• Title/Summary/Keyword: 궤적해석

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나선 주사 영상 궤적을 위한 경사자계 구현의 초기값 결정에 따른 영상 개선

  • 김휴정;김인기;장경섭;이정선;이흥규;안창범
    • Proceedings of the KSMRM Conference
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    • 2002.11a
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    • pp.125-125
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    • 2002
  • 목적: 나선 주사 영상의 경우 영상의 대조도와 질을 결정하는 k-space의 DC영역부터 데이터를 얻기 때문에 경사자계를 구현하는데 있어서 초기값이 중요한 역할을 한다. 또한, 영상의 재구성과정에서 데이터의 complex conjugation 특성을 이용하기 때문에 각 데이터의 대칭성도 중요하다. 본 연구의 목적은 나선주사 영상의 경사자계를 수학적인 방법과 수치 해석적인 방법을 이용하여 구현함으로써 초기 경사자계 인가의 문제점을 보완하여 영상의 질을 개선하는데 있다.

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Elliptical Trajectory Analysis of Ultrasonic Linear Motor (초음파 리니어 모터의 타원궤적 해석)

  • 김태열;김범진;박태곤;김명호
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 2000.07a
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    • pp.411-414
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    • 2000
  • An ultrasonic linear motor was composed of a slider and a stator vibrator including piezoelectric material and elastic material. The ultrasonic linear motors mainly consist of an ultrasonic oscillator which generates elliptical oscillations. Elliptical oscillations are generated by synthesizing two degenerated modes. Direction of vibratory displacement was analyzed by employing the finite element method. So, we could recognize that the direction of the slider's movement was controlled by changing the Phase difference of the drive voltage.

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A Study on the Simulation of Beam Trajectory in the Electron-Gun by FDM using the Irregular Mesh (불균등 Mesh를 사용한 유한차분법에 의한 전자총의 Beam 궤적 Simulation에 관한 연구)

  • 김남호;정현열;이무용;정기호
    • The Journal of Korean Institute of Communications and Information Sciences
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    • v.16 no.8
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    • pp.719-731
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    • 1991
  • This paper introduces a relatively simple computer simulation method for analyzing trajectory of electron beam in cylindrical electrode of the CRT, which outputs the cutoff voltag, beam current, spot size and plots out the trajectory, rom the input data on physical construction and applied voltages of electron gun. In order to improve computing speed in obtaining potential distibution, the authors have ivided the space into seveal setos and allocated different mesh sizes epending on the acuracy required to each sector and applied the finite difference method in calculation. The plot of trajectoy obtained from the simulation provided useful insight into the focusing mechanism of the CRT. The computed and measured result including beam curent. spot sizs and cutoff voltages for several model guns have ageed within eperimental error. The simulation program enables the designer to compare the effects of varied electrode shpe without the epense of building an actual gun and may be appli in esigning and implementing the electron gun assemply.

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Sliding-Mode Control of Container Cranes (컨테이너크레인 시스템의 슬라이딩모드제어)

  • Lee Suk-Jae;Park Hahn;Hong Keum-Shik
    • Journal of Navigation and Port Research
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    • v.29 no.8 s.104
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    • pp.747-753
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    • 2005
  • In this paper, as an anti-sway control strategy of container cranes, we investigate a variable structure control in which the moving load follows a given trajectory, whereas both the trolley and hoist controllers achieve their positioning problems. It is crucial, in an automated container terminal, that collisions should be avoided during the transference of containers from one place to another. It is also necessary, in the case of a quay crane, to select suitable loading and unloading trajectories of containers, so that possible collisions with surrounding obstacles are avoided. After a brief introduction of the mathematical model, a robust control scheme (i.e., a second-order sliding mode control that guarantees a fast and precise transference and a suppression of the resulted swing) is presented. Despite model uncertainties and unmodeled actuators dynamics, the swing suppression from the given trajectory is obtained by constraining the system motion on suitable sliding surfaces, which include both the desired path and the swing angle. The proposed controller has been tested with a laboratory-size pilot crane. Experimental results are provided.

Mission-based Operational Orbit Design for Sun-synchronous Spacecraft (임무기반 태양동기궤도 운영궤도 설계에 관한 연구)

  • Lee, Ji-Marn;No, Tae-Soo;Jung, Ok-Chul;Chung, Dae-Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.9
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    • pp.752-759
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    • 2012
  • This paper presents a mission orbit design method for spacecraft which use the sun-synchronous and ground repeat orbits. In this work, we have proposed a new design procedure, "Nonlinear simulation-based numerical optimization technique" using the commercial S/W's such as STK (Satellite Tool kit) and Matlab, which are widely adopted S/W's in the area of orbital mechanics and engineering analysis. Inclusion of all the perturbation effects on the spacecraft not only can more precisely satisfy the mission requirements for sun-synchronicity and repeated ground track, and also operational requirements such as minimum change in the S/C local time, maximization of the contact time with a specified ground station, etc. can be appropriately considered. Design examples for LEO sun-synchronous mission are presented to demonstrate the usefulness of the proposed method in this paper.

