• 제목/요약/키워드: Phase Trajectory

검색결과 265건 처리시간 0.027초

2차원 진동 미세가공을 위한 가진테이블 개발 (Development of Excitation Table for 2-dimensional Vibrational Micro Cutting)

  • 김기대;이강희
    • 한국기계가공학회지
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    • 제11권3호
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    • pp.62-67
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    • 2012
  • To realize 2-dimensional vibrational micro cutting in milling and drilling, etc. where the tools rotate, it could be a promising way to vibrate a workpiece instead of a rotating tool itself. In this study, an excitation work-table was developed using two piezoelectric materials orthogonally arranged. The trochoidal trajectory of a cutting tool which is necessary for 2D vibrational cutting is enabled in the excitation condition of higher excitation frequency and larger amplitude of vibration and the cutting condition of smaller diameter of cutting tool and lower spindle speed. The various trochoidal trajectories of a cutting tool could be generated in the excitation work-table by adjusting the input voltages to two piezoelectric materials and the phase between the two voltages and the trajectories could be readily used for the 2D vibrational micro cutting.

ANSYS를 이용한 초음파 리니어 모터의 타원궤적 해석 (Elliptical Trajectory Analysis of Ultrasonic Linear Motor using ANSYS)

  • 최명일;박태곤;김명호
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2002년도 추계학술대회 논문집 Vol.15
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    • pp.292-295
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    • 2002
  • Transducer for linear ultrasonic motor with symmetric and anti-symmetric modes was studied. The transducer was composed of two Langevin-type vibrators that cross at right angles with each other at tip. In order to excite two vibration modes, two Langevin-type vibrators must have 90-degree phase difference with each other. As a result, tip of transducers moves in elliptical motion. In this paper, elliptical trajectory of transducer was analyzed by employing the finite element method.

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DNP 제어기에 의한 비선형 동적 매니퓰레이터의 실시간 경로 제어 (Real-Time Collision-Free Trajectory Control of Nonlinear Dynamic Manipulator Control Using DNP Controller)

  • 조현섭
    • 한국산학기술학회논문지
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    • 제11권3호
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    • pp.835-840
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    • 2010
  • 본 논문은 가변 구조 제어기의 단점인 도달영역에서의 파리미터의 불확실성과 외부 외란에 대한 민감성을 감소시키는 방안으로 DNP제어를 제시한다. 비선형 동적 매니퓰레이터를 통하여 시스템의 상태 궤적이 초기 위치에서부터 평형점에 이르기까지 외란과 파라미터의 불확실성에 강인하게 되며 아울러 목표 직각 좌표까지 도달시간 뿐만 아니라 평형점까지의 도달시간도 감소하게 되는 특성을 보이고자 한다. 제안된 제어 구조의 효과는 시뮬레이션을 통해 증명하였다.

Effects of Customized 3D-printed Insoles on the Kinematics of Flat-footed Walking and Running

  • Joo, Ji-Yong;Kim, Young-Kwan
    • 한국운동역학회지
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    • 제28권4호
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    • pp.237-244
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    • 2018
  • Objective: Flat-footed people struggle with excessive ankle joint motion during walking and running. This study aimed to investigate the effects of customized three-dimensional 3D-printed insoles on the kinematics of flat-footed people during daily activities (walking and running). Method: Fifteen subjects (height, $169.20{\pm}2.61cm$; age, $22.87{\pm}8.48years$; navicular bone height, $13.2{\pm}1.00mm$) diagnosed with flat feet in a physical examination participated in this study. Results: The customized 3D-printed insoles did not significantly affect 3D ankle joint angles under walking and running conditions. However, they shifted the trajectory of the center of pressure (COP) laterally during fast walking, which enhanced the load distribution on the foot during the stance phase. Conclusion: The customized 3D-printed insoles somewhat positively affected the pressure distribution of flat-footed people by changing the COP trajectory. Further research including comparisons with customized commercial insoles is needed.

