• 한국실내디자인학회논문집
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• 제13권5호
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• pp.32-38
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• 2004

The value of the Tosi-Hanok have recently been appreciated and accordingly the resultant studies have actively been conducted. This is an attempt to probe our architectural type haying identity through our traditional architecture in Korean society that pursues only something new. But owing to the infusion of foreign cultures and modernization, the archetype of Korean-style house has either been damaged or indiscriminately transformed without the establishment of its proper norms. The understanding of the value of traditional cultures has gradually increased, and accordingly effort to preserve Korean-style houses through legal regulations or systems have continually been made in terms of appearance or cityscape. For this reason, it is thought that it Is insufficient to present the direction or alternative to preservation in relation to the change or use of the interior space with the pattern of requirement for other programs other than dwelling. Therefore, this study attempted to find out the original meaning of Korean-style house by highlighting the advantages of Tosi-Hanok and supplementing its disadvantage while accommodating the diverse requirement for programs as contemporary residential space. And it was intended to propose the model for Tosi-Hanok that accommodates social changes in content while maintaining its meaning by analyzing the Tosi-Hanok with a focus on interior space and preserving historical continuity on its basis.

• 한국우주과학회:학술대회논문집(한국우주과학회보)
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• 한국우주과학회 2010년도 한국우주과학회보 제19권1호
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• pp.25.3-25.3
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• 2010

Our previous study used a bar-type reference mirror to measure the relative distance to the target surface. The target measurement accuracy was required to $1{\mu}m$ PV for aspheric optical surface up to 1m in diameter. Earlier system suffers from the reference surface deformation when the measuring part moves. In order to reduce the deformation, measuring part and the reference part separated from each order in the new design. This system utilizes a kinematic support assembly using invar flexure to minimize the reference surface deformation under gravity and vibration. The surface deformation requirement of reference mirror is defined as of $0.2{\mu}m$ under gravity and 40Hz vibration. The finite element results, shows reference mirror deformation of $0.164{\mu}m$. The first resonance mode was computed to analysis 46.05Hz for reference part and 43.44Hz for measuring part. Thesis satisfies the frequency requirement.

• Journal of Astronomy and Space Sciences
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• 제27권4호
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• pp.345-352
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• 2010

Korea multi-purpose satellite-5 (KOMPSAT-5) is a low earth orbit (LEO) satellite scheduled to be launched in 2010. To satisfy the precision orbit determination (POD) requirement for a high resolution synthetic aperture radar image of KOMPSAT-5, KOMPSAT-5 has atmosphere occultation POD (AOPOD) system which consists of a space-borne dual frequency global positioning system (GPS) receiver and a laser retro reflector array. A space-borne dual frequency GPS receiver on a LEO satellite provides position data for the POD and radio occultation data for scientific applications. This paper describes an overview of AOPOD system and operation concepts of the radio occultation mission in KOMPSAT-5. We showed AOPOD system satisfies the requirements of KOMPSAT-5 in performance and stability.

• International Journal of Aeronautical and Space Sciences
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• 제17권3호
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• pp.401-408
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• 2016

During daylight, the solar array of low earth orbit satellites harvests electrical power to operate satellites. The power conversion of the solar array is carried out by control of the operation point using the solar array regulator when the solar array faces the sunlight. Thus, the design of the solar array should comply with not only the power requirement of satellite system but also the input voltage requirement of the solar array regulator. In this paper, the design requirements of the solar array for low earth orbit satellites are defined, and the means of satisfying these requirements are described. In addition, the architecture of a multi-distributed interface is suggested to maximize the power harvested from a solar array having high temperature deviation between each panel. The power analysis in this paper shows the optimal number of multi-distributed interfaces with a converter.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2007년도 Proceedings of ISRS 2007
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• pp.105-108
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• 2007

The COMS LRIT/HRIT broadcast service should satisfy the 15 minutes timeliness requirement. The timeliness requirement is an important enough to impact on the overall performance of LHGS. Therefore, the simulation for the LHGS processing was performed with the LHGS prototype in this paper. First, processing time is measured for each process (per modules) of the LHGS without I/O time. Then, the LHGS processing is performed with worst scenario and the processing time is measured. Finally, analyses for processing time and time constraint are performed.

