• Title/Summary/Keyword: 충돌동역학

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Study on a 2-Dimensional Dynamic Modeling Technique to Analyze the Overriding Phenomena of Rollingstock (열차의 타고오름 해석을 위한 2차원 충돌동역학 모델링 기법 연구)

  • Kim, Geo-Young;Koo, Jeong-Seo;Kwon, Tae-Soo
    • Journal of the Korean Society for Railway
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    • v.14 no.1
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    • pp.11-18
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    • 2011
  • This paper proposed a new 2-D multi-body dynamic modeling technique to analyze overriding behaviors taking place during train collision. This dynamic model is composed of nonlinear springs, dampers and masses by considering the deformable characteristics of carbodies as well as energy absorbing structures and components. By solving this dynamic model for rollingstock, energy absorbing capacities of collision elements, accelerations of passenger sections, impact forces applied to interconnecting devices, and overriding displacements can be well estimated. For a case study, we chose KHST (Korean High Speed Train), obtained crush characteristic data of each carbody section from 3-D finite element analysis, and established a 2-D multi-body dynamic model. This 2-D dynamic model was simulated under the train-to-train collision scenarios, and evaluated with 3-D virtual testing model. It was founded from the simulation results that this 2-D dynamic model could well predict overriding behaviors, and the modeling technique of carbody deformation was very important in overriding estimation.

Rigid Body Dynamic Analysis on the Spent Nuclear Fuel Disposal Canister under Accidental Drop and Impact to the Ground: Theory (사고로 지면으로 추락낙하 충돌하는 고준위폐기물 처분용기에 대한 기구동역학 해석: 이론)

  • Kwon, Young-Joo
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.26 no.5
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    • pp.359-371
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    • 2013
  • This paper is the first paper among two papers which constitute the paper about the rigid body dynamic analysis on the spent nuclear disposal canister under accidental drop and impact on to the ground. This paper performed the general theoretical study on the rigid body dynamic analysis. Through this study the impulsive force which is occurring in the spent nuclear fuel disposal canister under accidental drop and impact to the ground and required for the structural safety design of the canister is intended to be theoretically formulated. The main content of the theoretical study is about the equation of motion in the multibody dynamics. On the basis of this study the impulsive force which is occurring in the multibody in the case of collision between multibody is theoretically formulated. The application of this theoretically formulated impulsive force to computing the impulsive force occurring in the spent nuclear fuel disposal canister under accidental drop and impact to the ground is investigated.

Equivalent Modeling Technique for 1-D Collision Dynamics Using 3-D Finite Element Analysis of Rollingstock (열차의 3차원 유한요소해석을 이용한 1차원충돌 동역학 등가 모델링 기법)

  • Park, Min-Young;Park, Young-Il;Koo, Jeong-Seo
    • Journal of the Korean Society for Railway
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    • v.13 no.2
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    • pp.139-146
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    • 2010
  • In this study, a new equivalent modeling technique of rollingstock for 1-D collision dynamics was proposed using crash analysis of 3-D finite element model in some detail. To obtain good simulation results of 1-D dynamic model, the force-deformation curves of crushable structures should be well modelled with crash analysis of 3-D finite element model. Up to now, the force-deformation curves of the crushable structures have been extracted from crash analyses of sectionally partitioned parts of the carbody, and integrated into 1-D dynamic model. However, the results of the 1-D model were not satisfactory in terms of crash accelerations. To improve this problem, the force-deformation curves of the crushable structures were extracted from collision analysis of a simplified train consist in this study. A comparative study applying the suggested technique shows in good agreements in simulation results between two models for KHST.

Longitudinal Motion Planning of Autonomous Vehicle for Pedestrian Collision Avoidance (보행자 충돌 회피를 위한 자율주행 차량의 종방향 거동 계획)

  • Kim, Yujin;Moon, Jongsik;Jeong, Yonghwan;Yi, Kyongsu
    • Journal of Auto-vehicle Safety Association
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    • v.11 no.3
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    • pp.37-42
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    • 2019
  • This paper presents an autonomous acceleration planning algorithm for pedestrian collision avoidance at urban. Various scenarios between pedestrians and a vehicle are designed to maneuver the planning algorithm. To simulate the scenarios, we analyze pedestrian's behavior and identify limitations of fusion sensors, lidar and vision camera. Acceleration is optimally determined by considering TTC (Time To Collision) and pedestrian's intention. Pedestrian's crossing intention is estimated for quick control decision to minimize full-braking situation, based on their velocity and position change. Feasibility of the proposed algorithm is verified by simulations using Carsim and Simulink, and comparisons with actual driving data.

