• Title/Summary/Keyword: Analytical Prediction

Search Result 872, Processing Time 0.03 seconds

An Experimental Study on the Prediction Control Technique for a Magnetic Bearing (자기베어링 예측 제어 기법의 실험적 연구)

  • Kim, Chae Sil;Jung, Hoon Hyung;Shin, Min Jae
    • Journal of the Korean Society for Precision Engineering
    • /
    • v.31 no.2
    • /
    • pp.99-104
    • /
    • 2014
  • Active vibration control methods are required in the high speed rotor systems supported by magnetic bearings. A prediction control technique is one of the control methods. Gain and phase angle are primarily chosen with analyzing the responses for a certain rotor speed. The feasibility of this technique has been reported for only analytical simulations. Therefore this paper constructs the test rig supported by ball bearings with a magnetic bearing type actuator and develops a prediction control system by using LabVIEW and Compact RIO. Finally as rotating speeds are modulated, the gains and phase angles for the speeds are determined with vibration control of the test rig. This leads that the prediction control technique may be applied to the rotor system with the magnetic bearing.

An Overview of Flutter Prediction in Tests Based on Stability Criteria in Discrete-Time Domain

  • Matsuzaki, Yuji
    • International Journal of Aeronautical and Space Sciences
    • /
    • v.12 no.4
    • /
    • pp.305-317
    • /
    • 2011
  • This paper presents an overview on flutter boundary prediction in tests which is principally based on a system stability measure, named Jury's stability criterion, defined in the discrete-time domain, accompanied with the use of autoregressive moving-average (AR-MA) representation of a sampled sequence of wing responses excited by continuous air turbulences. Stability parameters applicable to two-, three- and multi-mode systems, that is, the flutter margin for discrete-time systems derived from Jury's criterion are also described. Actual applications of these measures to flutter tests performed in subsonic, transonic and supersonic wind tunnels, not only stationary flutter tests but also a nonstationary one in which the dynamic pressure increased in a fixed rate, are presented. An extension of the concept of nonstationary process approach to an analysis of flutter prediction of a morphing wing for which the instability takes place during the process of structural morphing will also be mentioned. Another extension of analytical approach to a multi-mode aeroelastic system is presented, too. Comparisons between the prediction based on the digital techniques mentioned above and the traditional damping method are given. A future possible application of the system stability approach to flight test will be finally discussed.

Machine Learning vs. Statistical Model for Prediction Modelling: Application in Medical Imaging Research (예측모형의 머신러닝 방법론과 통계학적 방법론의 비교: 영상의학 연구에서의 적용)

  • Leeha Ryu;Kyunghwa Han
    • Journal of the Korean Society of Radiology
    • /
    • v.83 no.6
    • /
    • pp.1219-1228
    • /
    • 2022
  • Clinical prediction models has been increasingly published in radiology research. In particular, as a radiomics research is being actively conducted, the prediction model is developed based on the traditional statistical model, as well as machine learning, to account for the high-dimensional data. In this review, we investigated the statistical and machine learning methods used in clinical prediction model research, and briefly summarized each analytical method for statistical model, machine learning, and statistical learning. Finally, we discussed several considerations for choosing the prediction modeling method.

Common Model EMI Prediction in Motor Drive System for Electric Vehicle Application

  • Yang, Yong-Ming;Peng, He-Meng;Wang, Quan-Di
    • Journal of Electrical Engineering and Technology
    • /
    • v.10 no.1
    • /
    • pp.205-215
    • /
    • 2015
  • Common mode (CM) conducted interference are predicted and compared with experiments in a motor drive system of Electric vehicles in this study. The prediction model considers each part as an equivalent circuit model which is represented by lumped parameters and proposes the parameter extraction method. For the modeling of the inverter, a concentrated and equivalent method is used to process synthetically the CM interference source and the stray capacitance. For the parameter extraction in the power line model, a computation method that combines analytical method and finite element method is used. The modeling of the motor is based on measured date of the impedance and vector fitting technique. It is shown that the parasitic currents and interference voltage in the system can be simulated in the different parts of the prediction model in the conducted frequency range (150 kHz-30 MHz). Experiments have successfully confirmed that the approach is effective.

Analysis of Thrust/Torque Signature of MOV (원자력 발전소 모터구동밸브의 쓰러스트/토크 신호 분석)

  • Ryu, Ho-Geun;Park, Seong-Keun;Kim, Dae-Woong
    • Proceedings of the KSME Conference
    • /
    • 2001.06e
    • /
    • pp.613-618
    • /
    • 2001
  • For the evaluation of operability of MOV(Motor Operated Valve), the precision prediction of thrust/torque acting on the valve is important. In this paper, the analytical prediction method of thrust/torque was proposed. The design basis stem thrust calculation typically considers the followings: Packing thrust, Stem rejection load, design basis differential pressure load. In general, test results show that temperature, pressure, fluid type, and differential pressure, independently and combination, all have an effect on the friction factor. The prediction results of thrust/torque are well agrement with dynamic test results.

