• Title/Summary/Keyword: Deployment Analysis

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Dynamic Analysis of a Deployable Space Structure Using Passive Deployment Mechanism (수동형 전개힌지를 이용한 전개형 우주 구조물의 전개 동특성 해석)

  • Choi, Young-Jun;Oh, Hyun-Ung;Choi, Yong-Hoon;Lee, Kyung-Joo
    • Journal of the Korea Institute of Military Science and Technology
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    • v.11 no.3
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    • pp.161-168
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    • 2008
  • The deployable space structure is necessary to minimize the satellite volume and launch cost. For the deployment, passive deployment mechanism has widely been used to attenuate a latch shock induced when the structure is just fully deployed. To reduce the latch shock, viscous damper is applied to the passive deployment mechanism and it can control the deployment speed of the structure. In this paper, dynamic analysis of the deployable space structure using the passive deployment mechanism with the viscous damper has been performed. The viscous damping values have been optimized through numerical simulation. The satellite's attitude influenced by pyro activation for the release of the structure has also been investigated.

Analysis on Deployment of Fire Service Force in Korea (한국 소방력배치의 실태 분석)

  • Back, Min-Ho;Lee, Hae-Pyeong
    • Fire Science and Engineering
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    • v.20 no.1 s.61
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    • pp.55-70
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    • 2006
  • The purpose of this study is to analyze an adequate deployment of fire service force to be prepared to respond appropriately and effectively in Korea by settlement pattern. In order to examine the deployment of fire service force by the present standard, we analyzed the logical basis and the deployment of fire service force by city and province. We also classified clusters for settlement pattern through the statistical methods and raised several points for the existing deployment model of fire service force by the classified settlement pattern. As a result, it was confirmed that the deployment of fire service force by the settlement pattern was irrelevant to fire service need.

Analysis of Folding Wing Deployment with Aero and Restraint Effects (공기력 및 구속 효과를 고려한 접힘 날개 전개 성능 분석)

  • Kim, Seung-il
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.6
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    • pp.533-539
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    • 2015
  • Recently, guided missiles applies folding wings to save space. During wing deployment, aero force acting on wing effects significantly on deployment performance, usually aerodynamic coefficient are calculated by CFD analysis. However, Missile Datcom can calculates estimated aerodynamic coefficient very quickly by assuming wing deployment motions as dihedral angle of wing. If missile has external store, wings may need to be folded on top of each other. In this case, one of wing help or interrupt other wing deployment, locking effect. In this study, both effects were included on wing deployment performance analysis to criteria for wings locked condition and formulated wing deploy performance, and compared with wind tunnel test data. Analysis predicted vulnerable wind direction of wing deployment very well.

A Study on Improvement of Fire Service Deployment Standard in Korea (한국 소방력배치 기준의 개선에 관한 연구)

  • Lee, Hae-Pyeong;Back, Min-Ho
    • Fire Science and Engineering
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    • v.20 no.1 s.61
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    • pp.28-42
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    • 2006
  • The purpose of this study is to offer the improvement for deployment of fire service force in Korea by settlement patterns on the basis of analysis for the present standard and deployment of fire service force. For the adequate deployment and operation of fire service force by settlement patterns, we carried out the analysis of the present standard calculated with allocation of the authorized strength. We also classified clusters for settlement pattern through the statistical methods. We proposed the standard for deployment of fire service force reflected with environmental and need factors through the introduction of standardized index.

Solar Array Deployment Analysis of a Satellite (인공위성 태양전지판 전개해석)

  • Kim, Kyung-Won;Kim, Sun-Won;Lim, Jae-Hyuk;Rhee, Ju-Hun;Hwang, Do-Soon;Jin, Ik-Min;Kim, Hak-Jung;Song, Woon-Hyung;Choi, Hang-Suk
    • Journal of Satellite, Information and Communications
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    • v.3 no.1
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    • pp.29-34
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    • 2008
  • After spacecraft is separated from the launch vehicle, first of all spacecraft deploy the solar array. Solar array deployment is one of the key factors deciding the success of the spacecraft mission. Therefore, It is necessary to predict the solar array deployment motion and check the safety through calculating the load on the tape hinges of solar array using the deployment analysis in the initial design phase. In this paper, solar array deployment analysis is performed by multi-body dynamics simulation program. From the analysis results, assessment on the safety also is carried out. In addition, hinge characteristic test is fulfilled to find out hinge characteristic, and is applied to the deployment analysis.

