• 제목/요약/키워드: Impact Path

검색결과 618건 처리시간 0.024초

기동표적에 대한 입사각 정의와 입사각 제어 유도법칙 (Definition of Impact Angle and Impact Angle Control Law Against Maneuvering Target)

  • 김현승;박상섭;유창경
    • 한국항공우주학회지
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    • 제43권8호
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    • pp.669-676
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    • 2015
  • 본 논문에서는 기동하는 표적에 대한 입사각 제어 유도법칙을 제안하였다. 제안된 유도법칙은 정지표적에 대한 최적입사각제어 유도법칙을 변형한 것으로서 기존의 PN(Proportional Navigation) 유도법칙에 입사각제어 항이 추가된 바이어스 PN 유도법칙의 형태를 갖는다. 시선각, 비행경로각, 그리고 표적에 대한 상대 비행경로각 관점에서의 세 가지 다른 종류의 입사각을 정의하였다. 다양한 공대공 교전 시나리오에 대한 수치 시뮬레이션을 통해 제안한 유도법칙의 성능을 검증하였다.

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.

Path-Integral Solution을 이용한 랜덤동요된 조화가진력을 받는 임팩트시스템의 거동분석 (Dynamic Behaviors of an Impact System under Randomly Perturbed Harmonic Excitation by the Path-Integral Solution Procedure)

  • 마호성
    • 한국전산구조공학회논문집
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    • 제17권1호
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    • pp.83-91
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    • 2004
  • 랜덤동요된 조화가진력을 받는 임팩트시스템의 비선형거동을 개발된 반해석적절차에 의해 확률영역에서 분석하였다. 반해석적절차는 path-integral solution을 이용하여 임팩트시스템의 추계론적 미분방정식으로부터 구함으로 얻어진다. 결합확률밀도함수의 전개를 구하고 시스템의 비선형거동 특성인 혼돈거동에 대하여 분석하고 노이즈의 영향을 시간영역과 확률영역에서 알아보았다. 결과로부터 반해석적절차는 결합확률밀도함수를 통하여 임팩트시스템의 거동에 대한 정보를 제공하는 것을 알 수 있었다. 노이즈의 영향은 혼돈거동의 특성을 약화시키며 궁극적으로 사라지게 함을 알 수 있었으며 또한 혼돈거동의 특성이 상대적으로 높은 노이즈아래에서도 남아있는 것을 밝혔다. 결합확률밀도함수는 응답앙상블이 약정상과정임을 확인시켜 주었다.

쇄석기의 충격하중 정량화에 대한 연구 (A Study on the Impact Load Quantification of the Jaw Crusher)

  • 홍성주;양해정
    • 드라이브 ㆍ 컨트롤
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    • 제16권2호
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    • pp.1-7
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    • 2019
  • Jaw crusher is a device that breaks rock collected from mines or quarries to produce aggregates of the size desired by user. A representative method for measuring load is to measure them by attaching force sensors directly to the part where the load is generated. However, the direct method has many limitations such as high-impact loads generation in equipment or space constraints, sensor capacities and costs. Therefore, Transfer Path Analysis (TPA) was used to indirectly measure impact loads by attaching acceleration sensors. In this study, both direct and TPA methods were used to measure the impact load of Jaw crusher. This study finally quantifies the impact of the load generated by the Jaw crusher using direct method and TPA method, and comparing the impact load measured calculated the derive the error rate.

GIS에 의한 댐 유역 수질오염사고 평가 (The Assessment of Water Pollution Accident on Dam Watershed using GIS)

  • 명광현;정종철
    • 환경영향평가
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    • 제20권4호
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    • pp.489-496
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    • 2011
  • The water pollution such as oil spill from stream and river because of car accidents have been frequent cases in the watershed of Dam. However we don't have any simulation methods about flow modeling on the watershed and stream tree. In this study aims to analyze water pollution accidents area on impact range for ANDONG-Dam. The focused watershed and the risk range of path analysis model was designed by GIS database. The frequency of transportation accidents which may occur from road accidents in the level of quantitative and qualitative analysis to map flow analysis using ArcHydro Model and Open Geospatial Consortium(OGC) API. and the path way from the accident point to the reservoir stayed on the path was simulated. The area of risk accessment index was displayed with cell and grid of dam area.