Rigid Body Dynamic Analysis on the Spent Nuclear Fuel Disposal Canister under Accidental Drop and Impact to the Ground: Numerical analysis (사고로 지면으로 추락낙하 충돌하는 고준위폐기물 처분용기에 대한 기구동역학 해석: 수치해석)

  • Kwon, Young-Joo
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.26 no.5
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    • pp.373-384
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    • 2013
  • This paper is the second paper among two papers which constitute the paper about the rigid body dynamic analysis on the spent nuclear fuel disposal canister under accidental drop and impact to the ground. This paper performed the numerical study on the rigid body dynamic analysis. Through this study the impulsive force which is occurring in the spent nuclear fuel disposal canister under accidental drop and impact to the ground and required for the structural safety design of the canister is computed numerically. The main content of this numerical study is about the technical method how to compute the impulsive forces occurring in the canister under accidental drop and impact to the ground by using the commercial rigid body dynamic analysis computer codes. On the basis of this study the impulsive force which is occurring in the canister in the case of collision with the ground is numerically computed. This numerically computed impulsive force is increasing as the canister weight is increasing, and the canister falls plumb down and collides with the ground in three types according to the analysis results.

Optimal Terminal Guidance Law for BTT Missiles Considering Impact-Angle Constraint of Stationary Target (정지 표적의 표적 충돌각을 고려한 BTT 미사일의 최적 종말 유도 법칙 설계)

  • Yeom, Joon-Hyung;Park, Sung-Min;Ha, In-Joong
    • Proceedings of the KIEE Conference
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    • 2009.07a
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    • pp.1737_1738
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    • 2009
  • 미사일의 표적 충돌각을 원하는 각도로 제어하는 것은 표적의 취약점을 공략하기 위해 필수적인 기술이다. 표적 타격 지점 및 충돌각을 고려하지 않으면 타격에 성공하였다고 하더라도 표적의 방어 능력이 좋거나 신관이 충돌각에 민감하면 표적의 효과적인 파괴에 실패할 수도 있다. 이런 경우 유도 미사일의 종말 유도 효율을 증가시키기 위해 미사일이 표적을 타격하는 각도인 표적 충돌각(Impact Angle)을 제어할 수 있으면 적정 비행경로의 설정에 유리하고 우회공격 등이 가능할 뿐 아니라 미사일 탄두의 효과를 극대화할 수 있다. 하지만 이러한 장점을 갖는 표적 충돌각 유도 기법에 대한 연구는 아직 활발하게 행해지고 있지는 못하다. 기존 연구 결과들은 2차원 평면상에서의 충돌각 제어만을 다루고 있어, 요와 피치 채널의 커플링 문제가 있는 BTT 미사일에 적용하기가 어렵다는 문제점을 갖고 있다. 또한 미사일 동역학을 무시하거나 단순화하여 문제를 풀고 있기 때문에 실제 상황에 적용이 어렵다는 단점이 있다. 본 논문에서는 3차원 공간상에서의 롤 명령을 모두 포함하면서 동시에 미사일 자동조종제어기, 핀 구동기 동역학을 모두 고려한 새로운 BTT 미사일의 표적 충돌각 유도 기법을 제안한다.

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Numerical Modeling of the Detonation of Explosives Using Hydrodynamics Codes (유체 동역학 코드를 이용한 화약의 폭발과정에 대한 수치 모델링)

  • Park, Dohyun;Choi, Byung-Hee
    • Explosives and Blasting
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    • v.34 no.2
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    • pp.31-38
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    • 2016
  • The hydrodynamics code is a numerical tool developed for modeling high velocity impacts where the materials are assumed to behave like fluids. The hydrodynamics code is widely used for solving impact problems, such as rock blasting using explosives. For a realistic simulation of rock blasting, it is necessary to model explosives numerically so that the interaction problem between rock and explosives can be solved in a fully coupled manner. The equation of state of explosives, which describes the state of the material under given physical conditions, should be established. In this paper, we introduced the hydrodynamics code used for explosion process modeling, the equation of state of explosives, and the determination of associated parameters.

