• 한국군사과학기술학회지
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• 제11권3호
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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.

• 한국공간구조학회논문집
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• 제14권1호
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• pp.93-99
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• 2014

Deployable structure is a system on which the study is being actively performed in various fields including architecture field. However, There is little study which can enhance the practicality since the interpretation condition is difficult as the unstable structure in the architecture field. In this study, the Scissors system has been focused on among the Deployable structure. The structure was developed using the Scissors system and the Mock-up test was performed. Through this, the unfolding method was proposed and the practicability was surveyed through the specific design of the Test model. Also, the structure stability was reviewed through structure analysis of Mock-up test model. and stabilizing method was proposed.

• 한국공간구조학회논문집
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• 제14권3호
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• pp.101-108
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• 2014

Recently, natural disasters such as earthquake, tsunami, typhoon and tornado are increasing, and cause huge economical loses and victim. Thus, when the disaster occurs, it is important to prepare emergency evacuation shelters for fast and easy construction compared to general building system. And, deployable structures will provide a great help for such aim. Deployable structures have the great advantage of being faster and easier to erect and dismantle compared to conventional building forms. In this study, we confirm the possibility of deployment for shelter structures using scissor structure system. First, Basic model was performed to recognize the appllicability of the deployable systems of the dome-shaped structure. Second, Advanced model that more improved inner space and deployment mechanism was confirmed.

• 한국공간정보시스템학회:학술대회논문집
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• 한국공간정보시스템학회 2004년도 춘계 학술발표회 논문집 제1권1호(통권1호)
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• pp.176-183
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• 2004

Deployable structures are space frames consisting of straight bars that are linked together into bundle and can be deployed large, load bearing structures. Deployable structures are easy to set up, to assemble, to disassemble, to transport and to keep for the use. Also, reusability and flexibility are another important advantages for environmental matter. Since deployable structures have various advantages, they offer viable alternatives for a wide range of potential applications in the temporary construction industry as well as in the aerospace industry. The purpose of this thesis is to decide on geometrical parameters of the design through the numerical analysis and create a final configuration of deployable structures using the geometrical parameters. The Multibody Dynamic Analysis that is dealt with mechanics and aeronautics is used for the method of analysis.

• 한국항공우주학회지
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• 제42권8호
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• pp.701-706
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• 2014

최근 인공위성 연구는 "Faster, Smaller, Better, Cheaper"라는 슬로건 하에 나노급, 마이크로급 인공위성 개발, 복수위성 발사 등에 대한 연구가 활발히 진행되고 있다. 광학구조체는 인공위성에서 대부분의 비율을 차지하며, 이를 축소하기 위한 방안으로 광학구조체에 전개 메커니즘을 접목시킨 전개형 광학구조체에 대한 연구가 각광받고 있다. 본 논문에서는 기존 고정형 광학구조체의 요구조건을 바탕으로 전개형 광학구조체 전개 시 정렬 정밀도를 제안하고, 이 정밀도를 만족시킬 수 있는 전개 메커니즘 후보를 제안하였다. 또한 기구학적 해석을 수행하여, 위성의 광학성능에 영향을 미치는 미러 사이의 tilt, de-space, de-center중, 기구의 입력 오차에 의하여 발생될 수 있는 기구장치의 de-space 정밀도를 평가하였다.

• Advances in aircraft and spacecraft science
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• 제9권2호
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• pp.103-117
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• 2022

In this paper, a novel morphing mechanism using a deployable scissor structure was proposed for a variable camber morphing wing. The mechanism was designed through the optimization process so that the rib can form the target airfoils with different cambers. Lastly, the morphing wing was manufactured and its performance was successfully evaluated. The mechanism of the morphing wing rib was realized by a set of deployable scissor structure that can form diverse curvatures. This characteristic of the structure allows the mechanism to vary the camber that refers to the airfoil's curvature. The mechanism is not restrictive in defining the target shapes, allowing various airfoils and overall morphing wing shape to be implemented.

