• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.40 no.4
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• pp.300-308
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• 2012

In GPS/INS/barometer navigation system for UAV, two procedures were proposed in order to set three reference parameters for the pressure altitude of QNH or QFE settings, using the navigation data from on-board system alone. These procedures yield required the reference parameters through mathematical process with the altitude and the atmosphere properties measured for a short duration of flight, of which a special pattern is requested according to the selected procedure. Dependency only upon the on-board navigation data can eliminate a requirement for the atmospheric measurement system in the ground support system and can expand a flight boundary to a remote area where the ground support is not available. Especially the procedure with the regression method uses altitude and pressure but temperature to produce the three reference parameters. No need of temperature measurement for the pressure altitude system can simplify the on-board air data system.

• Current Industrial and Technological Trends in Aerospace
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• v.6 no.2
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• pp.80-89
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• 2008

Photogrammetry is a non-direct 3-dimensional coordinate measurement technique using 2-dimensional photographic images. For reconstruction 3-dimensional data from the 2-dimensional photos, photogrammetry uses the fundamental principle of triangulation. Digital photogrammetry solve for the camera location and coordinates simultaneously through the mapping, scaling and bundle processing in software processing. In this paper, several applications for photogrammetry measurement are introduced, such as 'photogrammetric measurement of the gravity deformation of a cassegrain type antenna', 'analysis of photogrammetry data from ISIM mockup', 'underwater photogrammetric verification of nuclear fuel assemblies', 'spacecraft optical bench measurement' and 'spacecraft ground support equipment measurement'.

• Aerospace Engineering and Technology
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• v.3 no.2
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• pp.56-64
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• 2004

In this research, design results of computer hardware which control solid motor movable nozzle thrust vector control(TVC) actuator for Korea Space Launch Vehicle I(KSLV-I) are described. TVC computer hardware is the equipment which has jobs for receiving control commands from Navigation Guidance Unit(NGU) and then actuating TVC actuator. Also, it has ability to communicate with other on board or ground equipments. Computer hardware has a digital signal processor as the main processor which is capable of high speed calculating ability of control algorithm, so it can have more stability, reliability and flexibility than the previous analog controller of KSR-III. Target board was designed for on board program development and then first prototype hardware was developed. Top level system design criteria, hardware configurations and ground support equipment of TVC computer system are described.

• 발명특허
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• v.13 no.1 s.143
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• pp.36-37
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• 1988

경기도 안양시 호계동 럭키금성 제1연구단지 내에 위치한 금성통신연구소는 지하1층, 지상 3층(대지 4천 4백 55평, 건평 1천 2백 96평)의 규모로 적극적으로 첨단과학기술의 흡수 및 확산을 목적으로 신설한 연구단과 이러한 신기술을 기업여건에 적합하게 응용하는 개발단을 재편성하여 유선통신단말기를 개발하는 개발 1실, 무선통신단말기를 개발하는 개발 2실, 컴퓨터주변기기를 개발하는 개발 3실, 의료기 및 정보통신기를 개발하는 개발 4실 및 연구개발업무의 효율화를 지원하는 연구관리부 등 현재 2백 20명의 연구원이 연구개발에 매진하고 있다. 또한 CAD실, 전산실, 음향측정실, 키폰 종합실험실, MF실, 기술자료실, 시작실과 Mini Computer, CV Model CAD System, MOS, 음향측정장비, Spectrum Analyzer등 7백여점의 연구기자재를 갖추어 놓고 연구개발업무를 수행하고 있다.

• Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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• 2011.05a
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• pp.173-176
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• 2011

New paradigm is based on the e-navigation policy which is the harmonised collection, integration, exchange, presentation and analysis of maritime information onboard and ashore by electronic means to enhance berth to berth navigation and related services, for safety and security at sea and protection of the marine environment. One of the requirements is seamless communications between various communication systems. So we need the maritime wireless communications based on the SDR technology. In this paper we analyse characteristics and issues of maritime wireless communication technology and service framework and propose a SDR based maritime system platform which can operate in multi-mode.