• Journal of Astronomy and Space Sciences
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• 제31권3호
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• pp.265-276
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• 2014

The application of software engineering is not common in the development of astronomical observation system. While there were component-wise developments in the past, large-scale comprehensive system developments are more common in these days. In this study, current methodologies of development are reviewed to select a proper one for the development of astronomical observation system and the result of the application is presented. As the subject of this study, a project of operation software development for an astronomical observation system which runs on the ground is selected. And the output management technique based on Component Based Development which is one of the relatively recent methodologies has been applied. Since the nature of the system requires lots of arithmetic algorithms and it has great impact on the overall performance of the entire system, a prototype model is developed to verify major functions and performance. Consequently, it was possible to verify the compliance with the product requirements through the requirement tracing table and also it was possible to keep to the schedule. Besides, it was suggested that a few improvements could be possible based on the experience of the application of conventional output management technique. This study is the first application of the software development methodology in the domestic astronomical observation system area. The process and results of this study would contribute to the investigation for a more appropriate methodology in the area of similar system development.

• 한국전자거래학회지
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• 제12권4호
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• pp.99-125
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• 2007

최근 U-City와 같은 유비쿼터스 지능 공간(USS) 개발 계획이 확산됨에 따라 USS 특성에 맞는 시스템 분석 및 설계 방법론으로 USS과제의 생산성을 높이는 것이 중요하게 되었다. 하지만 전통적 UML과 같은 기존의 개발 방법론은 상황 인식, 서비스 기반 아키텍처 및 다중에이전트와 같은 USS에 필수적으로 고려되는 컴포넌트를 고려하지 않는다. 즉 기존 방법론들은 USS 분석 및 설계에 최적이 아니다. 따라서 본 논문의 목적은 USS 개발을 위한 보다 정교한 개발 방법론을 제안하기 위해서 BPR-USS와 UML-USS라는 복합적 접근법을 제안하는 것이다. BPR-USS는 공간 설계 제공하고, StarUML 툴킷을 기반으로 하는 UML-USS는 확장된 UML을 제공한다. 본 논문에서 제안한 접근법의 적합성을 나타내기 위해서 서울 소재의 특정 복합상가를 대상으로 하는 실제 USS 개발 과제에 대한 예제를 제시하였다.

• 한국항공우주학회지
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• 제42권1호
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• pp.76-81
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• 2014

군용 헬리콥터는 적 지역에 침투 시 저공비행 및 침투비행으로 인해 적의 소형화기에 노출되면서, 피탄에 의한 항공기의 폭발 유발 가능성이 높다. 최근 군요구도에 있어서 피탄에 의한 폭발 환경에 대해서 생존성 확보를 위한 내탄 성능을 요구한다. 국내 최초의 군용 헬리콥터인 한국형기동헬기의 연료계통 요구도에도 적의 피탄에 대한 내폭발성을 요구하고 있으며, 요구도 충족을 위해 국내 최초로 탑재형 불활성 가스발생장치(OBIGGS)를 적용하였다. 개발단계에서 미흡하게 설계된 내폭발성과 연관된 Vent System을 개선하여 내폭발성 성능을 재평가하고 설계에 적합함을 입증하였다.

• 한국항공우주학회지
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• 제45권9호
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• pp.734-745
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• 2017

달 착륙선의 항법 시스템은 자율 정밀 항법 성능을 확보하기 위해 관성측정기와 별추적기, 고도계, 속도계, 지형상대항법 카메라 등 다양한 항법용 전장부품으로 구성되는데 착륙선의 착륙 시나리오와 임무 요구 성능에 따라 적합한 성능의 항법용 전장부품 선정이 필요하다. 본 논문에서는 달 착륙선에 요구되는 항법용 전장부품의 사양을 공분산해석을 통해 분석하였다. 77차 상태변수로 구성되는 기준 시스템 오차모델과 센서의 측정모델을 정의하고 착륙선의 임무 요구 성능은 90m($3{\sigma}$) 착륙 위치 정확도를 요구하는 정밀탐사 임무와 6km($3{\sigma}$)의 착륙 오차가 허용되는 영역탐사 임무로 구분하였다. 자율항법 시작 시점에 따라 PDI(Powered descent initiation)와 DOI(Deorbit initiation) 시나리오로 나누고 항법용 전장부품의 조합과 착륙 시나리오에 따른 성능 분석을 통해 가상의 임무 요구 성능을 만족하기 위한 항법 시스템의 요구사양을 도출하였다.

• 대한산업공학회지
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• 제30권4호
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• pp.294-300
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• 2004

This paper considers a trade-off effect between in-house storage space and leased storage space in generic warehouses operated under a randomized storage assignment policy. The amount of in-house storage space is determined based on the law of large numbers satisfying a given service level of protection against space shortages. Excess space requirement is assumed to be met via leased storage space. A new analytic model is formulated for determining the excess space such that the total cost of storage space is minimized. Finally, computational results are provided for the systems where the standard economic-order-quantity inventory model is used for all items.