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A Study on Factors for Influence SW Development Productivity on The IT Service Company (IT Service기업의 Software개발 생산성 영향 요인에 관한 실증 연구 : SW개발 방법론 중심으로)

  • Song, Young-Woon;Kim, Wanki
    • Journal of Information Technology Services
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    • v.13 no.2
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    • pp.195-217
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    • 2014
  • This paper has explored when implementing SW development project of the IT service corporations, what factors affect its productivity in SW development methodology. The importance of the AHP analysis surveyed from the experts in IT service companies and related committee, was shown in the order of the following processes : 1) Deployment process 2) Management process 3) Establishment process. It is measured the methodology levels of establishment, deployment and management in each project using the survey results collected from project execution members and analyzed the productivity of projects that have been executed within 2 years. Using project methodology level, productivity correlation analysis, and regression analysis, this study confirms that the methodology deployment level brings positive effects significantly to SW development productivity. The significance of this study would be not only to research and analyze SW development productivity using the real project execution data but also to underline the necessities and the importance of steady research, deployment and support for SW development productivity improvement.

A Study on the Construction of Function Tree using Function Deployment (기능 전개 결과를 이용한 Function Tree 구성에 관한 연구)

  • 하성도;이언경;박선주;강달모
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 2000.11a
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    • pp.401-406
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    • 2000
  • Fault tree analysis (FTA) is a widely used methodology for reliability analysis. The method is useful in that it suggests a very comprehensive way of describing the hierarchical relations of causes of faults and the corresponding results. However it is difficult to get appropriate fault trees for given products or systems without very profound knowledge and experience. This work aims to develop a methodology of fault tree construction using the results of function deployment for machine parts, which provides an objective way of preparing fault trees. The failure modes are defined to each function network generated by the function deployment method and the fault tree with respect to each viewpoint is constructed by arranging the failure modes. The fault tree is finally obtained by synthesizing the fault trees with respect to each viewpoint. The example of fault tree construction is also shown.

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Implementation Options and Economics of Phased UMTS Deployment

  • Grillo, Davide;Montagna, Maurizio;Alfano, Franco;Colombo, Antonio;Ricci, Simone
    • Journal of Communications and Networks
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    • v.4 no.4
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    • pp.282-291
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    • 2002
  • 3GPP (Third Generation Partnership Project) is defining UMTS (Universal Mobile Telecommunication System) releases which span the transition from GSM/UMTS coexistence to All-IP UMTS networks. The deployment of an UMTS network depends, in the first place, on the intended service offerings and the release an operator chooses to start service with. Other key decisions in-fluencing UMTS deployment relate to the timing of the functional enhancements and capacity increases along the economic life of the network. This paper gives an overview on the architectural and technical options for UMTS deployment. It also outlines the methodology underlying the business plan aimed at estimating the returns from investments in the UMTS infrastructure, thus helping to tune operators’ strategies for UMTS deployment.

A Study on the Solar Panel Deployment of a Satellite (인공위성 태양전지판의 전개에 관한 연구)

  • Seo, Jong Hwi;Han, Sang Won;Park, Tae Won;Chae, Jang Su;Seo, Hyeon Seok
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.4
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    • pp.53-59
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    • 2003
  • Strain Energy Hinge(SEH) has been used in Korea Multi-purpose Satellite(KOMPSAT) series to deploy the solar panel due to the good record of reliability. However, when it reached a desired deployment position, a large buckling force is applied to the main body. This may cause structural damage and also affect control of the satellite. Therefore, reliable dynamic analysis for the deployment system is required at a design stage. Moreover, various mission of a satellite has made the size of solar panels got bigger, so elastic effect has to be considered seriously to get more precise analysis results. In this paper, a dynamic analysis method to predict the deployment is verified by KOMPSAT-2 deployment test.

Applying QDRD for Safety Products Design (제품안전설계를 위한 QDRD의 적용)

  • Jung, Won;Kim, Jun-Hong;Yoo, Wang-Jin
    • Journal of Korean Society for Quality Management
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    • v.30 no.4
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    • pp.164-173
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    • 2002
  • The first product liability laws went into effect in Korea in July 2002. A person who suffers personal injury or damage to property due to defects in a product may sue both the manufacturer and the seller of the product under the principles of Korea tort law. This paper presents an integrated methodology which is called the QDRD(Quality deployment and reliability deployment) for hazards analysis in new product designs. QDRD applies QFD, FMEA and FTA to identify the hazards component, hazardous situations and hazardous events which could lead to an accident. An example is provided to demonstrate hazards analysis on a product using the QDRD method.