• Journal of Intelligence and Information Systems
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• v.3 no.1
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• pp.143-160
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• 1997

현재 우리 군에서는 첨단과학무기를 이용한 전투력을 신속히 집중, 전환시키고 효과적으로 통합 운용해야하는 각급 제대의 지휘관 및 참모의 지휘통제능력 향상을 위하여 첨단 컴퓨터장비를 이용하여 시뮬레이션 기법을 통한 워게임 모델을 개발하여 이를 이용한 훈련을 실시하고 있다. 이 워게임 모델중 지상전투의 가장 기본이 되는 근접전투 시뮬레이션은 미국에서 개발도입된 "COBRA" 시스템을 이용하고 있으나 한국실정에 맞는 시스템으로 확장 및 유지보수가 어렵고, 상위시스템의 서브시스템으로만 운영되고있어 자체 교육훈련 및 전투분석을 위한 단독시스템으로 운영이 어려운 실정이다. 본 논문에서는 이러한 문제점을 극복하고, 방대한 양의 지식을 효율적이고 효과적으로 표현할 수 있으며 시스템의 확장 및 유지보수가 용이하고 우리실정에 적합한 전투 훈련을 실시하도록 지원하는 워게임(근접전투) 지원용 멀티미디어 전문가시스템을 개발하였다. 본 논문에서 개발한 전문가시스템은 쌍방이 부대들의 근접전투를 실시할 때 실전에서 나타날 수 있는 가능한 모든 상황의 데이터를 이용하여 전투상황을 분석하며, 기존의 획일적이고 단순한 형태로 결과를 판정하던 것을 전투원의 사기, 체력, 전투한계 등 심리적 요소까지 고려함으로써 새로이 변화되는 전쟁양상에 쉽게 적응할 수 있는 확장성 및 유지보수가 용이하며 시스템 단독으로 운영하여 반복적으로 전투를 분석하고 교육훈련을 실시하도록 함으로써 실전적이고 실질적인 근접전투 워게임지원이 가능하다. 본 논문에서는 전문가 시스템을 개발함에 있어서 지식베이스 모듈, 추론엔진 모듈 및 설명 모듈은 전문가 시스템 개발도구인 Smart Elements를 이용하여 구축하였으며, 사용자 인터페이스 모듈은 멀티미디어 저적도구인 툴북 3.0을 이용하였으며, 마지막으로 전체적인 모듈은 API를 이용 통합하여 하나의 응용소프트웨어를 생성하였다.

• Journal of Climate Change Research
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• v.1 no.3
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• pp.211-217
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• 2010

Off-road transportation sector including construction equipment, ground support equipment in airport, cargo handling equipment and agroforestry machinery have not calculated as emission source classification in 1A3e2. In this study, the statistics of oil consumption for construction, aviation, shipping and agroforestry are separated for this sector by oil type. And the greenhouse gas emission by off-road transportation emission factor in 1996 & 2006 IPCC Guidelines are calculated and compared with each other. As a result, the nationwide $CO_2$ equivalent emission from off-road transportations by the emission factor of 1996 & 2006 IPCC Guidelines are calculated as 4,919 kton/yr and 5,530 kton/yr in 2007. The contribution ratio of off-road transportation emission by this study is estimated as 5.5% to the subtotal emission from on-road transport sector.

• Aerospace Engineering and Technology
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• v.9 no.2
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• pp.22-30
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• 2010

KARI had integrated and tested GEO satellite in cooperation with Astrium Inc., France. In the middle of integration and test, It was necessary to check GEO satellite SA(solar array) status and require electrical interface verification with bus. SA of GEO satellite have different mechanical characteristics in comparison with those of LEO satellite which was tested in KARI. LEO SA has been deployed by simple mechanical hinge system but GEO SA has been done by more complicated method. so in this paper, we designed the test configuration and analyzed the test result of solar array electrical integration of GEO satellite.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.31 no.2
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• pp.96-102
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• 2003

The thermal design of MGSE(Mechanical Ground Support Equipment) panel is performed for thermal vacum thest of Ka-band EQM(Engineering Qualification Model) payload of communications and broadcasting satellite. The thermal environments are predicted to evaluate the performance of transponder equipments in the thermal vacum chamber. SINDA is used to verify the thermal design of the heat pipe layout. Embedded 16 heat pipes in the EQM payload developed for Ka-band trasponder equipments are designded properly. The heat fluz loaded on the external facesheet is 265W/㎡ for the hot platear function test of the traspinder equipments, and the zero heat flux for the cold plateau case. The maxium predicted heat transport capability is 2723 W-cm.

• Current Industrial and Technological Trends in Aerospace
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• v.6 no.2
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• pp.40-50
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• 2008

Most of satellite program process consists of mission analysis, thermal, structure, electronics design, and operation, etc. Each step has several steps like design phase, development phase, and verification phase, etc. As to do this kind of process, very high costs and much time are required, further high risk is included. So for solving those difficulties, satellite developers have designed and used satellite simulator system. In early stage of satellite development, simulator system was just used for a fragment of development and verification, so it could not give enough advantage on satellite development. In order to get high advantage on satellite development, full system level simulators which can be used for several steps for development and verification are evolved. So This paper introduces the trend of simulation systems for satellite development and verification used by several satellite developers.