• Title/Summary/Keyword: mass moment of inertia

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해저작업 로봇 매니퓰레이터의 강건한 신경망 제어기 (A Robust Neural Control of Robot Manipulator Operated Under the Sea)

  • 박예구;최형식;이민호
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1995년도 추계학술대회 논문집
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    • pp.337-341
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    • 1995
  • This paper presents a robust control scheme using a multilayer network for the robot manipulator operating under the sea which has large uncertainties such as the buoyancy and the added mass/moment of inertia. The multilayer neural network acts as a compensator of the conventional sliding mode controller to maintain the control performance when the initial assumptions of uncertainty bounds are not valid. By the computer simulation results, the proposed control scheme dose not effectively compensate large uncertainties, but also reduces the steady stare error of the conventional sliding mode controller.

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고속 연삭기 주축 시스템의 회전체 역학 해석 (Rotor Dynamics Analysis of a Spindle System for a High speed Grinding Machine)

  • 최영휴
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2000년도 춘계학술대회논문집 - 한국공작기계학회
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    • pp.714-719
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    • 2000
  • This paper describes a transfer matrix approach to analyze the dynamics of a high sped flexible rotor system supported at 2 positions by five ceramic bearings. The rotor system is modelled as lumped parameters in which many factors are considered not only lumped inertia or mass, bending moment, shear force but also gyroscopic effect and unbalance. The equation of motion is derived in the transfer matrix form, from which the eigenvalues equation is also derived. The transfer natural frequencies and modes. The eigenvalues, eigenmodes, campbell diagram, whirling critical speed, whirling modes, and the response of unbalance are calculated and discussed.

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플라이휠의 새로운 설계 해석 (A New Design Analysis of Flywheel)

  • 김재호;신영재
    • 대한기계학회논문집
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    • 제15권3호
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    • pp.1063-1066
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    • 1991
  • 본 연구에서는 기계 기구의 각속도 변동을 줄이는데 사용되는 플라이휠을 운동에너지의 법칙을 이용하여 해석하고, 주어진 허용 각속도 변동률을 정확히 만족하 는 플라이휠의 크기를 결정하는 새로운 방법을 제시하였다. 또한 수치 해석을 통하 여 본 해석방법에 의해 설계된 플라이휠과 종래 방법에 의한 플라이휠의 성능을 비교 하였다.

Bar Formation and Evolution in Disk Galaxies with Classical Bulges

  • Seo, Woo-Young;Kim, Woong-Tae
    • 천문학회보
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    • 제44권2호
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    • pp.37.2-37.2
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    • 2019
  • To study the effects of central mass concentration on the formation and evolution of galactic bars, we run fully self-consistent simulations of Milky Way-sized, isolated galaxies with initial classical bulges. We let the mass of a classical bulge mass less than 20% of the total disk mass, and vary the central concentration of a dark matter halo. We find that both classical bulge and halo concentration delay the bar formation and weaken the bar strength. The presence of a bulge increases the initial rotational velocity near the center and hence the bar pattern speed. Bars in galaxies with a more concentrated halo slowdown relatively rapidly as they lose their angular momentum through interaction with the halo. In some of our models, bars do not experience slowdown at the expense of the decrease in their moment of inertia as the bar evolves, with the resulting pattern speed similar to that of the bar in the Milky Way.

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특성행렬 직접 규명법에 의한 강체특성의 실험적 추정 (Experimental Identification of Rigid Body Properties by Direct System Identification Method)

  • Jeong, W.B.;Ryu, S.J.;Koe, D.M.
    • 한국정밀공학회지
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    • 제12권9호
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    • pp.22-29
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    • 1995
  • An experimental method to identify the rigid properties (mass, moment of inertia, center of mass) of mounted structures is presented. A direct system identification method is developed and applied to identify the mass, damping and stiffness martix directly from the translational response of vibration testing. Conventional method is sensitive to noise since it needs artificial rotational response of temporary center of mass which is made by the linear transformation of translational response. A presented method needs only the translational response, and it is robuster to noise than conventional method. Several experimental and numerical implementations show the presented method is effective.

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Spacecraft Spin Rate Change due to Propellant Redistribution Between Tanks

  • Choi, Kyu-Hong
    • Journal of Astronomy and Space Sciences
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    • 제1권1호
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    • pp.23-34
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    • 1984
  • A bubble trapped in the liquid manifold of INTELSAT IV F-7 spacecraft caused a mass imbalance between the System 1 propellant tanks and a wobble half angle of 0.38 degree to 0.48 degree. A maneuver on May 14, 1980 passed the bubble through the axial jet and allowed propellant to redistribute. A 0.2 rpm change in sin rate was observed with an exponential decay time constant of 6 minutes. In this paper, moment of inertia, tank geometry and hydrodynamic models are derived to match the observed spin rate data. The values of the total mass of propellant considered were 16, 19 and 20 kgs with corresponding mass imbalances of 14.3, 15 and 15.1 Kgs, respectively. The result shows excellent agreement with observed spin rate data but it was necessary to assume a greater mass of hydrazine in the tanks than propellant accounting indicated.

