• Journal of the Korean Society of Food Culture
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• v.15 no.5
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• pp.387-397
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• 2000

A survey was carried out to investigate relation between life stress and nutrient intake status in female university students. It was represented that increasing trends of food intake under the stress condition and preference taste was sweet and hot in female students. The female students thought that food intake for coping with stress was produced negative results and they perceived the relation between stress and their health problem. There was a positive correlation between stress level and the change of food intake in female students statistically(p<0.01). They had higher stress in future prospect, academic problem, friend relationship, personality and family relationship. The average calorie intake of female university students was 1553.06kcal(77.65% of RDA). The intake of protein, calcium and iron were quite less than the RDA, whereas the intake of phosphate, vitamin A, $B_2$, C, niacin were more than the RDA. In changes of nutrient intake under the stress conditions, the higher stress group had decreased intake of calcium, iron, vitamin $B_1,\;B_2$, C than the lower stress group(p<0.05).

• Journal of Astronomy and Space Sciences
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• v.23 no.4
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• pp.445-452
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• 2006

In this paper, the conceptual design of satellite digital base put which is based upon data interface between satellite on-board computer and remote devices like satellite sub-components is presented. This conceptual design shows the unification of the interface between on-board computer and satellite remote devices and the hierarchical results of the interface level. A comparison of different system and merits and demerits of digital base part coming from this conceptual design is performed.

• Journal of Astronomy and Space Sciences
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• v.17 no.1
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• pp.117-122
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• 2000

The KOMPSAT(Korea Multi-Purpose SATellite) has two optical imaging instruments called EOC(Electro-Optical Camera) and OSMI (Ocean Scanning Multispectral Imager). The image data of these instruments are transmitted to ground station and restored correctly after post-processing with the telemetry data transfeered from KOMPSAT spacecraft. The major timing information of the KOMPSAT is OBT (On-Board Time) which is formatted by the on-board computer of the spacecraft, based on 1Hz sync. pulse coming from the GPS receiver involved. The OBT is transmitted to ground station with the house-keeping telemetry data of the spacecraft while it is distributed to the instruments via 1553B data bus for synchronization during imaging and formatting. The timing information contained in the spacecraft telemetry data would have direct relation to the image data of the instruments, which should be well explained to get a more accurate image. This paper addresses the timing analysis of the KOMPSAT spacecraft and instruments, including the gyro data timing analysis for the correct restoration of the EOC and OSMI image data at ground station.

• Proceedings of the Korea Information Processing Society Conference
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• 2005.11a
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• pp.1421-1424
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• 2005

저궤도 위성인 다목적실용위성 2호의 컴퓨터 시스템은 3개 프로세서로 구성된 분산처리 구조이며 프로세서와 프로세서, 프로세서와 주변 장치들과의 통신은 MIL-STD-1553B 버스를 통해 이루어진다. 이들 3개 프로세서들 상에서 실행되는 탑재소프트웨어는 위성의 하드웨어 및 주변 입출력 장치들을 제어 및 관리한다. 그리고 위성의 결함을 관리하는 기능과 비상시에는 지상과의 연결 없이 위성을 자동제어 하는 기능들 또한 탑재소프트웨어에 구현되어져있다. 본 논문에서는 저궤도 위성인 다목적실용위성-2호의 임무를 수행하기 위한 탑재소프트웨어의 구성 및 기능, 개발과정과 개발환경을 소개한다.

• Journal of the Korean Society for Aviation and Aeronautics
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• v.17 no.3
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• pp.70-77
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• 2009

We proposed the method of avionics integrated architecture using high-speed fiber optic bus. Typically, data bus of aircraft consists of electronic and optic data transmission method. Avionics systems are difficult to operate the electronic data transmission method for the high speed data processing, synchronization and interconnection between flight control system and flight management system efficiently. In this paper, it is known to look into the problem of data bus and the advanced trend in avionics systems, and propose the appropriate data bus of the advanced avionics systems.

• Proceedings of the KIEE Conference
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• 2003.07c
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• pp.1553-1555
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• 2003

Coatings on glass with highly transparent conducting oxide films(TCOs) are performed mostly by using indium tin oxide(ITO). This Oxide material is very common for applications where both high electrical conductivity. Photovoltaic cells, transparent electrical heater, selective optical filter, and a optical transmittance are essential. In this study, ITO thin films were deposited on $SiO_2$/soda-line glass plates by a dc magnetron sputtering technique. The crystallinity and electrical properties of the films were investigated by X-ray diffraction(XRD), atomic force microscopy(AFM) scanning and 4-point probe. The optical transmittance of ITO films in the range of 300-800nm were measured with a spectrophotometer. As a result, we obtained polycrystalline structured ITO films with (222), (400), and (440) peak. Transmittance of all the films were higher than 90% in the visible range.

