• 한국전자파학회논문지
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• 제21권11호
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• pp.1304-1310
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• 2010

낮은 고도로 접근하는 고속 표적을 탐지 및 추적하기 위해 사용하는 K 대역의 FMCW(Frequency Modulated Continuous Wave) 레이다의 송수신기 설계 방법을 제안한다. 송신기는 레이다 유효 반사 면적(RCS : Radar Cross Section)이 작은 표적의 추적 및 넓은 송신 안테나 빔 폭으로 인해 고출력이 요구되며, 수신기의 경우는 인터페로메타 방법을 이용하여 표적을 추적하기 위해 다채널 수신기가 요구된다. 송신기는 고출력 송신 증폭기와 도파관 스위치 및 주파수 상향 변환 기판으로 구성된다. 수신기는 5 채널 수신기, 중간 주파수 상향 및 하향 변환 모듈, X 대역 국부 발진기 및 파형 발생 모듈로 세분화 할 수 있다. 제안한 구조를 제작하기 전에 모델링 및 시뮬레이션 방법을 통해 여러 파라메타를 측정함으로써 가능성을 입증한다. 그리고 제안한 송수신기를 산업용 부품을 사용하여 제작하고 성능 파라메타를 측정하였다. 그 결과, 송신기 출력은 39.64 dBm, 수신기 이득은 29.1 dB이며, 그 외 모든 설계 요구 조건을 만족함을 입증하였다.

• 대한기계학회논문집A
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• 제37권6호
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• pp.805-814
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• 2013

유압식 Dipod 플랫폼은 기동차량에서 위성을 지향하는 안테나의 안정화 및 추적에 사용된다. 이러한 플랜트의 제어기 설계에는 외란제거와 추적 두 가지 성능목표 뿐만 아니라 강인성을 함께 절충해야 하는 제약조건으로 인해 1자유도 제어기에 비해 설계 유연성이 큰 2자유도 $H_{\infty}$ 제어기가 선호된다. $H_{\infty}$ 기반한 2자유도 제어기 종합방법에는 두 가지 프레임웍이 사용되는데 유압식 Dipod 플랫폼의 예를 통해서 일괄종합 방법이 더 우수한 성능을 보인 반면 분리종합 방법은 더 우수한 강인성을 보임을 확인할 수 있었다. $H_{\infty}$ 2자유도 종합방법에 따른 이러한 두 결과의 차이를 시스템 정합행렬의 구조화 특성을 통해 비교하여 보았다.

• Journal of Astronomy and Space Sciences
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• 제36권4호
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• pp.293-306
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• 2019

In this study, the observational arc-length effect on orbit determination (OD) for the Korea Pathfinder Lunar Orbiter (KPLO) in the Earth-Moon Transfer phase was investigated. For the OD, we employed a sequential estimation using the extended Kalman filter and a fixed-point smoother. The mission periods, comprised between the perigee maneuvers (PM) and the lunar orbit insertion (LOI) maneuver in a 3.5 phasing loop of the KPLO, was the primary target. The total period was divided into three phases: launch-PM1, PM1-PM3, and PM3-LOI. The Doppler and range data obtained from three tracking stations [included in the deep space network (DSN) and Korea Deep Space Antenna (KDSA)] were utilized for the OD. Six arc-length cases (24 hrs, 48 hrs, 60 hrs, 3 days, 4 days, and 5 days) were considered for the arc-length effect investigation. In order to evaluate the OD accuracy, we analyzed the position uncertainties, the precision of orbit overlaps, and the position differences between true and estimated trajectories. The maximum performance of 3-day OD approach was observed in the case of stable flight dynamics operations and robust navigation capability. This study provides a guideline for the flight dynamics operations of the KPLO in the trans-lunar phase.

• 전기학회논문지
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• 제59권1호
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• pp.144-151
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• 2010

The shadowing effects lead to the serious power losses of the PV module. The shadowing effects are caused by several factors such as leafs, dust, antenna and clouds. The dye-sensitized solar cells are more economical than the conventional silicon solar cell that's why the dye-sensitized solar cells are recently focused on. We carried out research on the efficiency of the dye-sensitized solar cell depending on the level of shadow changing the formula of the circuit. The research on the efficiency of the large dye-sensitized solar cell depending on the level of shadow focused on commercialization was carried out. As the results, it is known that the series and parallel connection method is the best choice for the least losses of PV module assemblies. It is especially known that one more series connection is the best choice for the least losses about shadowing effects and current losses in the series and parallel connection.

