• The Journal of Korean Institute of Information Technology
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• v.16 no.12
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• pp.41-47
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• 2018

The buoy-enabled underwater surveillance system is a device that is installed in a particular sea area and operated for a certain period of tine and moved to another sea area after recovery. In this paper, a mooring method which is applied for a buoy-enabled underwater surveillance system was selected to maintain installation and enure stable operation. Also, the structure of the mooring line was designed. Two-point mooring method was selected considering interference with the communication cable of array-assembly. The composite structure of buoy chain, nylon rope, and anchor chain is designed as the basic component of mooring line. For the verification of design, a numerical simulation and wave tank experiment were performed. Their results were confirmed similarity in test condition. Finally, the mooring lines were designed for the environment of the sea trial location. The mooring line produced by the final design confirmed the stability above the significant wave height considered in the design on the sea trial.

• The KIPS Transactions:PartD
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• v.8D no.6
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• pp.691-698
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• 2001

Component-based development methods are regarded as one of the most important tools for us to cope with ever-increasing software complexity and, at the same time, to improve productivity in software development. This paper presents how to generate test-cases for integrated software from those of member components and how to validate composition of components, by the analysis of domain relations of components. This paper shows the applicability of the proposed technique by the real experiment. This study is based on the dataflow systems architecture and process components, and the technique developed here is an application of domain testing technique.

• Journal of the Korean Geotechnical Society
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• v.25 no.12
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• pp.57-67
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• 2009

Along with the advanced construction technologies, the maximum size of coarse aggregate used for dam construction ranges from several cm to 1m. Testing the original gradation samples is not only expensive but also causes many technical difficulties. Generally, indoor tests are performed on the samples with the parallel grading method after which the results are applied to the design and interpretation of the actual geotechnical structure. In order to anticipate the exact behavior characteristics for the geotechnical structure, it is necessary to understand the changes in the shear behavior. In this study, the Large Triaxial Test was performed on the parallel grading method samples that were restructured with river bed sand-gravel, with a different maximum size, which is the material that was used to construct Dam B in Korea. And the Stress - Strain characteristics of the parallel grading method samples and the characteristics of the shear strength were compared and analyzed. In the test results, the coarse-grained showed strain softening and expansion behavior of the volume, which became more obvious as the maximum size increased. The internal angle of friction and the shear strength appeared to increase as the maximum size of the parallel grading method sample increased.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.37 no.4
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• pp.275-282
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• 2024

A recently proposed rapid-disassembly , carbon-minimized dismantle connection was tested using cyclic loading. To better understand the behavior of the test specimen, three-dimensional finite element (3D-FE) analyses were conducted using a "tied model" (bolted contact surfaces are tied together) and a "bolt-slip model" (contact surfaces slip and separate). The tied model suggests that plastic hinging of the beam occurs if the proposed connection behaves rigidly. The bolt-slip model suggests that the proposed connection, if manufactured and assembled properly, can dissipate energy to about 0.5 times that experienced by a rigid connection. However, when compared in a test, its moment-rotation hysteresis curve does not match well, which suggests that the low performance of the test specimen is attributable to a manufacturing deficiency. Regardless, the results corroborate the pinching phenomenon observed in the experimental hysteresis and fracture failure of the test specimen.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.43 no.5
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• pp.432-439
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• 2015

MEMS solid thruster module is composed of solid thruster and its control board. It was developed for the purpose of an academic research. Therefore, thermo-mechanical design and verification for space usage were not considered in the design phase. To mount it on a cube satellite without any design modification, technical efforts at the system level structure design is required. In this study, we proposed a structural design concept to mount the MEMS thruster module by using brackets for guaranteeing structure safety under launch loads and easier mating and de-mating of MEMS thruster module during test phase. The effectiveness of the design has been verified through structural analysis and vibration test. In addition, electrical connection method using spring pins between MEMS thruster and control board is effective for guaranteeing the structural safety under launch vibration loads.