  • PDF

A Study on the Prediction of the Aerodynamic Characteristics of a Launch Vehicle Using CFD (전산유동해석에 의한 발사체 공력 특성 예측에 관한 연구)

  • Kim Younghoon;Ok Honam;Kim Insun
    • 한국전산유체공학회:학술대회논문집
    • /
    • 2004.03a
    • /
    • pp.17-22
    • /
    • 2004
  • A space launch vehicle departs the ground in a low speed, soon reaches a transonic and a supersonic speed, and then flies in a hypersonic speed into the space. Therefore, the design of a launch vehicle should include the prediction of aerodynamic characteristics for all speed regimes, ranging from subsonic to hypersonic speed. Generally, Empirical and analytical methods and wind tunnel tests are used for the prediction of aerodynamic characteristics. This research presents considerable factors for aerodynamic analysis of a launch vehicle using CFD. This investigation was conducted to determine effects of wake over the base section on the aerodynamic characteristics of a launch vehicle and also performed to determine effects of the sting which exist to support wind tunnel test model.

  • PDF

State of the Art on Prediction of Concrete Pumping

  • Kwon, Seung Hee;Jang, Kyong Pil;Kim, Jae Hong;Shah, Surendra P.
    • International Journal of Concrete Structures and Materials
    • /
    • v.10 no.sup3
    • /
    • pp.75-85
    • /
    • 2016
  • Large scale constructions needs to estimate a possibility for pumping concrete. In this paper, the state of the art on prediction of concrete pumping including analytical and experimental works is presented. The existing methods to measure the rheological properties of slip layer (or called lubricating layer) are first introduced. Second, based on the rheological properties of slip layer and parent concrete, models to predict concrete pumping (flow rate, pumping pressure, and pumpable distance) are explained. Third, influencing factors on concrete pumping are discussed with the test results of various concrete mixes. Finally, future need for research on concrete pumping is suggested.

Prediction of the Radiated Noise of a Structure Excited by Harmonic Force Using the Doubly Asymptotic Approximation (이중점근 근사법을 이용한 조화가진 구조물의 방사소음 예측)

  • Han, Seungjin;Jung, Woojin
    • Transactions of the Korean Society for Noise and Vibration Engineering
    • /
    • v.27 no.1
    • /
    • pp.51-56
    • /
    • 2017
  • This paper presents an approach of predicting the radiated noise due to the structural vibration by internal harmonic forces using the doubly asymptotic approximation (DAA). Acoustic transfer vector is derived from the Helmholtz integral equation and the fluid-structure interaction relation of DAA. Numerical results and analytical results of radiated noise for a cylindrical shell were compared and showed that they were consistent in most of frequencies and radiation directions, but showed errors in some radiated directions in the mid-frequency region. Despite these errors, the prediction method will be suitable for practical radiated noise prediction.

A study on the availability prediction analysis for the Environmental Satellite Earth Station (환경위성지상국 시스템 가용도 예측분석 연구)

  • Eun, Jong Won;Choi, Won Jun;Lee, Eun Gyu
    • Journal of Satellite, Information and Communications
    • /
    • v.10 no.4
    • /
    • pp.107-112
    • /
    • 2015
  • To predict the system availability of the National Environmental Satellite Center Earth Station, mathematical models of H/W and S/W availability, the availability estimating methods for parallel were systematically presented in this paper. Furthermore, the results of the availability prediction for the Environmental Satellite Earth Station were estimated. The analytical results of Environmental Satellite Earth Station system availability were estimated as 0.998072.

Prediction of Steady-state Strip Profile during Hot Rolling - PartⅡ: Development of a Mathematical Model (열연 공정 정상상태 판 프로파일 예측 - PartⅡ: 수식 모델 개발)

  • Lee, J. S.;Hwang, S. M.
    • Transactions of Materials Processing
    • /
    • v.25 no.1
    • /
    • pp.61-66
    • /
    • 2016
  • In the current study, we present a new model for the prediction of the strip profile and the residual stresses. This new approach is an analytical model that predicts the residual stresses from the effect of post-deformation. Since the residual stress cannot exceed the yield strength of the material, post-yielding may possibly occur in the post-deformation zone prior to the strip reaching the steady-state zone. The prediction accuracy of the proposed model is examined through comparison with the predictions from 3-D finite element (FE) simulations.