• 한국공간구조학회논문집
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• 제8권4호
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• pp.57-64
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• 2008

본 연구는 설치와 해체가 용이하여 간이식 구조에서 활용되는 시저스 전개형 구조에 관한 것으로, 입면상의 곡률변화 방법을 고찰하고 그에 따른 구조특성을 파악하고자 한 것이다. 먼저 시저스 구조의 입면상 곡률과 시저스부재의 내부절점 편심거리와의 관계를 식과 그래프를 이용하여 나타내었다. 이에 따라, 동일한 시저스부재에서 내부절점 편심거리를 조절하여 곡률을 변화시킬 수 있는 해석모델을 고찰함으로써, 곡률변화에 따른 시저스 구조부재들의 구조적 특성을 고찰하였다. 또한 고찰된 구성방식에 근거하여 실 모델을 제작하고 전개과정을 살펴봄으로써 실제 전개가능성을 검토하였다.

• 한국공간구조학회논문집
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• 제17권4호
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• pp.133-140
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• 2017

Recently, the interest in the smart buildings is increasing in the architecture field. Among them, a research of facade design using a transformable system that can adjust the effect of the external environment is in progress. One of a typical example of the deployable system is a Scissors system that can change shape by using the geometric conditions of a unit member. Scissors system is a high-tech structural system which can construct the deployable plan and curved space by using the SLE (Scissors-Like Element) consisted of two Bar and Pivot. If the facade is designed by applying Scissors system, it is possible to maximize the performance and aesthetic effect of the structure by using a shape change of the line member. This paper presents a study of deployable facade design applying hybrid-typed Scissors system. A new deployable pattern of facade design is developed by combining Angulated Scissors system and tessellation pattern. Applying the deployable pattern a double skin construction method which is to add an outer wall for design, it raises three dimensional effects and can maximize the artistic essence of the change in shape upon deployment.

• Structural Engineering and Mechanics
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• 제54권6호
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• pp.1153-1174
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• 2015

Deployable structures have gained more and more applications in space and civil structures, while it takes a large amount of computational resources to analyze this kind of multibody systems using common analysis methods. This paper presents a new approach for dynamic analysis of multibody systems consisting of both rigid bars and arbitrarily shaped rigid bodies. The bars and rigid bodies are connected through their nodes by ideal pin joints, which are usually fundamental components of deployable structures. Utilizing the Moore-Penrose generalized inverse matrix, equations of motion and constraint equations of the bars and rigid bodies are formulated with nodal Cartesian coordinates as unknowns. Based on the constraint equations, the nodal displacements are expressed as linear combination of the independent modes of the rigid body displacements, i.e., the null space orthogonal basis of the constraint matrix. The proposed method has less unknowns and a simple formulation compared with common multibody dynamic methods. An analysis program for the proposed method is developed, and its validity and efficiency are investigated by analyses of several representative numerical examples, where good accuracy and efficiency are demonstrated through comparison with commercial software package ADAMS.

• 한국항공우주학회지
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• 제47권6호
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• pp.405-413
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• 2019

전개형 구조물은 크기와 모양의 변형이 가능하여 수납과 이동이 용이한 장점으로 인해 우주 임무에 많이 사용된다. 특히, 우주에서 사용되는 구조물들의 경우에는 운용과정에서 직면하는 다양한 외란들을 견디기 위하여 높은 구조 강성을 가지도록 설계되어야 한다. 특히 전개형 구조물의 경우, 구조 경량화를 위하여 얇고 가벼운 소재를 사용하는 경우가 많기 때문에 전개 과정에서 발생하는 내력이나 전개 완료 상태에서의 구조 강성 등에 대한 면밀한 분석이 수행되어야 한다. 본 논문에서는 전개형 구조물 중에서 널리 사용되는 시저스 구조물에 대해 동역학적 모델을 수립하고 전개 속도, 각 조인트에 걸리는 내력 등 전개 거동을 분석한다. 또한, 구조물의 전개 완료 형상에 따른 구조 강성 변화를 분석하기 위하여 1단과 2단 두 가지 형상에 대해 모드 해석을 수행하였으며, 저차 모드의 모드 형상 및 고유 진동수 변화를 확인하고 변화의 원인을 고찰하였다.