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Robust Adaptive Control Simulation of Wire-Suspended Parallel Manipulator

  • Farahani, Hossein S.;Kim, Bo-Hyun;Ryu, Je-Ha
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2004년도 ICCAS
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    • pp.46-51
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    • 2004
  • This paper presents an adaptive control method based on parameter linearization for incompletely restrained wire-suspended mechanisms. The main purpose of this control method is utilizing it in a walking assist service robot for elderly people. This method is computationally simple and requires neither end-effector acceleration feedback nor inversion of estimated inertia matrix. In the proposed adaptive control law, mass, moment of inertia and external force and torque on the end-effector are considered as components of parameter adaptation vector. Nonlinear simulation for walking an elderly shows the effectiveness of the parameter adaptation law.

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자율 주행 반송차의 궤적 오차와 마찰력에 대한 매개 변수의 민감도 해석 (Parameter Sensitivity Analysis of Autonomous Robot Vehicle for Trajectory Error and Friction Force)

  • 김동규;박기환;김수현;곽윤근
    • 한국자동차공학회논문집
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    • 제4권2호
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    • pp.115-126
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    • 1996
  • In order to obtain the principal design data for developing the Autonomous Robot Vehicle(ARV), Sensitivity analysis on the trajectory error and friction force with respect to the dynamic parameters is performed. In the straight motion, the trajectory error has been proved to be much affected by the mass variance of the ARV while the lateral friction force is much affected by the location of the mass center. In the curved motion, the effect of mass and moment of inertia is considered importantly. In addition, the lateral offset gives more effect than the geometric dimension of the ARV on the trajectory errors and friction force.

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볼 베어링 및 가스 포일 베어링으로 지지되는 고속 전동기의 회전체 관성정지 및 가속 성능 연구 (Rotor Coastdown and Acceleration Performances of High-speed Motors Supported on Ball Bearings and Gas Foil Bearings)

  • 문형욱;서정화;김태호
    • Tribology and Lubricants
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    • 제35권2호
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    • pp.123-131
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    • 2019
  • This study characterizes the coastdown performances of two small electric motors supported on high-speed ball bearings (BBs) and gas foil bearings (GFBs), and it predicts their acceleration performances. The two motors have identical permanent magnetic rotors and mating stators. However, the shaft of the GFBs has a larger mass and polar/transverse moments of inertia than that of the BBs. Motor coastdown tests demonstrate that the rotor speed decreases linearly with the BBs and nonlinearly with the GFBs. A simple model for the BBs predicts a constant drag torque and linear decay of speed with time. The test data validate the model predictions. For the GFBs, the hydrodynamic lubrication model predictions reveal that the drag torque increases linearly with speed, and the speed decreases exponentially with time. The predictions agree very well with the test data in the speed range of 100-30 krpm. The boundary lubrication model predicts a constant drag torque and linear decay of speed with time. The predictions agree well with the test data below 15 krpm. Mixed lubrication occurs in the speed range of 30-15 krpm. Rotor acceleration performances are predicted based on the characteristics of deceleration performances. The GFBs require more time to reach 100,000 krpm than the BBs because of their larger shaft polar moment of inertia. However, predictions for the assumed identical polar moment of inertia reveal that the GFBs have a nearly identical acceleration performance to that of the BBs with a motor torque greater than $0.03N{\cdot}m$.

주행하는 대형 트럭의 요관성모멘트 실시간 추정 (Real-Time Estimation of Yaw Moment of Inertia of a Travelling Heavy Duty Truck)

  • 이승용;나카노키미히코;김세광
    • 대한기계학회논문집A
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    • 제41권3호
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    • pp.205-211
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    • 2017
  • 차량제어의 고도화에 의해, 자동 대열 주행 제어와 같은 정밀한 제어의 필요성이 더욱 높아지고 있다. 정밀 제어를 수행하기 위해서는 차량제어에 필요한 차량 파라미터를 항상 파악하는 것이 중요하다. 특히 화물 운송용 트럭의 경우, 화물 적재 상태에 따라 차량 질량과 차량 관성모멘트 등의 차량 파라미터가 크게 변화한다. 따라서 미지의 파라미터가 있을 경우, 실시간으로 파라미터 추정하여 제어시스템에의 반영이 요구된다. 본 연구에서는 차량이 곡선 주행할 때에 차량의 조향제어에 중요한 차량 파라미터 중 하나인 요관성모멘트에 대하여 Dual Kalman filter알고리즘과 GPS센서를 이용하여 차량이 주행 중에 미지의 요관성모멘트 값을 실시간으로 추정할 수 있는 방법을 제안하고, 차량동역학 상용 프로그램을 이용한 시뮬레이션을 통해 추정방법의 타당성을 검토한다.