• 제목/요약/키워드: impact angle

검색결과 745건 처리시간 0.042초

CFRP 사교적층판의 충격손상에 관한 연구 (A Study on the Impact-Induced Damage in CFRP Angle-ply Laminates)

  • 배태성;입야영;양동률
    • 대한기계학회논문집
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    • 제17권2호
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    • pp.237-247
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    • 1993
  • 본 연구에서는 CFRP 적층재를 구조재료로 사용할 경우 우수한 인장강도를 갖 지만, 충격하중에 취약한 특성을 갖기 때문에 구조안정성에 관한 큰 문제의 하나로 충 격손상을 받은 적층판의 잔류 압축강도가 현저히 저하되는 것이 문제점으로 지적되어 왔다.특히, 충격손상에 의한 압축강도의 저하는 인장강도보다 압축강도에 중점을 두는 항공기의 강도설계에서 중요한 문제가 되므로, 저속충격에 의한 복합재료 구조체 의 충격파괴의 문제를 잘 이해하는 것이 요구된다. 지금까지의 연구에 의하면 CFRP 복합적층재의 손상은 주로 층간박리현상과 손상역의 크기변화를 실험적으로 고찰하였 다.

충돌 자세각 제한조건을 갖는 종단 유도를 위한 시변 편향 비례항법 (Time-varying biased proportional navigation for terminal guidance with impact attitude angle constraint)

  • 김병수;이보형;이장규;김삼수;조현진
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
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    • pp.355-358
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    • 1996
  • The primary objective of guidance system is to generate suitable commands so that the pursuer comes closer to its target. It is necessary, however, in the guidance of a certain pursuer that the attitude angle at impact should be within a prescribed range in addition to specification on the miss distance. These guidance requirements can not be satisfied by the general guidance laws developed for miss distance minimization. Compared with the demand in many applications, the guidance laws dealing with impact attitude angle constraint are not easily found. In this paper, biased PNG laws are proposed to obtain the guidance purposes. By Lyapunov method, it is shown that the pursuer can intercept the target with a prescribed attitude angle under the assumption that the pursuer is sufficiently fast and the target maneuver is negligible. The simulation results are presented to demonstrate the performance of the suggested guidance laws.

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Real-time midcourse guidance with consideration of the impact condition

  • Song, Eun-Jung;Joh, Mi-Ok
    • International Journal of Aeronautical and Space Sciences
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    • 제4권2호
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    • pp.26-36
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    • 2003
  • The objective of this study is to enhance neural-network guidance to consider the impact condition. The optimal impact condition in this study is defined as an head-on attack. Missile impact-angle error, which is a measure of the degree to which the missile is not steering for a head-on attack, can also have an influence on the final miss distance. Therefore midcourse guidance is used to navigate the missile, reducing the deviation angle from head on, given some constraints on the missile g performance. A coordinate transformation is introduced to simplify the three-dimensional guidance law and, consequently, to reduce training data. Computer simulation results show that the neural-network guidance law with the coordinate transformation reduces impact-angle errors effectively.

The Influence of Impact Angle on Hip Fracture in Fallings

  • Choi, Jae-Bong
    • International Journal of Safety
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    • 제4권1호
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    • pp.1-7
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    • 2005
  • The direction of the applied load and displacement rate on the femur during falls may be an important factors in the etiology of hip fractures. Nonetheless, previous studies did not consider these two factors simultaneously for falling condition. Therefore, in the present study, an impact test system is developed to simulate the falling condition and the influence of impact angle on the deformation pattern changes of proximal femur is investigated. The results showed that a slight variation in impact angle quite affects deformation pattern of the proximal femur. Along with bone mineral density and trabaecular morphology, the impact angle can be another important factor affecting the structural capacity of the proximal femur.

이동표적 타격을 위하여 물리적 구속조건을 고려한 충돌각 제어 복합 유도법칙 (Composite Guidance Law for Impact Angle Control Against Moving Targets Under Physical Constraints)

  • 박봉균;김태훈;김윤환;권혁훈
    • 한국항공우주학회지
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    • 제43권6호
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    • pp.497-506
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    • 2015
  • 본 논문은 기동이 없는 이동표적에 대하여 탐색기의 FOV(field-of-view) 및 기동가속도 제한 내에서 충돌각 제어를 위한 복합 유도법칙을 제안한다. 제안하는 유도법칙은 비례 항법(proportional navigation)의 특성을 이용하는 것으로 총 두 단계의 유도 명령을 생성하게 된다. 첫 번째 유도명령은 초기 유도단계에서 표적에 대한 지향각(look angle)을 일정하게 유지하게 하고, 특정한 시선각 조건을 만족하면 두 번째 비례 항법 유도로 전환하여 원하는 충돌각으로 표적을 타격하게 된다. 충돌각 설정을 용이하게 하기 위하여 제한된 유도탄의 성능 조건을 가지고 달성 가능한 최대 충돌각 계산방법을 제시한다. 수치 시뮬레이션을 통해 설계된 유도법칙의 성능 및 실제 유도탄 환경에 대한 적용가능성을 분석한다.