Analysis of the Flight Trajectory Characteristics of North Korea SLBM (북한 SLBM의 비행특성 해석)

  • Lee, Kyoung-Haing;Seo, Hyeong-Pil;Kwon, Yong-Soo;Kim, Jiwon
    • Journal of the Korea Society for Simulation
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    • v.24 no.3
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    • pp.9-16
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    • 2015
  • This research focuses on analysis of the flight trajectory characteristics of SLBM (Submarine Launched Ballistic Missile) of North Korea. Recently, North Korea tested launching of SLBM which is threatening international security. Also it is known that North Korea had possessed the technologies about SLBM since they disassembled submarines out of commission of the former Soviet Union. If the development of the SLBM of North Korea is completed, it should be affected as asymmetric threat to South Korea. Therefore, for active respondence to these threat, it is essential to analyze the SLBM systematically. In this point of view, this work made a SLBM flight model and simulated. In addition, we controled flight trajectories according to adjusting loft angle and described their characteristics. The sea-based ballistic missile defense system is required for an effective response to the flight trajectory of the SLBM from mid-course to terminal phase.

Frequency modulation spectroscopy of a super-cavity using a single mode He-Ne laser (단일모드 헬륨네온레이저를 사용한 초공진기의 주파수 변조 분광연구)

  • 서호성;윤태현;조재흥;정명세;류갑열;김영덕;최옥식
    • Korean Journal of Optics and Photonics
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    • v.3 no.1
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    • pp.27-36
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    • 1992
  • Frequency modulation spectroscopy of the super-cavity, of which finesse is app. 40,000 has been demonstrated by using a sigle mode He-Ne laser. In-phase and quardrature components of frequency modulation signals (FM signal) were obtained by using the 1.5 MHz-driven-electrooptic phase modulator. The vector locus of the FM signa in the phase space, which is consisted of in-phase and quardrature components of the FM signal, was observed and analyzed for the dependence of FM signal upon the phase of the reference signal of a phase-sensitive-detector. According to rotating the phase of the reference signal, the vector locus was observed to rotate with the same phase angle as the reference signal. The in-phase component of the FM signals will be used to stabilize the frequency of the He-Ne laser to the resonant frequency of the super-cavity.

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Development of Optimization Code of Type 3 Composite Pressure Vessels Using Semi-geodesic algorithm (준측지궤적 알고리즘을 이용한 타입 3 복합재 압력용기의 최적설계 프로그램 개발)

  • Kang, Sang-Guk;Kim, Myung-Gon;Kim, Cheol-Ung;Kim, Chun-Gon
    • Composites Research
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    • v.21 no.1
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    • pp.1-7
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    • 2008
  • Composite vessels for high pressure gas storage are commonly used these days because of their competitive weight reduction ability maintaining strong mechanical properties. To supplement permeability of composite under high pressure, it is usually lined by metal, which is called a Type 3 vessel. However, it has many difficulties to design the Type 3 vessel because of its complex geometry, fabrication process variables, etc. In this study, therefore, GUI (graphic user interface) optimal design code for Type 3 vessels was developed based on semi-geodesic algorithm in which various factors of geometry and fabrication variables are considered and genetic algorithm for optimization. In addition, hydrogen vessels for 350/700 bar that can be applied to FCVs(fuel cell vehicles) were designed using this code for verification.

Lagrangian Simulation Model of Heavy Particle Motion in a Turbulent Flow (라그랑지 관점에 입각한 난류유동장 내의 관성입자운동 모사 모델)

  • Moon, Sun;Maeng, Joo-Sung
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.15 no.1
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    • pp.241-251
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    • 1991
  • The present simulation model relies on a new approach of the heavy particle motion in a turbulent flow considering the time and space correlation to the Lagrangian point of view. The turbulent field is, here, assumed that its characteristic scales are random and follow a Poisson's distribution. Using this model, we have computed the trajectory of each particle, that is, its velocity and position at each time in order to study the dispersion of particles in a grid turbulent flow. The computed results have been compared to the corresponding experimental data. Due to the complex mechanism of turbulence and the theoretically and experimentally lacking information, we had to make some assumptions for simplifying the situation, but we have found the good agreement between simulated and measured results. In particular, the application of the present method on the Lagrangian correlation of particle provides an interesting alternative to the usual computational methods.

Analysis of Machined Surfaces by Ball-end Milling using the Ridge Method (능선 궤적법을 이용한 볼엔드밀 가공면 해석)

  • 정태성;남성호;박진호;양민양
    • Journal of the Korean Society for Precision Engineering
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    • v.21 no.1
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    • pp.51-60
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    • 2004
  • Ball-end milling is one of the most common manufacturing processes for the parts with sculptured surface. However, the conventional roughness model is not suitable for the evaluation of surface texture and roughness under highly efficient machining conditions. Therefore, a different approach is needed for the accurate evaluation of machined surface. In this study, a new method, named ‘Ridge method’, is proposed for the effective prediction of the geometrical roughness and the surface topology in ball-end milling. Theoretical analysis of a machined surface texture was performed considering the actual trochoidal trajectories of cutting edge. The characteristic lines of cut remainder are defined as three-types of ‘Ridges’ and their mathematical equations are derived from the surface generation mechanism of ball-end milling process. The predicted results are compared with the results of conventional method. The agreement between the results predicted by the proposed method and the values calculated by the simulation method shows that the analytic equations presented in this paper are useful for evaluating a geometrical surface roughness of ball -end milling process.