주요 사격자세에 따른 인체 충격량 특성 해석 (A study on the human impulse characteristics with the typical shooting posture)

  • 최영진;이영신;한규현;채제욱;최의중
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2004년도 추계학술대회
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    • pp.459-464
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    • 2004
  • The rifle impact of human body affected by the posture of human for rifling. The interaction human-rifle system influence the firing accuracy. In this paper, impact analysis of human model for shooting posture is carried out. ADAMS code and LifeMOD is used in impact analysis of human model and modeling of the human body, respectively. On the shooting, human model is affected by rifle impact during the 0.001 second. Performed simulation time for shooting is 0.1 second. Applied constraint condition to human-rifle system is rotating and spherical condition. As the results, the displacement of rifle and transfer path analysis of impact of human model is presented.

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대학생들의 셀프리더십, 진로결정자기효능감이 진로준비행동에 미치는 영향 (A Study on the affect of Self-leadership, Self-efficacy of Career Path Decision on the University Students' Career Path Preparation Behavior)

  • 박종순;이종만
    • 디지털산업정보학회논문지
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    • 제10권2호
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    • pp.213-227
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    • 2014
  • The Purpose of this research was to examine the influence of university students' self-leadership and career decision self-efficacy upon career preparation behavior. A total of 342 participants in 1th ~ 3th grades from universities in Seoul. Result from multiple regression analysis indicated the following. First, self-leadership and career decision self-efficacy had an impact on career preparation behavior. Second self-leadership had impact an career decision self-efficacy. Third, career decision self-efficacy had an impact on career preparation behavior. The result showed that there was significant interaction. Finally, the limitations of this study and suggestions for future research on career path preparation behavior were discussed. The implication of this study is that self-leadership and self-efficacy can the university students' career path preparation behavior. This research findings, theoretical and practical implications were suggested. Consequently it mean that the career guide program for university student. Therefore, effective counseling strategies to enhance career preparation behavior.

군용항공기의 운항 경로 변경에 따른 소음영향 및 저감 평가 (Evaluation on the Noise Influence and Reduction due to the Change of Military Aircraft Flight Path)

  • 이진영;이찬;길현권
    • 환경영향평가
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    • 제18권3호
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    • pp.143-150
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    • 2009
  • The present study investigates the effects of the flight paths of military aircraft on noise map and its WECPNL(Weighted Equivalent Continuous Perceived Noise Level) distribution. Aircraft noise modeling and simulation have been performed on a Korean military air base by means of INM(Integrated Noise Model) with the input data of airfield location, aircraft specifications, flight paths and aircraft's operation schedules. The result of noise modelling has been verified in comparison with the result of measured noise level. The flight path of military aircraft, as the key parameter of the present study, was modeled by combining takeoff, overfly, approach and touch-and-go modes. The present INM simulations have been conducted for various flight path cases with different takeoff, approach modes and overfly modes. The simulation results showed that the change of flight path can remarkably affect the noise influence region and the WECPNL distribution around the airfield.

비행 경로각을 이용한 대함 유도탄의 호밍 유도법칙 (Homing Guidance Law of Anti-Ship Missiles Using Flight Path Angle)

  • 김승호;양빈;황정원;박승엽;박승제
    • 한국항행학회논문지
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    • 제14권5호
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    • pp.596-603
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    • 2010
  • 본 논문에서는 비행 경로각을 이용하여 비행시간과 충돌각을 동시에 제어하는 호밍 유도법칙을 제안한다. 독립변수를 기존의 비행시간에서 유도탄 비행궤적의 비행 경로각으로 바꿔 비선형 모델을 구성한다. 제안한 호밍 유도법칙이 종말 종속 충돌각과 비행시간 제어가 가능하며, 목표물에 정확히 도달하는 것을 보여준다. 시뮬레이션을 통해 제안한 유도법칙의 성능을 확인한다.