• International Journal of Precision Engineering and Manufacturing
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• 제6권4호
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• pp.21-25
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• 2005

In the dynamic analysis of a mechanism, if one or more of the components are flexible, then the simulation will not be accurate because of the violation of the rigid body assumption. Mode shapes are used to represent the dynamic behavior of an elastic structure. A modal synthesis method which uses a combination of normal modes, constraint modes, and attachment modes, was used to represent effectively the elastic deformation of a flexible multibody. Since the combination of these modes should be different for each type of connecting part, the modal synthesis method was studied for the various types of interconnecting joints. In addition, the analysis procedure for the flexible body was explained. A satellite system with flexible solar panels was chosen as an example to show the effectiveness of the proposed method.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2001년도 추계학술대회논문집 II
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• pp.725-730
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• 2001

This paper presents a vibration analysis method for constrained mechanical systems driven by constant generalized speeds. Equilibrium positions are obtained first and vibration analysis are performed around the positions. The method developed in this paper employs partial velocity matrix to obtain a minimum number of differential equations. To verify the accuracy of the proposed algorithm, linear vibration analyses of two numerical examples are performed and the results are compared with results from a commercial program or previous literature.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 1997년도 추계학술대회논문집; 한국과학기술회관; 6 Nov. 1997
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• pp.166-172
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• 1997

In order to find out relationship between hit probability and gun firing of a moving tank, a turret and flexible gun system model has been developed using the recursive flexible multibody dynamics. For a firing simulation model, nodal coordinates for a finite element model of a flexible gun have been employed to include traverse loads to the gun tube due to moving bullet and ballistic pressure. Modal coordinates are also used to represent the motion induced gun vibration before a firing occurs. An efficient switching technique from modal equations to nodal equations has been introduced for an entire gun firing simulation with rotating turret.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2008년도 추계학술대회 논문집
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• pp.358-363
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• 2008

Through this study, 2D multibody dynamics models for analysis of train collisions have been developed to evaluate the crashworthiness requirements of the TSI regulation. The crashworthiness regulation requires some performance requirements for two heavy collision accident scenarios; a train-to-train collision at the relative speed of 36 kph, and a collision against a standard deformable obstacle of 15 ton at 110 kph. The complete train set will be composed of hybrid model with 2D and 1D model. Using numerical analysis of the hybrid model, some crashworthy design were evaluated in terms of mean crush forces and energy absorptions for main crushable structures and devices. especially, 2D model can evaluate overriding effect in train collisions. It is shown from the simulation results that the suggested hybrid model can easily evaluate the crashworthiness requirements.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2014년도 춘계학술대회 논문집
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• pp.275-276
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• 2014

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2013년도 춘계학술대회 논문집
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• pp.634-635
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• 2013

• 대한기계학회논문집A
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• 제39권12호
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• pp.1213-1220
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• 2015

망간단괴를 채집하는 심해저 통합 채광시스템은 채광선, 수직양광관, 중간버퍼, 유연관, 채광로봇으로 구성되어 있다. 최근 심해저 통합 채광시스템 연구에서는 생산성을 극대화하기 위한 다수의 채광로봇으로 구성되는 새로운 다중로봇 통합 채광시스템의 개념이 소개되었다. 본 논문에서는 다중로봇 통합 채광시스템 해석의 효율성을 향상시키고, 다중로봇 시스템의 확장이 이하도록 부분시스템 합성방법이 적되었다. 또한 유연 다물체 동역학이 적된 부분구조로 나눔으로써 수직양광관과 유연관의 대변위가 고려되었다. 일반적인 해석방법과 부분시스템 합성방법의 산술 연산 횟수를 비교함으로써 통합 채광시스템의 부분시스템 합성방법의 이론적인 효율성 연구가 수행되었다.

• 대한기계학회논문집A
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• 제37권4호
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• pp.581-587
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• 2013

반경이 작은 곡선이 종종 존재하는 도시 내에서 운행되는 도시형자기부상열차는 전자석과 레일 사이에 기계적 접촉 없이 곡선주행을 할 수 있어야 한다. 특히, 안내제어가 없는 자기부상열차에 있어서는 승차감을 확보하면서 곡선추종성능을 향상시키기 위하여 차간 댐퍼의 설치가 고려된다. 자기부상 차량용 차간 댐퍼는 곡선 진출입시 차량에 발생하는 요(Yaw) 방향의 진동을 최소화할 수 있어야 함과 동시에, 부상 전자석이 레일과 접촉이 없도록 해야 한다. 본 논문에서는 곡선주행에서의 차간 댐퍼의 승차감과 곡선추종성에의 영향을 분석하는데 목적이 있다. 이를 위하여 부상제어, 차량, 대차 및 궤도가 포함된 동역학 모델을 이용한 동특성 시뮬레이션이 수행된다. 시뮬레이션을 통하여 차간 댐퍼의 효과가 분석되고 시험 선로에서의 주행시험을 실시하여 해석 결과의 신뢰성에 대한 검증이 이루어졌다.

• 대한기계학회논문집A
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• 제40권2호
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• pp.229-236
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• 2016

본 연구에서는 자주박격포의 다물체동역학 모델을 만든 뒤, 포탄의 탄도학을 고려하여 시뮬레이션 하였다. 자주박격포 모델은 박격포 모델 및 차량 모델로 구성하였으며, 상용 다물체 해석 프로그램인 RecurDyn 을 사용하였다. 차량 모델은 6 자유도 강체플랫폼으로 모델링 하였으며, 박격포 발사 직후의 움직임에는 강내탄도학을 적용하였다. 강내탄도학 해석의 결과를 바탕으로, 포신을 떠난 후의 강외탄도 해석을 수행하였다. 몬테카를로 기법을 활용한 반복 해석으로 발사각과 차량 동특성에 의한 변동이 고려된 탄착점의 분산도를 구하여 사격정확도를 제시하였다.

• Advances in aircraft and spacecraft science
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• 제4권5호
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• pp.529-541
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• 2017

Landing phase is one of the crucial and most important phases during robotic aerospace explorations. It concerns the impact of the landing module of a spacecraft on a celestial body. Risks and uncertainties of landing are mainly due to the morphology of the surface, the possible presence of rocks and other obstacles or subsidence. The present work quotes results of a computational analysis direct to investigate the stability during the landing phase of a lander on Phobos, a Mars Moon. The present study makes use of available software tools for the simulation analyses and results processing. Due to the nature of the system under consideration (i.e., large displacements and interaction between several systems), multibody simulations were performed to analyze the lander's behavior after the impact with the celestial body. The landing scenario was chosen as a result of a DOE (Design of Experiments) analysis in terms of lander velocity and position, or ground slope. In order to verify the reliability of the present multibody methodology for this particular aerospace issue, two different software tools were employed in order to emphasize two different ways to simulate the crash-box, a particular component of the system used to cushion the impact. The results show the most important frames of the simulations so as to provide a general idea about how lander behaves in its descent and some trends of the main characteristics of the system. In conclusion, the success of the approach is demonstrated by highlighting that the results (crash-box shortening trend and lander's kinetic energy) are comparable between the two tools and that the stability is ensured.