• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.9
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• pp.747-754
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• 2013

This paper describes SCTE(System and Control unit Test Equipment) as an integrated test equipment for airborne SAR system and control unit. SCTE enhances reusability of test equipment by modular design for required functions and strengthens automatic testing and test convenience by providing functions such as script-based testing function and report generation function. Also, it includes a navigation data simulator which can simulate various flight conditions. In this paper, we details SCTE requirements, H/W and S/W design, implementation, and test results with control unit and SAR system.

• Bulletin of the Korean Space Science Society
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• 2006.04a
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• pp.129-132
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• 2006

Animal Tracking System consists of Animal Tracking System Receiver on the Satellite segment, Animal Tracking Terminal and Ground Station for data analysis on the Ground segment. This paper describes operation concept and hardware design for Animal Tracking System which is the payload of HAUSAT-2 being developed by the Space System Research Laboratory (SSRL). Algorithms for determination of animal position and data processing are also referred to.

• Atmosphere
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• v.12 no.4
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• pp.56-68
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• 2002

In this study, an overview of the Earth Observing System (EOS) program is provided with discussions on its spacecrafts and instruments, and on the scientific issues. The EOS satellites aim at monitoring the Earth environmental system by observing parameters of subsystems such as atmosphere, ocean, land, and biosphere. The first EOS flagship, Terra, was launched on December 1999. Five instruments onboard Terra can measure cloud and aerosol properties, radiation, terrestrial surface, and ocean color. The second EOS flagship, Aqua, which was launched on May 2002, loads six instruments that measure clouds, radiation, precipitation, terrestrial surface, ocean color and sea surface temperature. The observational data available from the EOS satellites may complement data from the Communication-Oceanography-Meteorology satellite, which will be launched in 2008, for meteorological and environmental forecasts.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.6
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• pp.142-147
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• 2004

Satellite laser ranging (SLR), which is the most accurate geodetic method for precise orbit determination of artificial satellites, will be used to determine the precise orbit of STSAT2. This paper will present the development of a Laser Reflector Array (LRA) of STSAT2. Currently one LRA was designed, analyzed, manufactured, optically tested and assembled.

• Current Industrial and Technological Trends in Aerospace
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• v.6 no.2
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• pp.116-124
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• 2008

Korea Aerospace Research Institute(KARI) is developing COMS (Communication, Ocean and Meteorological Satellite) which is scheduled to take off in June, 2009. COMS is the first geosynchronous satellite developed in Korea which is able to perform three missions 24 hours a day. The oceanic payload was transferred from France to Korea in November, 2008 and made it possible to integrate all three payload together. After the integration COMS is planned to be transferred to Guiana Space Center (on French territory) to be launched. In this paper the trend of domestic and international development of the multi-purpose geosynchronous satellite considering the COMS is the first operational geosynchronous multipurpose satellite in the world.

• Proceedings of the IEEK Conference
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• 2002.06b
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• pp.181-184
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• 2002

본 논문에서는 600Hz 무선 LAN 시스템에 탑재를 위한 600㎓ 대역 전력증폭기 모듈을 개발 하였다. 600㎓ 대역 전력증폭기 모듈에 실장된 600㎓ 대역 전력증폭기 MMIC는 ETRI에서 설계 및 제작한 것으로 칩의 크기는 2.80 × 1.75㎟이며, on-wafer측정을 하여 얻은 결과는 동작 주파수 58~620Hz에서 소신호 이득은 12.4dB이고, 최대 소신호 이득은 59~60G보z에서 ISdB이며, 출력전력(Pldn)은 16.3~16.7dBm을 얻었다. 이와 같은 특성을 갖는 전력증폭기 MMIC를 사용하여 모듈을 제작하였으며, RF feed line을 위해 Rogers 사의 R03003 기판을 사용하였다. 모듈의 입출력은 동작 주파수 대역에 적합한 WRl5라는 waveguide 형태를 사용하였고, DC 바이어스 공급을 위해 3.5㎜ K-connector를 사용하였다 제작한 모듈의 크기는 40 × 30 × 15㎣이며, 최적의 성능을 얻고자 tuning bar를 상하로 이동하여 최적점을 찾았으며 나사로 고정하여 상태를 유지하도록 하였다. DC 바이어스 및 RF feed line과 칩의 연결은 본딩에 의한 인덕턴스를 최소화하기 위하여 3mil 두께의 리본 본딩을 하였다 전력증폭기 모듈을 측정한 결과, 동작주파수 600㎓ 대에서 소신호 이득은 6dB 이상, 입력 정합은 -lOdB 이하, 출력 정합은 -4dB 이하로 측정되었긴, 출력전력은 SdBm 이상으로 측정되었다. 동국대에서 제작한 600Hz 무선 LAN 시스템에 전력증폭기 모듈을 시스템 송신부에 탑재 시험한 결과, 동영상을 실시간으로 전송하는데 성공하였다.

• The Journal of Korean Institute of Electromagnetic Engineering and Science
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• v.20 no.6
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• pp.580-588
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• 2009

A Missile Warning Radar is an essential sensor for active protection system to detect antitank missile in all weather environments. This paper presents the design, development, and test results of L-band pulsed Doppler radar system for main battle tank. This radar system consists of 3 LRUs, which include antenna unit, transmitter and receiver unit and radar signal & data processing unit. The developed core technologies include the patch antenna, SSPA transmitter, coherent I/Q detector, DSP based Doppler FFT filter, adaptive CFAR, SIW tracking capability, and threat decision. The design performance of the developed radar system is verified through various ground fixed and moving vehicle test.

• Journal of the Society of Naval Architects of Korea
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• v.41 no.5
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• pp.55-62
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• 2004

The logistics of entire shipbuilding process are integrated during the block erection process and the schedules for the erection process are made prior to. the schedules of any other processes. Therefore, efficient scheduling of the block erection process are one of most important issues in shipbuilding. There are only a few studies published regarding block erection scheduling methods because of its complexity and variability. This paper proposes an algorithm for diminution of maximum load based on constraint satisfaction technique. it is developed primarily for the efficiency in load leveling and applicability to the actual block erection process. The proposed algorithm is applied to actual block erection process and the results shows improvements in load leveling. It can also be used for the scheduling of fabrication, sub-assembly, and assembly to improve load leveling.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.38 no.8
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• pp.834-841
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• 2010

The STSAT-3 (science and technology satellite) is the first satellite whose entire structure was made of composite materials in Korea and it will be launched later in 2011. As like other small satellites, it is also equipped with several advanced instruments whose major objectives focused on the scientific tests in space. The HPS (hall thruster propulsion system) using xenon gas as a propellant has been developed and its overall ground tests were conducted. This research emphasizes on the technologies and procedure applied to the development of the entire HPS and its function and environment tests.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.41 no.12
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• pp.1018-1024
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• 2013

On-Board computers (OBC) for LEO & GEO satellites have been developed with their own dedicated architecture so far even though they have many similar functionalities. In this paper, we present a conceptual study results of standard OBC architecture design and propose the domestic development plan for the next generation satellite OBC. Proposed architecture is highly flexible and can be used at LEO/MEO/GEO and Moon Explorer/Deep Space Probe. Also, we introduce current status of standard OBC which is under development.