• 제목/요약/키워드: Relative motion

검색결과 789건 처리시간 0.028초

용량성 전극의 동잡음 측정 장치 연구 (A Study on Measurement of Capacitive Electrode Motion Artifact)

  • 임용규
    • 대한의용생체공학회:의공학회지
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    • 제38권3호
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    • pp.137-141
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    • 2017
  • The indirect-contact bio-electric measurements using capacitive electrodes show large motion artifacts in comparison with conventional direct-contact measurements. It is necessary to measure the motion artifacts quantitatively, for the researches of reducing the motion artifacts. In this study, a device for quantitative measurement of motion artifacts was built. Using the device, an electrode was rubbed against some cloth(cotton) and the voltage variation of the electrode was measured as motion artifact in several environmental conditions(temperature and relative humidity). The measured waveforms agreed with that expected by the triboelectricity and the prior observations of the motion artifacts. Therefore, the results demonstrated the usability of the measurement system built in this study. The measurement system will be a great contribution to future research for reducing motion artifact.

KSUPRAMAX-O 선형의 규칙파 중 상대파고 계측에 대한 연구 (A Study on Relative Wave Elevation Measurement of KSUPRAMAX-O in Regular Waves)

  • 박동민;권용주;김건우;남현승;황승현
    • 대한조선학회논문집
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    • 제60권5호
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    • pp.305-319
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    • 2023
  • This study focuses on measuring the relative wave elevation around the KSUPRAMAX-O ship and comparing it with numerical analysis results (potential and computational fluid dynamics). The relative wave elevation is a good indicator of the pressure distribution on the ship's surface, which is affected by the ship's motion, incident waves, and distributed waves. Prior to measuring the relative wave elevation, a comparative test was conducted on resistance type, capacitance type, and ultrasonic type wave probe to measure the relative wave elevation, and it was confirmed that the resistance type wave probe was suitable for measuring the relative wave elevation. A model test was performed at low speed and design speed using resistance type wave probe and compared with the results of numerical analysis result. As for the motion response, it was confirmed that the result of experiments and the result of the numerical analysis were in good agreement. The relative wave elevation showed a similar trend between the experiment and the computational fluid dynamics, but the potential analysis result showed a difference from the experiment in design speed.

2개의 자유도를 가진 병렬 매니퓰레이터의 기구학 해석 (Kinematics Analysis of a 2-DOF Parallel Manipulator)

  • 이종규;이상룡;이춘영;양승한
    • 한국정밀공학회지
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    • 제29권1호
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    • pp.64-71
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    • 2012
  • In this paper, a parallel manipulator is comprised of two sliders and four links. Sliders execute a linear reciprocating motion depending on parallel guides and make the connected links rotate. A couple of links connected by sliders do coupling motion. The end-effector called a link tip has orientation angle. Through the kinematics analysis of this manipulator, we found displacement, velocity and acceleration using direct and inverse kinematics. We used equations that derived from this analysis and determined five constraint conditions. These conditions had much to do with rotation states of links, the relative relation of link length and coupling motion state. To verify those, we suggest a new algorithm regarding constraint conditions of a manipulator. With the result which performed the algorithm, we found out that operation range of coupled links was limited by relative relation of link length and that manipulator was not able to carry out a series of link motion, in case of being the link vertical between two parallel guides.

비정렬 중첩격자기법을 이용한 유도무기의 기체분리운동 모사 (Numerical Simulation of Airframe Separation of a Missile System Using an Unstructured Overset Mesh Technique)

  • 정문승;이상욱;권오준;허기훈;변우식
    • 한국항공우주학회지
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    • 제34권5호
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    • pp.19-29
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    • 2006
  • 본 연구에서는 비행중인 유도무기의 기체분리에 대한 수치적 해석을 수행하였다. 기체의 정확한 분리운동을 모사하기 위해 삼차원 공간에서 각각의 물체가 연결되어 움직이는 6자유도 운동방정식을 유도하였으며, 물체를 둘러싼 격자계의 독립적인 처리를 위해 개발된 비정렬 중첩격자기법과 연계하였다. 개발된 해석기법은 유도무기의 받음각이 0도와 5도인 경우의 기체분리운동 해석에 적용되었으며, 이를 통해 본 연구에서의 해석기법이 다중 물체간의 상대운동이 있는 비정상 유동장을 해석하는데 효과적임을 알 수 있었다.

수중 영상 소나의 번들 조정과 3차원 복원을 위한 운동 추정의 모호성에 관한 연구 (Bundle Adjustment and 3D Reconstruction Method for Underwater Sonar Image)

  • 신영식;이영준;최현택;김아영
    • 로봇학회논문지
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    • 제11권2호
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    • pp.51-59
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    • 2016
  • In this paper we present (1) analysis of imaging sonar measurement for two-view relative pose estimation of an autonomous vehicle and (2) bundle adjustment and 3D reconstruction method using imaging sonar. Sonar has been a popular sensor for underwater application due to its robustness to water turbidity and visibility in water medium. While vision based motion estimation has been applied to many ground vehicles for motion estimation and 3D reconstruction, imaging sonar addresses challenges in relative sensor frame motion. We focus on the fact that the sonar measurement inherently poses ambiguity in its measurement. This paper illustrates the source of the ambiguity in sonar measurements and summarizes assumptions for sonar based robot navigation. For validation, we synthetically generated underwater seafloor with varying complexity to analyze the error in the motion estimation.