무인기를 위한 최적 경로점 유도 (Optimal Waypoint Guidance for Unmanned Aerial Vehicles (UAVs))

  • 유창경;신효상;탁민제
    • 제어로봇시스템학회논문지
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    • 제11권3호
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    • pp.240-245
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    • 2005
  • In this paper, planar waypoint guidance synthesis for UAVs using the LQ optimal impact-angle-control guidance law is proposed. We prove that the energy-optimal control problem with the constraint of passing through the waypoints is equivalent to the problem of finding the optimal pass angles on each waypoint of the optimal impact-angle-control law. The optimal pass angles can be obtained as a numerical solution of the simple pass angle optimization problem that requires neither input parameterization nor constraints. The trajectory obtained by applying the optimal impact-angle-control law with these optimal pass angles becomes energy optimal.

액적 충돌에 동반된 열전달에 관한 수치적 연구 (Numerical Study of Heat Transfer Associated with Droplet Impact)

  • 김성일;손기현
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 춘계학술대회
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    • pp.1897-1902
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    • 2004
  • Numerical analysis of the heat transfer associated with droplet impact on a hot solid surface is performed by solving the mass, momentum and energy equations for the liquid-gas region. The deformed droplet shape is tracked by a level set method which is modified to achieve volume conservation during the whole calculation procedure and to include the effect of contact angle at the wall. The numerical method is validated through test calculations for the cases reported in the literature. Based on the numerical results, the effects of advancing/receding contact angle, impact velocity and droplet size on the heat transfer during droplet impact are quantified.

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3차원 공간에서의 비행 경로각을 이용한 비행시간 및 충돌각 제어 유도법칙 (Guidance Law of Missiles for Control Impact-Time-and-Angle by Flight Path Angle in Three Dimensional Space)

  • 김승호;이천기;양빈;황정원;박승엽
    • 한국항행학회논문지
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    • 제16권1호
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    • pp.8-15
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    • 2012
  • 본 논문에서는 표적이 고정되고 유도탄의 속도가 일정하다고 가정하고, 3차원 공간에서 비행 경로각을 이용하여 비행시간과 충돌각을 동시에 제어하는 호밍 유도법칙을 제안한다. 유도탄 비행궤적의 비행 경로각을 독립변수로 하여 비선형 모델을 구성한다. 제안한 호밍 유도법칙이 종말 종속 충돌각과 비행시간 제어가 가능하며, 목표물에 정확히 도달하는 과정을 보여준다. 그리고 동시공격시나리오에도 적용할 수 있다. 시뮬레이션을 통해 제안한 유도법칙의 성능을 확인한다.

런닝화의 경도 차이가 후족 제어 및 충격력에 미치는 영향 분석 (An Effect Analysis of Rearfoot Movement and Impact force by Different Design of Running Shoes Hardness)

  • 이동춘;이우창
    • 한국산업경영시스템학회:학술대회논문집
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    • 한국산업경영시스템학회 2002년도 춘계학술대회
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    • pp.291-296
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    • 2002
  • The midsole hardness of athletic footwear affects capability of absorbing impact shock and controls rearfoot movement during running and walking. The prior studies were focused on examining the proper hardness of footwear for rearfoot movement or to finding effective hardness for absorbing impact shock. The displacements of maximal Achilles tendon angle described a amount of pronation motion is decreased when medial hardness of midsole is large more than lateral. Increasing hardness of footwear midsole are effected to reduce maximum and intial pronation angle, but declined the ability of impact shock during heelstrike. For determination of effectiveness hardness of midsole, therefore, the study that makes a compromise between rearfoot movement and absorbing impact during footstrike must be performed. The purpose of this study is to examine quantitative values of rearfoot control and absorbing impact shock with different hardness of medial and lateral midsole on heel portion. The results are useful to define biomechanical hardness of midsole for developing running shoes. As variable for impact shock, accelerations onto shank and knee are measured during 4 running speeds (5, 7, 9, 11km/h). Also, maximum and $10\%$ pronation angle (Achilles tendon angle) were measured using high-speed camera.

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테니스 양손 백핸드 스트로크 스윙자세의 운동학적 분석 (A Kinematic Analysis of Two Hand Backhand Stroke Swings in Tennis)

  • 강상학;손원일
    • 한국운동역학회지
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    • 제17권1호
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    • pp.41-52
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    • 2007
  • The present study analyzed the two hand backhand stroke motion of six female high school tennis players who won the championship at the National Athletic Meeting in 2006, and drew conclusions as follows. The open angle of the racket at the moment of impact was 90 degree without significant difference among the players, making a wide contact between the ball and the racket. The racket angle was 43 degree at take back and 91 at impact, showing a style of holding the racket rather upright in general. In back swing from the top to the impact, the shoulders and the hips turned by 97 degree and 40 degree, respectively. At the moment of impact, the height of the impact was 54%H, and the position of the impact was 10%H ahead of and 37%H left from the central axis of the body. The right hand made a continental grip and the left hand made a Western or semi Western grip. Through the entire swing motion, the grip angle of the left hand was smaller than that of the right hand, and those who maintained a large grip angle of the right hand at the moment of take back put the racket head slightly farther from the body. In the swing of the racket head from the lowest point to the impact, the vertical length of movement was 11%H and the horizontal length of movement was 60%H, quite long.