중개궤도를 이용한 지구-달 천이궤적의 설계 및 분석 (The Earth-Moon Transfer Trajectory Design and Analysis using Intermediate Loop Orbits)

  • 송영주;우진;박상영;최규홍;심은섭
    • Journal of Astronomy and Space Sciences
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    • 제26권2호
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    • pp.171-186
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    • 2009
  • 이 연구에서는 미래 한국의 달 탐사에 대비, 지구-달 천이궤적을 설계하고 분석하였다. 궤적 설계는 최소연료로 지구 주차궤도에서부터 달 임무궤도까지 도달하는 모든 단계에 대해서 실시하였으며 미래 한국의 달 탐사 개발 계획에 실질적인 도움이 되기 위해 2017년, 2020년, 2022년으로 각각 나누어 설계를 하였다. 탐사선의 운동방정식의 구현을 위하여 태양, 지구, 달의 중력에 의한 섭동력이 포함된 N체 운동 방정식을 사용하였으며 보다 실질적인 우주환경의 모사를 위하여 지구의 비대칭 중력장(Geopotential), 태양 복사압(Solar radiation pressure) 그리고 달의 J2 섭동에 의한 영향도 고려하였다. 임무 설계를 위해 가정된 추력은 순간 추력(Impulsive thrust)으로 가정하였으며 발사체의 성능은 현재 개발 예정인 KSLV-2로 가정하였다. 미래 한국의 가상 달 탐사선이 지구-달 천이 궤적(Trans Lunar trajectory)에 진입하는 방법으로는 지구 주차 궤도에서 직접 진입 하는 방법과 여러번의 타원 중개 궤도를 거친 후 지구-달 천이 궤적으로 진입하는 방법을 모두 이용하였다. 아울러 TLI(Trans Lunar Injection) 기동시 탐사선의 대전 지상국에서의 가시성에 따른 기동의 크기에 대한 영향이 분석되었다. 이 연구를 통한 임무 설계 결과는 달 탐사 임무 설계를 위한 발사 가능 시기(launch opportunity), 성공적인 임무 수행을 위한 임무 단계별 최적의 기동량 및 해당 궤도의 특성 그리고 다양한 임무 파라미터등의 해석을 포함하고 있다. 임무 설계 결과, 미래 한국이 쏘아 올릴 수 있는 달 탐사선의 전체 질량은 해당 임무의 수행시기 보다는 초기 지구 출발 궤도의 초기 고도와 발사제의 초기 궤도 투입 성능에 따라 더욱 크게 좌우됨을 확인하였다.

횡단 유동장의 기액비 및 레이놀즈수 변화에 따른 외부혼합형 이상유체 제트의 액적크기 및 체적유속 특성 (Characteristics of SMD and Volume Flux of Two-phase Jet Injected into Cross-flow with Various Gas-liquid Ratio and Reynolds Number)

  • 김종현;이봉수;구자예
    • 한국자동차공학회논문집
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    • 제17권2호
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    • pp.75-81
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    • 2009
  • A study was performed to investigate the characteristics of two-phase jet injected into subsonic cross-flow using the external mixed gas blast two-phase nozzle. The shadowgraph method was adopted for the cross-flow jet visualization and PDPA system was used to measure droplet size, velocity, and volume flux. The atomization of two-phase jet is initially determined according to gas to liquid mass flow-rate ratio and the Reynolds number of cross-flows. The highest penetration trajectories of two-phase jet injected into cross-flow are governed by the momentum ratio at subsonic cross-flow. As GLR of two-phase jet injected into cross-flow increases, the droplet size decreases and the distribution area of volume flux increases. The distribution of volume flux that influenced by the counter vortex pair at the downstream of cross-flow is symmetric in shape of horseshoe.

비행단계 식별 알고리즘을 이용한 초고속 표적의 탄착점 예측 (Impact Point Prediction of the Ballistic Target Using a Flight Phase Discrimination)

  • 정재경;황동환
    • 한국군사과학기술학회지
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    • 제18권3호
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    • pp.234-243
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    • 2015
  • It is required to have the capability to predict the impact point of the ballistic target in order to assign the firing unit with high engagement possibility for the interception in the ballistic target defense systems. In this paper, a novel method is proposed to predict the impact point of the ballistic target using a flight phase discrimination algorithm given the insufficient measurements on the partial trajectory. The flight of a ballistic target is composed of a boost phase and a ballistic phase with different dynamics. The flight phase is discriminated by using the normalized innovation distance between measurements and a priori estimated measurements. The threshold and tolerance in the flight phase discrimination are determined from the probabilistic characteristics of the estimation error. Monte Carlo simulations are performed to verify the proposed method.

