• 제목/요약/키워드: Impact Path

Search Result 618, Processing Time 0.023 seconds

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

  • Kim, Hyun-Seung;Park, Sang-Sup;Ryoo, Chang-Kyung
    • Journal of the Korean Society for Aeronautical & Space Sciences
    • /
    • v.43 no.8
    • /
    • pp.669-676
    • /
    • 2015
  • In this paper, a guidance law for intercepting maneuvering target with a desired impact angle is proposed. The proposed guidance law is modified from the optimal impact angle control law for a fixed target and given by a biased PN law with the impact angle control term in addition to the conventional PN law. Three different kinds of desired impact angles in the respect of LOS angle, flight path angle, and relative flight path angle to the target are defined. The performance of the proposed guidance law is investigated via numerical simulations for various air-to-air engagement scenarios.

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

  • Jin, Sheng-Hao;Lee, Chun-Gi;Yang, Bin;Hwan, Chung-Won;Park, Seung-Yub
    • Journal of Advanced Navigation Technology
    • /
    • v.16 no.1
    • /
    • pp.8-15
    • /
    • 2012
  • This paper on the assumption that the target is stationary and the velocity of missile is fixed value. In three dimensional space. Using flight path angle to simultaneous control impact-time-and-angle base on a homing guidance law. The independent variable in the nonlinear engagement model is the flight path angle of the missile. The propose homing guidance law can see the controllability of impact-time-and-angle. And also can see the processing of the missile arrive at the target. It is applied to several salvo attack scenarios. The performance of the proposed guidance law is verified by simulations.

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

  • 마호성
    • Journal of the Computational Structural Engineering Institute of Korea
    • /
    • v.17 no.1
    • /
    • pp.83-91
    • /
    • 2004
  • Nonlinear system responses of an impact system under randomly perturbed harmonic excitations are predicted in the probability domain by adopting the semi-analytical procedure previously developed. The semi-analytical procedure is obtained by solving the Fokker-Planck equation corresponding to the stochastic differential equation of the given impact system by utilizing the path-integral solution. The evolutionary joint probability density functions are generated by using the method, and the characteristics of nonlinear dynamic response behaviors of the system are examined. Noise effects on the responses are also examined. It Is found that the semi-analytical method can provides the accurate information of the responses via the joint probability functions for the impact system. It is found that the noises weaken and eventually terminate the chaos in the responses, but it is also found that the chaotic signatures reside in the presence of the external noise with relatively high intensity. The joint probability density function shows that the ensemble of the system responses are weakly stationary.

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

  • Hong, Sung Ju;Yang, Hae Jeong
    • Journal of Drive and Control
    • /
    • v.16 no.2
    • /
    • pp.1-7
    • /
    • 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.

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

  • Myeong, Gwang Hyeun;Jeong, Jong Chul
    • Journal of Environmental Impact Assessment
    • /
    • v.20 no.4
    • /
    • pp.489-496
    • /
    • 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.

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

  • Choi, Young-Jin;Lee, Young-Shin;Han, Kyoo-Hyun;Chae, Je-Uk;Choi, Eui-Jung
    • Proceedings of the KSME Conference
    • /
    • 2004.11a
    • /
    • pp.459-464
    • /
    • 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.

  • PDF

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

  • Park, Jong Soon;Lee, Jong Man
    • Journal of Korea Society of Digital Industry and Information Management
    • /
    • v.10 no.2
    • /
    • pp.213-227
    • /
    • 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.

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

  • Lee, Jin-Young;Lee, Chan;Kil, Hyun-Gwon
    • Journal of Environmental Impact Assessment
    • /
    • v.18 no.3
    • /
    • pp.143-150
    • /
    • 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.

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

  • Jin, Sheng-Hao;Yang, Bin;Hwang, Chung-Won;Park, Seung-Yub;Park, Seung-Je
    • Journal of Advanced Navigation Technology
    • /
    • v.14 no.5
    • /
    • pp.596-603
    • /
    • 2010
  • This paper presents a homing guidance law of anti-ship missiles using flight path angle to achieve an impact time constraint as well as an impact angle constraint. the independent variable in the nonlinear engagement model is change d from the flight time to the heading angle of the missile. The proposed guidance law can home a missile to the target with zero miss distance as well as satisfying both of the impact angle and time constraints. The performance of the proposed guidance law is evaluated by the computer simulations.