A Study on the Silicon Damages and Ultra-Low Energy Boron Ion Implantation using Classical Molecular Dynamics Simulation (고전 분자 동 역학 시뮬레이션을 이용한 실리콘 격자 손상과 극 저 에너지 붕소 이온 주입에 관한 연구)

  • 강정원;강유석;손명식;변기량;황호정
    • Journal of the Korean Institute of Telematics and Electronics D
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    • v.35D no.12
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    • pp.30-40
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    • 1998
  • We have calculated ultra-low energy silicon-self ion implantations and silicon damages through classical molecular dynamics simulation using empirical potentials. We tested whether the recently developed Environment-Dependent Interatomic Potential(EDIP) was suitable for ultra low energy ion implantation simulation, and found that point defects formation energies were in good agreement with other theoretical calculations, but the calculated vacancy migration energy was overestimated. Most of the damages that are produced by collision cascades are concentrated into amorphous-like pockets. Also, We upgraded MDRANGE code for silicon ion implantation process simulation. We simulated ultra-low energy boron ion implantation, 200eV, 500eV, and 1000eV respectively, and calculated boron profiles with silicon substrate temperature and tilt angle. We investigated that below 1000eV, channeling effect must be considered.

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Analytical Closed Form Solution for the Impact Load of a Collision between Rigid Bodies and its Application to a Spent Nuclear Fuel Disposal Canister Accidentally Dropped and Impacted on the Ground: Application(Numerical Analysis) (강체간의 충돌에 의한 충격력에 대한 수학적 정해 및 고준위폐기물 처분용기의 지면 추락낙하사고 시의 충돌충격에의 응용: 적용(수치해석))

  • Kwon, Young-Joo
    • Journal of the Computational Structural Engineering Institute of Korea
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    • v.28 no.5
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    • pp.451-457
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    • 2015
  • This paper presents the analytical closed form solution for the impact load of a collision between rigid bodies and its application to a spent nuclear fuel disposal canister accidentally dropped and impacted on the ground. This paper performed a study on the numerical rigid body dynamic analysis to compute the impact load between two rigid bodies, especially, the impulsive force which is applied to the spent nuclear fuel disposal canister in the accidental drop and impact event on the ground. Through this study the impulsive force which is occurring in the spent nuclear fuel disposal canister under accidental drop and impact event on the ground and required in the process of structural safety design of the canister is computed numerically. The main content of this numerical study is about the technical method how to compute the impulsive force applied to the canister under the accidental drop and impact event on the ground by using the commercial computer code for the rigid body dynamic analysis. On the basis of this study a problem to compute the impulsive force which is occurring in the canister in the case of collision with the ground is numerically treated. This numerically computed impulsive force is compared with the theoretical value, which shows a good agreement.

A Study on the Damage of Satellite caused by Hypervelocity Impact with Orbital Debris (우주파편 초고속충돌에 의한 위성구조체의 손상에 관한 연구)

  • Kang, Pil-Seong;Im, Chan-Kyung;Youn, Sung-Kie;Lim, Jae-Hyuk;Hwang, Do-Soon
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.7
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    • pp.555-563
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    • 2012
  • In earth orbit, a great number of orbital debris move around in extremely high velocity, and they become serious threats to satellites. In this study, smoothed particle hydrodynamics(SPH) is used to analyze the damage of a low earth orbit satellite due to the hypervelocity impact with orbital debris. The damage of honeycomb sandwich panel(HC/SP) used for walls of a satellite is analyzed with respect to impact velocities. For the additional analysis to examine the safety of interior components of the satellite, an attached electronic box and an offset electronic box are considered. As a result of the analysis considering the orbital debris having a probability of collision more than 2% at altitude of 685km, it is shown that the HC/SP can be perforated but only small craters are formed on both the attached electronic box and the offset electronic box.