X-대역 400 W 펄스신호를 위한 위상변환기 설계 및 제작 (Design and Manufacture of Phase Shifter for 400 W Pulse Signal in X-Band)

  • 박인용;민승현
    • 한국항공우주학회지
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    • 제46권3호
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    • pp.251-256
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    • 2018
  • 고속 비행체의 궤적 추적을 위하여 사용하는 레이다 중계기의 경우, 짧은 폭의 펄스를 방사한다. 이러한 신호의 위상 변위를 위하여 branch type 위상 변위기가 사용 된다. 이 변위기는 branch 전송선 끝의 가변 리액턴스를 이용하여 전송선 상의 위상을 변화 시킨다. 또한 고출력 신호의 제어가 용이하고, 리액턴스의 고장 시에도 삽입 손실이 크지 않은 장점이 있다. 이 논문에서는 $0^{\circ}$, $30^{\circ}$, $60^{\circ}$, $90^{\circ}$로 순차적으로 위상을 변위 시키는 400 W급 위상 변환기를 제작 시험 결과를 논한다.

단일 카메라의 영상분리를 이용한 자유 상승 기포의 고속 이상 유동 PIV 계측 (Time-Resolved Two-Phase PIV Measurements of Freely Rising Bubble Flows with an Image Separation Method)

  • 성재용;박상민;유정열
    • 한국가시화정보학회지
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    • 제2권1호
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    • pp.39-45
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    • 2004
  • A time-resolved two-phase PIV system using a single camera has been developed, which introduces a method of image separation into respective phase images, and is applied to freely rising single bubble. Gas bubble, tracer particle and background have different gray intensity ranges on the same image frame when reflection and dispersion in the phase interface are intrinsically eliminated by optical filters and fluorescent particles. Further, the signals of the two phases do not interfere with each other. Gas phase velocities are obtained from the separated bubble image by applying the two-frame PTV. On the other hand, liquid phase velocities are obtained from the tracer particle image by applying the cross-correlation algorithm. As a result, the bubble rises rectilinearly just after it is released from an injector and then has a zigzag motion in the far field. From the trajectory of the bubble, it is found that the period of the zigzag motion is closely related to the vortex shedding although the wavelength of it varies along its movement.

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불확실 일반 선형 시스템의 레귤레이션 제어를 위한 사전 제어 성능을 갖는 개선된 연속 적분 가변구조 시스템 (An Improved Continuous Integral Variable Structure Systems with Prescribed Control Performance for Regulation Controls of Uncertain General Linear Systems)

  • 이정훈
    • 전기학회논문지
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    • 제66권12호
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    • pp.1759-1771
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    • 2017
  • In this paper, an improved continuous integral variable structure systems(ICIVSS) with the prescribed control performance is designed for simple regulation controls of uncertain general linear systems. An integral sliding surface with an integral state having a special initial condition is adopted for removing the reaching phase and predetermining the ideal sliding trajectory from a given initial state to the origin in the state space. The ideal sliding dynamics of the integral sliding surface is analytically obtained and the solution of the ideal sliding dynamics can predetermine the ideal sliding trajectory(integral sliding surface) from the given initial state to the origin. Provided that the value of the integral sliding surface is bounded by certain value by means of the continuous input, the norm of the state error to the ideal sliding trajectory is analyzed and obtained in Theorem 1. A corresponding discontinuous control input with the exponential stability is proposed to generate the perfect sliding mode on the every point of the pre-selected sliding surface. For practical applications, the discontinuity of the VSS control input is approximated to be continuous based on the proposed modified fixed boundary layer method. The bounded stability by the continuous input is investigated in Theorem 3. With combining the results of Theorem 1 and Theorem 3, as the prescribed control performance, the pre specification on the error to the ideal sliding trajectory is possible by means of the boundary layer continuous input with the integral sliding surface. The suggested algorithm with the continuous input can provide the effective method to increase the control accuracy within the boundary layer by means of the increase of the $G_1$ gain. Through an illustrative design example and simulation study, the usefulness of the main results is verified.