• 대한전기학회:학술대회논문집
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• 대한전기학회 2011년도 제42회 하계학술대회
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• pp.1770-1771
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• 2011

In mission planning of UAV applications, especially for the missions requiring height transitions, it is required to generate reference flight trajectories considering the performances of the engine installed in the UAV. Even though the vertical line following guidance based height transition trajectory generation method has been developed to build reference height transition trajectories easily, it is not adequate for considering engine performances effectively since many engine characteristics and performances have conventionally been described in the V-H(speed-height) plane which is not the very space where the UAVs are actually flying. In this paper, we derive the trajectories in V-H plane for the vertical line following flights. And based on the results, a new algorithm to design the reference height transition trajectories for UAV applicaions. Simulation results demonstrate that the proposed algorithm is very effective and easily applicable.

• 한국실내디자인학회논문집
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• 제15권5호
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• pp.167-174
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• 2006

The purpose of this study is to provide basic guidelines for qualitatively advanced children facilities and spaces in grand bookstores. The main concept is considered with a situation that grand bookstores of large corporations are increasing in quantity, but their social missions for the user are often being connived. The study is peformed by research of current six domestic grand bookstores, two branches of each three large corporations, larger than 2,500py in Seoul, and the research is applied to Murtha's User Benefit Criteria as a basic format. As a result of the research, some problems to be improved are detected in ways of behavioral facilitation, physiological maintenance, perceptual maintenance, and social facilitation, therefore findings in survey turned out to be parents' dissatisfaction in many aspects. Finally, with this result, it is desirable for interior designers to reflect the indicated insufficient elements to their following children's bookstore space design for the user, children and their parents.

• 한국실내디자인학회:학술대회논문집
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• 한국실내디자인학회 2006년도 춘계학술발표대회 논문집
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• pp.119-124
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• 2006

The purpose of this study is to provide basic guidelines for qualitatively advanced children's facilities and spaces in grand bookstores. The main concept is considered with a situation that grand bookstores of large corporations are increasing in quantity, but their social missions for the user are often being connived. The study is performed by research of current six domestic grand bookstores, two branches of each three large corporations, larger than 2,500py in Seoul, and the research is applied to Murtha's User Benefit Criteria as a basic format. As a result of the research, some problems to be improved are detected in ways of behavioral facilitation, physiological maintenance, perceptual maintenance, and social facilitation, therefore findings in survey turned out to be parents' dissatisfaction in many aspects. Finally, with this result, it is desirable for interior designers to reflect the indicated insufficient elements to their following children's bookstore space design for the user, children and their parents.

• 전자통신동향분석
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• 제8권3호
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• pp.39-52
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• 1993

This study involves a Common Cause Failure (CCF) problem on the ultra-high reliability required system development such as war game operations, nuclear power control, air traffic control, space shuttle missions, and large scale network communication system. The system situation problems are defined according to CCF, reliability and system fault identifications for the development cast verifications in the multi-version redundant software system. Then, CCF analysis of redundant system, system principles and statistical dependence are also described. This validation oh the CCF in the human software interaction system will notify software engineers to conceive what really is CCF contribution factor, not only the internal but the external ones.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2004년도 추계 학술대회논문집
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• pp.137-139
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• 2004

The monopropellant hydrazine thrusters are widely used for the satellite on-board propulsion system fulfilling various missions in space. They have outstanding features caused by the nearly unlimited restart capability and the very high credibility. The sole monopropellant thruster used at precent in nation is MRE-1 that is a standard component of NASA. It can produce 4.45 N of nominal thrust. Due to the glowing complexity with a satellite mission, the needs for thrusters of the diverse performance are being increased. The numerical simulation could give useful information to develop a new type thruster instead of the experiments performed previously. Therefore it is critical to make a reliable computer code to prepare design change of a thruster. In this paper, the performance analysis and validation of the satellite monopropellant hydrazine thruster currently used is accomplished as the preliminary study to serve valuable data for future design change.

• 산업경영시스템학회지
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• 제33권3호
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• pp.154-161
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• 2010

This paper considers the simultaneously firing model for the artillery operations. The objective of this paper is to find the optimal fire sequence minimizing the final completion time of the firing missions of multiple artillery units for multiple targets. In the problem analysis, we derive several solution properties to reduce the solution space. Moreover, two lower bounds of objective are derived and tested along with the derived properties within a branch-and-bound scheme. Two efficient heuristic algorithms are also developed. The overall performances of the proposed branch-and-bound and heuristic algorithms are evaluated through various numerical experiments.

