• International Journal of Naval Architecture and Ocean Engineering
• /
• 제5권2호
• /
• pp.188-198
• /
• 2013

In constructing a collision avoidance system, it is important to determine the time for starting collision avoidance maneuver. Many researchers have attempted to formulate various indices by applying a range of techniques. Among these indices, collision risk obtained by combining Distance to the Closest Point of Approach (DCPA) and Time to the Closest Point of Approach (TCPA) information with fuzzy theory is mostly used. However, the collision risk has a limit, in that membership functions of DCPA and TCPA are empirically determined. In addition, the collision risk is not able to consider several critical collision conditions where the target ship fails to take appropriate actions. It is therefore necessary to design a new concept based on logical approaches. In this paper, a collision ratio is proposed, which is the expected ratio of unavoidable paths to total paths under suitably characterized operation conditions. Total paths are determined by considering categories such as action space and methodology of avoidance. The International Regulations for Preventing Collisions at Sea (1972) and collision avoidance rules (2001) are considered to solve the slower ship's dilemma. Different methods which are based on a constant speed model and simulated speed model are used to calculate the relative positions between own ship and target ship. In the simulated speed model, fuzzy control is applied to determination of command rudder angle. At various encounter situations, the time histories of the collision ratio based on the simulated speed model are compared with those based on the constant speed model.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2008년도 춘계학술대회논문집
• /
• pp.320-323
• /
• 2008

In this study the effect of collision model was evaluated in spray field by CFD. A collision is basically the interaction between droplets and criteria of collision is determined by drop Weber number, impact parameter, and drop-size ratio. Early developed collision model considered coalescence and grazing collision with the exchange of momentum. However in experimental research there were bouncing, coalescence, reflexive separating and stretching separating in interaction between droplets. In this study the collision considering such complex phenomena is modeled and was compared with the basic collision model.

• 한국통신학회논문지
• /
• 제33권8A호
• /
• pp.794-804
• /
• 2008

본 논문에서는 EPCglobal Class-1 Generation-2 (Gen2) 기반 Probabilistic Slotted 충돌방지 알고리즘에 대하여 살펴보고, 태그인식시간, 충돌 비율을 감소시키고, 데이터 처리량, 시스템 효율을 증가 시킬 수 있는 QueryAdjust 명령어를 사용한 FAFQ (fixed adjustable framed Q) 알고리즘과 AAFQ (adaptive adjustable framed Q) 알고리즘을 제안하며, 또한 Gen2 기반으로 태그 인식 효율을 향상 시킬 수 있는 Grouping 방법을 제안한다. 제안한 방법들 모두 Q 알고리즘의 성능 향상을 보이며, 제안하는 방법 중 AAFQ 알고리즘이 가장 높은 성능 향상을 나타낸다. 즉, AAFQ 알고리즘에 의하여 5% 정도의 시스템 효율 성능 향상과 4.5% 정도의 충돌 비율 감소를 얻을 수 있다. Grouping 방법은 FAFQ 알고리즘과 AAFQ 알고리즘에 대해선 Ungrouping 방법과 비슷한 성능을 보이지만, Gen2 Q 알고리즘의 경우 Ungrouping 방법과 비교 하였을 때 태그인식시간 및 충돌 비율을 감소시키고, 데이터 처리량 및 시스템 효율을 증가 시킨다.

• Journal of Astronomy and Space Sciences
• /
• 제5권1호
• /
• pp.19-30
• /
• 1988

지구-달계의 질량비인 $\mu$-0.9878449 와 Jacobi 상수 2.9~3.4인 범위의 조건일 때 j종족 충돌궤도가 존재하는가를 조사하였다. 수치적인 방법으로는 Birckhoff의 정칙화 평면에서 Fehlberg(1968)의 5차 Runge-Kutta가변구간 수치적분방법을 사용하여 궤도의 주기성을 검증하였다. 그 결과 4개의 j종족 충돌궤도와 5개의 특이형궤도를 얻었고, 또한, 이 j 종족 충돌궤도가 Pinotsis와 Zikides(1984)가 제시한 주기와 궤도형태의 상관관계를 보였다.

• 한국자동차공학회논문집
• /
• 제6권2호
• /
• pp.178-190
• /
• 1998

We have developed a planar impact model with a capability of reverse calculation to reconstruct various types of automobile collisions. This topic is the main part of what is referred to as accident reconstruction. The model uses the principle of impulse and momentum, and introduces a restitution coefficient and an impulse ratio at the impact center. Based on the car-to-car collision test results, we present how to estimate the restitution coefficient and the impulse ratio from some impact conditions. To validate the model and improve its reliability in accident analysis, the collision analysis has been performer with the estimated parameters. The analysis and experimental results agree well in the kinetic energy loss and the post-impact velocity.

• 한국전산유체공학회:학술대회논문집
• /
• 한국전산유체공학회 2008년도 춘계학술대회논문집
• /
• pp.559-564
• /
• 2008

A prediction of binary droplets collision is important in the formation of falling drops and the evolution of sprays. The droplet velocity, impact parameter and drop-size ratio have influence on the interaction of the droplets. By the effect of these parameter, the collision processes are generated with the complicated phenomena. The droplet collision can be classified into four interactions such as the bouncing, coalescence, reflexive separation and stretching separation. In this study, the two-phase flow of the droplet collision was simulated numerically by using the Level Set method. 2D axi-symmetric simulations on the head-on collisions in the coalescence and reflexive separation, and 3D simulation on the off-center collisions in the coalescence and stretching separation were performed. These numerical results showed good agreements with the experimental and analytical results. For tracking the identity of droplets after the collision, transport equation for the volume fraction of the each initial droplet were used. From this, the identities of droplets were analyzed on the collision of droplets having different size.

