNES or the French Space Agency), Instituto Nacional De Pesquisas Espaciais (Brazilian Space Agency), Danish Space Research Institute, and Agenzia Spaziale Italiana (Italian Space Agency). The SAC-C was launched at November 21, 2000. The altitude of SAC-C is 702 km and it carries a TurboRogue III GPS and four high gain antennas developed by the JPL. The receiver is able to generate the dual frequency code and carrier phase data. Double-differenced carrier phase measurements were formed using 25 IGS stations. The data were sampled at 30 seconds interval. Fully dynamic approach was adopted for POD. The POD results were compared with those of JPL using GOA n software. The comparison verifies that deci-meter level 3D position accuracy of low Earth orbiting satellite could be achieved. The POD system has been developed successfully.

• 천문학논총
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• 제30권2호
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• pp.629-631
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• 2015

In this proceedings, preliminary results of the KVN Source-Frequency Phase-Referencing (SFPR) observation of 3C 66A and 3C 66B are presented. The motivation of this work is to measure the core-shift of these 2 sources and study the temporal evolution of the jet opacity. Two more sources were observed as secondary reference calibrators and each source was observed at 22, 43, and 86 GHz simultaneously. Our preliminary results show that after using the observations at the lower frequency to calibrate those at the higher frequency of the same source, the residual visibility phases for each source at the higher frequencies became more aligned, and the coherence time became much longer; also, the residual phases for different sources, within 10 degrees angular separations, follow similar trends. After reference to the nearby calibrator, the SFPRed maps were obtained as well as the astrometric measurements, i.e. the combined coreshift. The measurements were found to be affected by structural blending effects because of the large beamsize of KVN, but this can be corrected with higher resolution maps (e.g. KAVA maps).

• Journal of Astronomy and Space Sciences
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• 제27권3호
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• pp.239-244
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• 2010

A simulation for the design of a $90^{\circ}$ differential phase shifter aimed toward Korean VLBI Network (KVN) 129 GHz band polarizer is described in this paper. A dual-circular polarizer for KVN 129 GHz band consists of a $90^{\circ}$ differential phase shifter and an orthomode transducer. The differential phase shifter is made up of a square waveguide with two opposite walls loaded with corrugations. Three-dimensional electromagnetic simulation has been performed to predict the $90^{\circ}$ differential phase shifter's characteristics. The simulation for the differential phase shifter shows that the phase shift is $90^{\circ}{\pm}3.3^{\circ}$ across 108-160 GHz and the return losses of two orthogonal modes are better than -30 dB within the design frequency band. According to the simulation results the calculated performance is quite encouraging for KVN 129 GHz band application.

• 전력전자학회논문지
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• 제8권3호
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• pp.230-238
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• 2003

본 연구에서는 3상 SRP-PWM기법을 2상에 적용한 고정 스위칭 주파수의 공간벡터 SRP-PWM(Separately Randomized Pulse Position PWM)기법을 제안하고 이를 산업현장에 적용 가능한가를 검증하기 위하여, 속도 피드백 실험을 행하였다. 제안된 2상 SRP-PWM은 랜덤하게 배치된 a상의 펄스 범위 내에서 나머지 상의 펄스 위치를 완전히 랜덤하게 배치 할 수 있는 변조기법이다. 제안된 방법이 적용된 속도 피드백 시스템은 부하와 연결된 3상 유도모터의 v/f 일정 제어를 기반으로 하였다. 실험 결과, 제안된 방법이 적용된 기존의 2상 중앙정렬 SVM의 경우와 비교하여 모터의 v/f 일정 제어의 성능은 동일함을 확인할 수 있었으며, 모터의 전압 및 소음 스펙트럼의 광대역화 효과는 제안된 방법이 훨씬 우수함을 입증할 수 있었다.

• 천문학회보
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• 제41권1호
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• pp.74.2-74.2
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• 2016

It is important to know how well observation errors are removed in the calibration process prior to ensuing scientific research. In mm-VLBI observations, a radio wave suffers from an atmospheric propagation delay due to the rapid change of atmospheric refraction. It makes phases of VLBI correlation output fluctuate rapidly, which essentially decreases the coherence of phases and reduces the integration time. Consequently, it is challenging to achieve a high signal-to-noise ratio and enhance the quality of scientific output. Among the causes of the atmospheric propagation delay, water vapor in the troposphere is the most decisive factor to affect phase errors in the high frequency range (> 10GHz). It is expected to have the non-dispersive characteristic that enables to introduce new calibration strategy, Frequency Phase Transfer (FPT). This new method utilizes low frequency phases to compensate phase errors in high frequency bands. In addition, Korean VLBI Network (KVN) which benefits from the simultaneous 4-channels (22/43/86/129 GHz) observations is ideal to probe FPT performance. In order to evaluate FPT performance of KVN, we present the results of FPT phase analysis and discuss its performance.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2004년도 학술대회 논문집 정보 및 제어부문
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• pp.705-707
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• 2004

In this paper, we propose a robust control technique against parameter uncertainties as well as external disturbances. It is robust control scheme using discrete-time state space disturbance observer. It does not require disturbance modeling, plant inverse modeling and/or Q filter. In frequency domain, its performance is evaluated in terms of sensitivity and complementary sensitivity as well as gain and phase margin. Finally we discuss design criterion of state space disturbance observer considering its performance in frequency domain.

• International Journal of Computer Science & Network Security
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• 제21권2호
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• pp.40-43
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• 2021

In the article of instability on the peak power level, duration and repetition period of a multifrequency space-time signal, we calculated the maximum values of the errors of the parameters of the laws of spatial-phase-frequency control. Requirements for the accuracy of the location of the phase centers of the emitters in a cylindrical phased array antenna with pyramidal horns; it is advisable to calculate the radiation field using single-stage and multi-stage distribution laws. The phase centers of individual radiation sources of a cylindrical phased array antenna have been studied; they have almost no effect on the duration and period of recurrence.

• 한국초전도ㆍ저온공학회논문지
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• 제5권1호
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• pp.111-117
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• 2003

In the design of the split type free displacer Stilting cryocooler the motion of the displacer is very important to decide the cooling capacity, which depends upon the working gas pressure, the swept volume in the compression space and the expansion space, operating frequency, the phase shift between piston and displacer, etc. In this study, Stirling cryocooler actuated by the electric farce of the dual linear motor is designed and manufactured. Cool down characteristics of the cold end with laser displacement sensor in the expander of the Stilting cryocooler is evaluated. The charging pressure was 15kg$_{f}$/$\textrm{cm}^2$ and operating frequency was 50Hz. Input power and the lowest temperature were about 32W and 67K, respectively. And, displacement of the piston is measured by LVDTs (Linear Variable Differential Transformers), displacement of thedisplacer is measured by laser optic method, and phase shift between piston and displacer is discussed. As the peak-to-peak pressure of the compressor was increased, peak-to-peak displacement of the displacer was increased. The peak-to-peak displacement of the displacer increases in the range of 0 - 64.5Hz(resonant frequency of the displacer), but decreases steeply when the operating frequency is bigger than the resonant frequency. Finally when the phase shift between displacements of the Piston and displacer is 45。, operating frequency is optimum and is decided by resonant frequency of the expander, mass and cross section area of the displacer and constant by friction and flow resistance.e.