• Journal of Korea Society of Industrial Information Systems
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• v.13 no.2
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• pp.18-27
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• 2008

In recent years, the functions added ta an embedded system have grown various and complex in most parts of the applications. Embedded software comes to include more functions and is getting bigger. Therefore it is getting difficult for software developers to keep the development time to market on time. This leads to a need for adequate design and test technique for embedded software. In this paper, we propose a software architecture style for embedded software. It facilitates the composition of reusable functions and helps developers reduce development time. We also propose a test method and tools for embedded software running on target systems.

• 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.45 no.4
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• pp.292-299
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• 2017

The KUH-1's Wheel Brake Assembly which is Brake System is an essential component to perform flight mission for pilot. It has function of taxing, differential braking and parking to sustain landing capability. However, the skid and abrasion of tire were occurred in mass-produce operation. Also, if it is occurred on the ground, the flight can not be performed. In this case, the defect is a major cause of the decrease in the operation rate of aircraft. In this paper, the cause of the defect in flight was identified and the failure process was organized. Also, it describes design improvements which was derived from troubleshooting and suggests verification results of flight test.

• Proceedings of the KIPE Conference
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• 2000.07a
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• pp.693-696
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• 2000

군사용 전동기는 고속 고출력 고신뢰성 저소음의 특징을 갖고 있어야 하며 이러한 성능을 구현하기 위한 전동기/드라이브의 설계 및 제조 시험은 일반적인 전동기 인버터 구조와는 많이 상이하다 우선 7상6극의 전동기 특성을 갖고 있어 같은 상전류에 대해 3상 전동기보다 높은 출력을 얻을 수 있어 동일출력의 3상제어반에 비해 적응 용량의 전력소자를 분산시킬수 있으므로 조립이 용이하다 또한 전류 리플을 동일 용량의 3상 전동기에 비해 약 2배 가량 감소시킬 수 있다 고속(25,000ppm) 회전을 통해 체적대비 출력을 극대화 하여 3kW/Kg으로 세계적인 수준에 도달된 상태이다 본논문에서는 한정된 전원전압 전류 범위 공간등의 제한하에서 목표 출력과 성능이 나올수 있는 드라이브구성 및 제어 알고리즘 시험결과를 기술한다.

• Satellite Communications and Space Industry
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• v.13 no.1 s.28
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• pp.72-80
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• 2006

통신해양기상위성은 기상관측, 해양관측 및 통신방송의 3가지 임무를 수행하는 정지궤도 복합임무 위성이다. 위성본체는 기존의 화성탐사선(Mars Express) 위성의 구조를 확장하여 새로 개발한 구조체에 기존의 E3000 통신위성 버스에 사용하였던 전기전자 부품 및 추진계를 사용한다. 3축제어 위성으로서 태양전지판은 한 쪽에만 부착되어 있으며, 반대쪽에는 종래의 기상위성이 모멘트 균형을 위하여 갖고 있었던 솔라세일(solar sail)을 갖고 있지 않다. 기상탑재체는 미국의 아이티티(ITT)가 제작 공급하고, 해양탑재체는 이에이디에스 아스트리움(EADS Astrium)사와 항공우주연구원이 공동으로 개발하며, 통신 탑재체는 전자통신연구원에서 개발한다. 지상국은 항공우주연구원이, 관제시스템은 전자통신연구원이 개발을 담당하고 있다. 개발의 전 과정이 해외협력 개발로 이루어진다. 설계는 프랑스의 뚤르즈 소재 이에이디에스 아스트리움(EADS Astrium)사에서 한국 기술진의 참여 하에 이루어지며, 조립 및 시험은 항공우주연구원의 시설을 이용하여 한국에서 이루어진다. 발사준비도 공동으로 수행하고, 발사 후 전이궤도운영은 아스트리움사의 지상국을 사용하여 수행하여 목표궤도에 진입시킨 후 항공우주연구원의 지상국에서 궤도 내 시험(in-orbit-test)를 완료한 후 위성을 인도 받는다.