• Proceedings of the Korea Information Processing Society Conference
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• 2015.10a
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• pp.345-347
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• 2015

인공위성은 다양한 센서장치, 구동장치, 전자장치들로 구성되어 있으며, 위성을 제어하는 컴퓨터 장치는 이들 장치들과 다양한 종류의 통신 버스로 연결되어있다. 정의된 프로토콜에 따라 명령을 전송하고 장치들의 상태 정보를 수집하여 위성을 운영한다. 위성에서 많이 사용되는 대부분의 상용 센서나 구동장치들은 표준화된 버스 (ex, 1553B, CAN, UART, etc ...) 인터페이스를 지원한다. 그러나 위성의 임무나 설계에 맞게 특수하게 제작된 장치의 경우는 범용의 버스보다는 용도에 적합한 프로토콜이 설계되고 제작된다. 본 논문에서는 2018년 발사 예정인 정지궤도복합위성 컴퓨터 장치 (GMU) 내의 프로세스 모듈과 시스템의 이상상태를 감지하여 GMU의 운용 모드 및 형상의 변경을 담당하는 MRE 모듈사이의 통신을 담당하는 IMGL 설계를 소개하고 IMGL 운영을 담당하는 소프트웨어 설계 및 구현 내용을 기술한다.

• Journal of Korean Port Research
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• v.12 no.1
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• pp.131-143
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• 1998

This paper presents derivation of stage-discharge curve for Yangsan river. To derivate of stage-discharge lationship is one of the essential research areas in the water resource field. It provides reliable data a long term planning and hydrologic quantity on water resource development by quantitative analysis. The rating curve derivated through 15 discharge-observation on Yangsan river basin in 1997 has been estimated Q=1283.0262-1553.3158H+477.2702H2. According to the rating curve, the highest water level 2.6m, the limited water-level should be bound to the maximum of 2.6m. Before this research, stage-discharge curve of Yangsan river has not been developed, and only 15 discharge observation(hydrometry) has been carried out though this research. Therefore it seems necessary to collect observation data through a long term process to obtain a reliable rating curve equation.

• Korean Journal of Pharmacognosy
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• v.51 no.3
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• pp.192-198
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• 2020

Caenorhabditis elegans model system was used to investigate the antioxidant activity of Beta vulgaris L. (Chenopodiaceae) methanol extract. The methanol extract showed DPPH radical scavenging and superoxide quenching activity in a dose-dependent manner. The B. vulgaris methanol extract was measured for the activity of superoxide dismutase (SOD), catalase, and oxidative stress tolerance by using C. elegans, along with reactive oxygen species (ROS) level. In addition, to see that the regulation of the stress response gene is responsible for the increased stress tolerance of C. elegans treated by the methanol extract, SOD-3 expression was measured using a transgenic strain. As a result, the B. vulgaris methanol extract increased SOD and catalase activities, and decreased ROS accumulation, dose-dependently. Furthermore, the methanol extract-treated CF1553 worm showed higher SOD-3::GFP intensity than the control.

• Journal of Astronomy and Space Sciences
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• v.20 no.4
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• pp.339-350
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• 2003

Engineering qualification model payload for a communications and broadcasting satellite(CBS) was developed by ETRI from May, 2000 to April, 2003. For. the purpose of functional test and verification of the payload, a real-time hardware-in-the-loop(HITL) CBS simulator(CBSSIM) was also developed. We assumed that the spacecraft platform for the CBSSIM is a geostationary communication satellite using momentum bias three-axis stabilization control technique based on Koreasat. The payload hardware is combined with CBSSIM via Power, Command and Telemetry System(PCTS) of Electrical Ground Support Equipment(EGSE). CBSSIM is connected with PCTS by TCP/IP and the payload is combined with PCTS by MIL-STD-1553B protocol and DC harness. This simulator runs under the PC-based simulation environment with Windows 2000 operating system. The satellite commands from the operators are transferred to the payload or bus subsystem models through the real-time process block in the simulator. Design requirements of the CBSSIM are to operate in real-time and generate telemetry. CBSSIM provides various graphic monitoring interfaces and control functions and supports both pre-launch and after-launch of a communication satellite system. In this paper, the HITL simulator system including CBSSIM, communications payload and PCTS as the medium of interface between CBSSIM and communications payload will be described in aspects of the system architecture, spacecraft models, and simulator operation environment.