불규칙파 중 초대형 부유식 해양 구조물에 대한 운동 해석 (Motion Analysis of a Very Large Floating Structure in Irregular Waves)

  • 신현경;이호영;임춘규;신현수;박인규
    • 한국해양공학회:학술대회논문집
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    • 한국해양공학회 2000년도 춘계학술대회 논문집
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    • pp.63-68
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    • 2000
  • A very large floating structure has rather small motion characteristics as to the whole body, while the motion at end part of such structure becomes largest due to the elastic motion of the structure. This paper presents on the theoretical result on the relative motion characteristics and green water phenomena of VLFS in waves This phenomena affect not only to strength of the structure but also the determination of depth of structure. To predict motion responses of structure in regular waves, the source-dipole distribution method and F.E.M is used By irregular wave results, the probability of occurrence of green water and response of the structure were calculated.

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Modeling and Simulation of Aircraft Motion on the Ground: Part I. Derivation of Equations of Motion

  • Ro, Kapseong;Lee, Haechang
    • International Journal of Aeronautical and Space Sciences
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    • 제2권1호
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    • pp.28-43
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    • 2001
  • Developed in these two series of paper is a complex dynamic model representing the motion of aircraft on the ground and a computer program for numerical simulation. The first part of paper presents the theoretical derivation of equations of motion of the landing gear system based on the physical principle. Developed model is 'structured' in the sense that the undercarriage system is regarded as an assembly of strut, tire, and wheel, where each component is modeled by a separate module. These modules are linked with two external modules-the aircraft and the runway characteristics-to carry out dynamic analysis and numerical simulation of the aircraft motion on the ground. Three sets of coordinate system associated with strut, wheel/tire and runway are defined, and external loads to each component and response characteristics are examined. Lagrangian formulation is used to derive the undercarriage equations of motion relative to the moving aircraft, and the resultant forces and moments from the undercarriage are transformed to aircraft body axes.

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카메라를 이용한 3차원 공간상의 이동 목표물의 거리정보기반 모션추정 (Motion Estimation of a Moving Object in Three-Dimensional Space using a Camera)

  • 좌동경
    • 전기학회논문지
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    • 제65권12호
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    • pp.2057-2060
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    • 2016
  • Range-based motion estimation of a moving object by using a camera is proposed. Whereas the existing results constrain the motion of an object for the motion estimation of an object, the constraints on the motion is relieved in the proposed method in that a more generally moving object motion can be handled. To this end, a nonlinear observer is designed based on the relative dynamics between the object and camera so that the object velocity and the unknown camera velocity can be estimated. Stability analysis and simulation results for the moving object are provided to show the effectiveness of the proposed method.

김벌 베어링 마찰의 영향을 고려한 4축 안정화 플랫폼의 운동에 관한 연구 (A Study of Motion for Four-Axis Stabilized Platform Including Effects of Gimbal Bearing Friction)

  • 신용진;조겸래;이진걸;조설;최석
    • 한국정밀공학회지
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    • 제12권6호
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    • pp.52-63
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    • 1995
  • This paper presents a detailed derivation of the equations of motion for the stable member of a four-axis platform. Gimbal bearing friction is considered for motion analysis. First, dynamic characteristics of platform, gimbal and gyro with Coulomb friction are studied due to vehicle's angular motion. Second, Vehicle's motion is assumed the sinusoidal function and dynamic characteristics of platform, gimbal and gyro are studied. Conclusively, considering effects of Coulomb friction, they could not follow the vehicle's angular motion and have constant errors. In case of sinusoidal motion, relative angles for each gimbal are amplified, but they are sinusoidal function with almost the same phases.

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듀얼 쿼터니언을 이용한 인공위성 근접운용에서의 위치-자세 결합운동 연구 (Position-Attitude Coupling Motion Using Dual Quaternion in Spacecraft Proximity Operation)

  • 나윤주;방효충
    • 한국항공우주학회지
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    • 제47권11호
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    • pp.795-802
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    • 2019
  • 본 논문에서는 인공위성의 근접운용에서 발생할 수 있는 위치-자세 결합운동을 정의하고, 이를 듀얼 쿼터니언 기반의 운동방정식을 통해 접근한다. 인공위성의 위치-자세 결합운동은 두 위성의 상대운동에서 목표 지점이 무게 중심이 아닌 위성체 위의 임의의 점에 위치할 때 발생하며, 특히 근거리 운용에서 명확히 보여진다. 듀얼 쿼터니언 기반의 운동방정식은 각속도 상태를 직접 반영하여, 자세의 변화가 위치에 영향을 미치는 위치-자세 결합운동을 간결하게 정의할 수 있다. 여기에서는 위치-자세 결합운동의 해결을 위해 기존의 접근방법과 함께 듀얼 쿼터니언 기반의 운동방정식을 새롭게 제시한다. 수치 시뮬레이션에서는 두 위성의 상대운동에서 위치-자세 결합운동으로 목표 지점에 대한 위치 오차가 발생함을 보이고, 듀얼 쿼터니언 기반의 운동방정식이 이를 해결할 수 있음을 검증한다.