• 한국전자파학회논문지
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• 제21권5호
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• pp.528-536
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• 2010

모노펄스 급전기는 공간 급전 방식을 사용하는 다기능 레이더 또는 추적 레이더의 복사 패턴 특성에 가장 큰 영향을 미친다. 세 개의 모노펄스 채널에 대해 최적 개구면 분포를 가지는 삼중 모드 방식 모노펄스 급전기의 설계 및 측정 결과에 관해 본 논문에 기술하였다. 측정 결과 설계 및 제작된 급전기는 최적 개구면 분포 특성을 만족할 뿐만 아니라 X-대역의 10 % 대역폭에서 매우 낮은 반사 손실 특성을 보였다. 급전기의 이러한 특성은 적용될 안테나가 저부엽 특성과 높은 모노펄스 기울기 특성을 보유함을 의미한다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1994년도 Proceedings of the Korea Automatic Control Conference, 9th (KACC) ; Taejeon, Korea; 17-20 Oct. 1994
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• pp.38-43
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• 1994

To provide more instructive and a safer ground control operation environments for satellite operators, and subsequently to implement a better look-and-feel user interface and a structural mechanism to enhance the efficiency of control and monitoring facilities, we have developed a prototype(laboratory model) ground control softwares targeting for the first generation KOREASAT scheduled to be launched in 1995. As far as the functionality is concerned, the developed system is covering almost all the mission phase operational functions except for some functions like antenna tracking control that are necessary for real operation environments. Most of the functions of the system is realized in softwares but some hardwares needed for TM/TC RF communications are also included in it. The system is now being integrated and under the system test. The performance and functionality is to be evaluated by the end of this year by using the satellite software simulator. Next year, this system could be configured to be used as a workbench for a online/off-line analysis of the operating KOREASAT satellites.

• 반도체디스플레이기술학회지
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• 제14권2호
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• pp.9-16
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• 2015

In this paper, selection criterions on selection diversity are researched. The diversity is applied to the multiple antenna system based on wireless access in vehicular environment (WAVE) standard for rapid varying channel. Least squares (LS) based decision feedback equalizer (DFE) are used for channel equalization. Received signal is regenerated by means of the decision feedback path. In the selection diversity, the regenerated signal as well as the received signal is selected according to selection criterion. The decision feedback algorithm can follow the fast speed of WAVE fading channel. To control the tracking speed of the time-varying channel, simple low pass filter is used. Finally, the estimated channel value recovers the distorted payloads. Signal power before automatic gain control (AGC) in analog stage can be used as a selection criterion. In the digital stage, signal power after AGC, noise power after AGC, signal to noise ratio after AGC and cross-correlation method can be used as selection criterions. According to the simulation results, the performance of the selection diversity is improved in comparison with that of the combining diversity for the WAVE fading channel.

• Journal of Communications and Networks
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• 제6권3호
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• pp.258-268
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• 2004

We demonstrate rotationally invariant space-time (ST) trellis codes with a 4-D rectangular signal constellation for data transmission over fading channels using two transmit antennas. The rotational invariance is a good property to have that may alleviate the task of the carrier phase tracking circuit in the receiver. The transmitted data stream is segmented into eight bit blocks and quadrature amplitude modulated using a 256 point 4-D signal constellation whose 2-D constituent constellation is a 16 point square constellation doubly partitioned. The 4-D signal constellation is simply the Cartesian product of the 2-D signal constellation with it-self and has 32 subsets. The partition is performed on one side into four subsets A, B, C, and D with increased minimum-squared Euclidian distance, and on the other side into four rings, where each ring includes four points of equal energy. We propose both linear and nonlinear ST trellis codes and perform simulations using an appropriate multiple-input multiple-output (MIMO) channel model. The 4-D ST codes constructed here demonstrate about the same frame error rate (FER) performance as their 2-D counterparts, having however the added value of rotational invariance.

• 천문학회보
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• 제36권2호
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• pp.82.1-82.1
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• 2011

Korea Astronomy and Space Science Institute (KASI) operates 2 solar radio observing facilities, e-CALLISTO (Earthwide network of Compound Astronomical Low-cost Low-frequency Instrument for Transportable Observatory) station and Korean Solar Radio Burst Locator (KSRBL). Although e-CALLISTO tracking system improvement.is underway, at least 6 new events were observed in this year. Software development for KSRBL is in progress. The antenna calibration software was updated and flux calibration software was developed. Also the automatic daily overview spectrum monitoring system is now operational. We found solutions to several problems including spurious data and FPGA board communication. However, a few minor unsolved hardware problems still persist. Meanwhile, at least 6 new events were observed by KSRBL in this year, and a comparative study with HXR is currently underway.

• 한국전자파학회논문지
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• 제18권12호
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• pp.1352-1358
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• 2007

본 논문에서는 차세대 이동위성 관제 시스템에서 위성 방향을 탐지하는 알고리즘으로 제안된 MUSIC(Multiple Source Classification) 알고리즘의 통계적 특성에 대하여 서술하였다. 이동위성 관제 시스템에서 MUSIC 알고리즘을 위성 방향 탐지 알고리즘으로 채택할 경우, 이동 위성 관제 시스템 성능이 MUSIC의 위성 방향 탐지 성능에 종속될 수밖에 없다. 따라서 본 논문에서는 여러 가지 데이터 길이와 신호대 잡음비에 따른 MUSIC 알고리즘에 사용되는 파라미터의 통계적 특성을 조사하고 이러한 파라미터가 궁극적으로 위성 방향 탐지에 미치는 영향을 분석하였다.