• 대한원격탐사학회:학술대회논문집
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• 대한원격탐사학회 2003년도 Proceedings of ACRS 2003 ISRS
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• pp.1307-1309
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• 2003

The EO-1 spacecraft, launched November 21, 2000 into a sun synchronous orbit behind Landsat 7, hosts advanced technology demonstration instruments, whose capabilities are currently being assessed by the user community for future missions. A significant part of the EO-1 program is to perform data comparisons between Hyperion, ALI and Landsat 7 ETM+. In this paper, a comparison of forest classification results from Hyperion, ALI, and the ETM+ of Landsat-7 are provided for Wangqing Forest Bureau, Jilin Province, Northeast China. The data have been radiometrically corrected and geometrically resampled. Feature selection and statistical transforms are used to reduce the Hyperion feature space from 86 channels to 14 features. Classes chosen for discrimination included Larch, Spruce, Oak, Birch, Popular and Mixed forest and other landuses. Classification accuracies have been obtained for each sensor. Comparison of the classification results shows : Hyperion classification results were the best, ALI's were much better than ETM+.

• Advances in aircraft and spacecraft science
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• 제4권3호
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• pp.335-351
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• 2017

Kalman filter based spacecraft attitude estimation has been used in many space missions and has been widely discussed in literature. While some models in spacecraft attitude estimation include spacecraft dynamics, most do not. To our best knowledge, there is no comparison on which model is a better choice. In this paper, we discuss the reasons why spacecraft dynamics should be considered in the Kalman filter based spacecraft attitude estimation problem. We also propose a reduced quaternion spacecraft dynamics model which admits additive noise. Geometry of the reduced quaternion model and the additive noise are discussed. This treatment is easier in computation than the one with full quaternion. Simulations are conducted to verify our claims.

• 우주기술과 응용
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• 제1권2호
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• pp.178-198
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• 2021

국내 태양우주환경 분야에서 널리 이용되는 자료와 모델의 이해와 활용도를 높이고, 세부 분야 간 공동연구의 기회의 장을 마련하고자, 최근 한국우주과학회 태양우주환경분과에서 국내 연구소와 대학을 중심으로 사용되는 태양우주환경 자료와 모델의 보유 및 활용에 대한 조사를 실시했다. 조사 결과를 크게 태양 및 행성간 공간, 자기권, 전리권의 세 분야로 나눠 정리하였고, 본 논문에서는 자기권 분야의 관련 자료와 모델을 소개한다. 자기권 연구의 특성 상 우주공간에서 지점관측을 위한 위성 개발과 운용에 투자가 많이 필요하여 국내 보유 자료는 다른 분야에 비해 상대적으로 적은 편으로 조사됐지만, 국내 지자기관측소를 통한 자기장 변화를 실시간으로 제공하고 있으며, 자기권 모델을 통해 꾸준한 연구를 수행 중이다. 본 논문에서는 자기권 분야 중 국내 위성자료를 이용한 연구들과 제 1원리 물리법칙에 바탕이 된 모델을 대표로 소개한다. 이번 조사 결과와 이를 정리한 논문이 우주과학 관련 자료에 대한 장기적이고 연속적인 관리에 대한 중요성을 인식하며, 우주과학 연구에 참여하는 다양한 인력들이 참조하여 국내에서 생산되고 있는 자료를 활용하여 국내 우주과학 자료의 위상을 높이는데 기여하기를 희망한다. 자료에 대한 조사 내용은 한국우주과학회 홈페이지에서 다운로드할 수 있다(http://ksss.or.kr/).

• Composites Research
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• 제31권3호
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• pp.83-87
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• 2018

An object in the Low Earth Orbit (LEO) is affected by many environmental conditions unlike earth's surface such as, Atomic oxygen (AO), Ultraviolet Radiation (UV), thermal cycling, High Vacuum and Micrometeoroids and Orbital Debris (MMOD) impacts. The effect of all these parameters have to be carefully considered when designing a space structure, as it could be very critical for a space mission. Polybenzimidazole (PBI) is a high performance thermoplastic polymer that could be a suitable material for space missions because of its excellent resistance to these environmental factors. A thin coating of PBI polymer on the carbon epoxy composite laminate (referred as CFRP) was found to improve the energy absorption capability of the laminate in event of a hypervelocity impact. However, the overall efficiency of the shield also depends on other factors like placement and orientation of the laminates, standoff distances and the number of shielding layers. This paper studies the effectiveness of using a PBI coating on the front bumper in a multi-shock shield design for enhanced hypervelocity impact resistance. A thin PBI coating of 43 micron was observed to improve the shielding efficiency of the CFRP laminate by 22.06% when exposed to LEO environment conditions in a simulation chamber. To study the effectiveness of PBI coating in a hypervelocity impact situation, experiments were conducted on the CFRP and the PBI coated CFRP laminates with projectile velocities between 2.2 to 3.2 km/s. It was observed that the mass loss of the CFRP laminates decreased 7% when coated by a thin layer of PBI. However, the study of mass loss and damage area on a witness plate showed CFRP case to have better shielding efficiency than PBI coated CFRP laminate case. Therefore, it is recommended that PBI coating on the front bumper is not so effective in improving the overall hypervelocity impact resistance of the space structure.