• 한국항공우주학회지
• /
• 제30권1호
• /
• pp.82-87
• /
• 2002

다목적 실용위성과 같은 저궤도 위성에서의 자세결정은 태양획득에서 중요한 문제이다. 특히, 다목적 실용위성의 태양획득 모드에서는 위성의 피치와 요의 각은 태양 센서로 알 수 있기 때문에 위성의 롤 방향만이 태양을 지향하고 있다. 즉, 한 축의 방향을 알고 있을 때 나머지 두 축의 관성 좌표계에 대한 자세를 결정하는 문제가 된다. 본 논문은 일반적인 저궤도 위성의 3축 중에서 한 축의 방향을 알고 있을 때 위성의 자세를 결정하는 새로운 방법을 제시하고 다양한 모의실험을 통해서 그 유용성을 검증한다.

• Journal of Astronomy and Space Sciences
• /
• 제28권4호
• /
• pp.345-354
• /
• 2011

Earth acquisition is to solve when earth can be visible from satellite after Sun acquisition during launch and early operation period or on-station satellite anomaly. In this paper, the algorithm and test result of the Communication, Ocean and Meteorological Satellite (COMS) Earth acquisition are presented in case of on-station satellite anomaly status. The algorithms for the calculation of Earth-pointing attitude control parameters including those attitude direction vector, rotation matrix, and maneuver time and duration are based on COMS configuration (Eurostar 3000 bus). The coordinate system uses the reference initial frame. The constraint calculating available time-slot to perform the earth acquisition considers eclipse, angular separation, solar local time, and infra-red earth sensor blinding conditions. The results of Electronics and Telecommunications Research Institute (ETRI) are compared with that of the Astrium software to validate the implemented ETRI software.

• 시스템엔지니어링학술지
• /
• 제5권2호
• /
• pp.35-42
• /
• 2009

A newly established provision to enforce the systems engineering was added in the regulation for arms acquisition management in January 2009, and a systems engineering guidelines for defence acquisition is being developed. In this paper we conduct a comparative study of the defence acquisition system in the United States and the Republic of Korea, and propose a improving plan about the domestic defence acquisition system.

• 대한전기학회:학술대회논문집
• /
• 대한전기학회 2011년도 제42회 하계학술대회
• /
• pp.1754-1755
• /
• 2011

GPS modernization program offers a new civil signal on L2 band and there are currently 9 GPS satellites transmitting L2C signal. The acquisition of L2C takes much time comparing with that of L1 signal. This paper suggests a fast acquisition method for the L2C GPS signals for software receivers.

• 천문학논총
• /
• 제11권1호
• /
• pp.243-250
• /
• 1996

Data acquisition system mounted on the Solar Flare Telescope at Bohyunsan Optical Astronomy Observatory is briefly described. The system is made up with CCD cameras, an image processor, a PCI-type PC and a SUN workstation. The image processor, MVC 150/40 comprises a variable scan acquisition module, an image manager and a binary correlator computational module. A typical polarization image of a sunspot is presented to demonstrate performance of the system.

• 한국항해항만학회:학술대회논문집
• /
• 한국항해항만학회 2006년도 International Symposium on GPS/GNSS Vol.2
• /
• pp.395-398
• /
• 2006

In this paper, for implementing a real-time software GNSS receiver we propose the highly efficient and fast algorithms such as partial down-conversion, phase rotator, composite I&Q accumulation, Virtual DCO technique, and parallel acquisition using FFT. When the proposed algorithms are used, more 30 tracking channels with 3 tracking arm(early-prompt-late) is operated real-time on Intel 2.8GHz personal computer. Also, the partial down-conversion reduces the FFT size, for parallel acquisition, to 1/8 of conventional FFT-size and the program size includes map is not exceed 1Mbyte. Finally, the proposed real-time software GNSS receiver using the proposed algorithms provides the navigation solution with below 10 meter rms error.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 2003년도 ICCAS
• /
• pp.876-881
• /
• 2003

Reliable attitude estimation during the launch and early orbit phase is a critical issue for a satellite. Typically gyroscopes and other sensors are utilized to estimate the attitude during this phase. It is difficult to estimate the attitude quickly and reliably using gyroscopes because it requires a large computational load and accurate sensor measurements. Furthermore, the gyroscope failure may lead to the loss of the satellite. This paper suggests a simple attitude estimation method of a low earth orbit satellite without using gyroscopes, but only using sun sensors and magnetometers in the sun-acquisition mode. Using Kompsat-I telemetry data, we verified that the suggested algorithm provides attitude estimation within 3 degrees on each axis.

• 시스템엔지니어링워크숍
• /
• 통권4호
• /
• pp.135-140
• /
• 2004

Defense analysis & evaluation includes menace analysis, validation analysis, problem analysis, scientific technical analysis, technical trad-off analysis, alternative analysis, cost analysis, etc. Reliable related data is required to perform these analysis activities efficiently. but in case of these defense analysis & evaluation data acquisition system, the data is insufficient and scattered about each organization. the data of database system is also not utilized sufficiently. abroad technical data is also low level data such as catalog or military officer's collection. therefore, this paper propose defense analysis & evaluation data acquisition system by systems engineering process. we also propose construction method of data acquisition system.

• 대한전자공학회:학술대회논문집
• /
• 대한전자공학회 2002년도 하계종합학술대회 논문집(5)
• /
• pp.223-226
• /
• 2002

Data Acquisition System of Cargo System using a large output X-ray in harbors is usually composed of Detector, Analog Board, Digital Board, Master Board, Backplane Board and Image Construction System. In this paper we have made an image of material in container-box with Data Acquisition System and studied mainly a configuration method and principle to each part of Data acquisition system.

• 한국정보통신학회논문지
• /
• 제12권7호
• /
• pp.1271-1277
• /
• 2008

본 논문에서는 CDMA-MIMO 상향링크 시스템에서 프리엠블 탐색을 위한 MIMO 채널에서 코드 동기 획득 기법에 대해 연구한다. 다중 송신 및 수신 안테나가 빔형성을 위해서 사용된다. 송수신 빔형성 기반의 ML 코드 동기 획득 기술의 성능이 동기 획득 확률을 통하여 이론적으로 분석된다. MIMO 코드 동기 획득 시스템에서 동기 획득의 성능과 평균 동기 획득 시간을 평가한다. 다중 송신 안테나가 코드 동기 획득 시스템에 송신 빔 이득을 제공하고 그 결과로 빔형성 기반의 MIMO 시스템이 SIMO에 비교하여 더 우수한 동기 획득 성능을 얻을 수 있음을 보인다.