• 디지털융복합연구
• /
• 제16권9호
• /
• pp.173-178
• /
• 2018

에어백이 작동되는 중고속 추돌 사고의 경우 에어백 작동 전후의 차량 데이터가 차량의 EDM(Event Driven Memory)에 저장되어 그 추돌 속도를 쉽게 알 수 있다. 하지만 에어백이 작동하지 않는 저속영역에서 추돌하는 경우 그 속도를 산정하기가 어렵다. 또한 저속이라 하더라도 추돌속도에 따라 운전자의 부상 정도가 크게 영향을 받기 때문에 그 속도의 산정이 중요하다. 본 연구에서는 블랙박스에 저장된 영상 이미지를 분석하여 저속영역의 추돌속도를 연산하는 알고리즘을 제안하였다. 전기모터로 와이어로프를 이용하여 차량을 견인하는 방식으로 저속의 후방추돌 상황을 정확하게 재현하면서 다양한 차종과 속도에 대해 실험을 수행하였다. 이 때 블랙박스의 영상 이미지에서 두 차량의 거리가 좁아지는 비율과 전방 차량의 번호판 길이가 증가하는 비율이 동일함을 이용하여 추돌속도를 정밀하게 계산할 수 있다. 즉, 미리 측정된 초기거리와 블랙박스의 영상에서의 번호판의 길이를 초기조건으로 설정하여 본 연구의 계산 알고리즘을 적용하면 저속 추돌 속도를 정확하게 산정할 수 있다. 직선 추돌사고에는 본 연구의 결과가 그대로 적용되지만 각도를 두고 추돌하는 경우에는 별도의 고려가 필요하다.

• 한국해양공학회:학술대회논문집
• /
• 한국해양공학회 2006년 창립20주년기념 정기학술대회 및 국제워크샵
• /
• pp.226-229
• /
• 2006

The safety of on-going ships is one of important concerns in the view of environment and human life. The ship in bad condition is likely to be subjected to accidental loads such as collision. Once she has one or several minor collision damages in the form of circle or ellipse, her ultimate strength under compression or tension load will be reduced. Here, it is important to evaluate the reduction ratio of ultimate strength due to the damage from safety point of view. The problem of strength reduction of a plate with cutout such as opening hole has been treated by many researchers. As a result, a closed-form formula on the reduction of ultimate strength of a plate considering the effect of several forms of cutout was suggested. However, the structure of ships is composed of a plate and a stiffener so-called a stiffened plate, and it is likely to be damaged at a plate and stiffeners together in collision. This paper is to investigate the effect of minor collision damage on ultimate strength of a stiffened plate by using numerical analysis. For this study, the shape of minor collision damage of a stiffened plate was made by using contact algorithm. The deformed shape was used as an initial shape for ultimate stress analysis. Then, a series of nonlinear FE analysis was conducted to investigate the reduction effects of ultimate strength of the stiffened plate. The boundary condition was applied as simply supported at all boundaries, and the tripping of stiffener among failure mode under compression loading was neglected. These results were settled in the form of reduction ratio between ultimate of original intact stiffened plate and that of damaged stiffened plate.

• 상하수도학회지
• /
• 제18권2호
• /
• pp.201-207
• /
• 2004

Dissolved air flotation (DAF) is a solid-liquid separation process that uses fine rising bubbles to remove particles in water. Most of particle-bubble collision occurs in the DAF contact zone. This initial contact considered by the researchers to play a important role for DAF performance. It is hard to make up conceptual model through simple mass balance for estimating collision efficiency in the contact zone because coupled behavior of the solid-liquid-gas phase in DAF system is 90 complicate. In this study, 2-phase(gas-liquid) flow equations for the conservation of mass, momentum and turbulence quantities were solved using an Eulerian-Eulerian approach based on the assumption that very small particle is applied in the DAF system. For the modeling of turbulent 2-phase flow in the reactor, the standard $k-{\varepsilon}$ mode I(liquid phase) and zero-equation(gas phase) were used in CFD code because it is widely accepted and the coefficients for the model are well established. Particle-bubble collision efficiency was calculated using predicted turbulent energy dissipation rate and gas volume fraction. As the result of this study, the authors concluded that bubble size and recycle ratio play important role for flow pattern change in the reactor. Predicted collision efficiency using CFD showed good agreement with measured removal efficiency in the contact zone. Also, simulation results indicated that collision efficiency at 15% recycle ratio is higher than that of 10% and showed increasing tendency of the collision efficiency according to the decrease of the bubble size.

• 한국산학기술학회:학술대회논문집
• /
• 한국산학기술학회 2007년도 추계학술발표논문집
• /
• pp.281-283
• /
• 2007

DCF 프로토콜 상에서 성공적인 패킷 전송을 위해서는 CW 값이 최솟값이 되어야 한다. 성공적인 전송을 위해서는 CW 값이 알맞아야 한다. 이것은 충돌을 유발할 수 있으므로 CW값은 경쟁레벨과 같은 길이가 되어야 한다. Slow CW Decrease(SD)는 경쟁레벨을 유지할 수 있는 방법을 제공한다. 본 논문에서는 Idle and Collision time Ratio(ICR)을 이용한 향상된 SD 방법을 제안한다.