• Title/Summary/Keyword: Torque Simulator

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A Study on the Simulator for Performance to Train Drive System (열차 추진 장치 모사를 위한 시뮬레이터 개발)

  • Ko Sung-Hwan;Chae Soo-Yong;Hong Soon-Chan;Ko Jung-Sun;Bae Chang-Han;Lee Byung-Song;Park Hyeon-Jun
    • Proceedings of the KIPE Conference
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    • 2006.06a
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    • pp.4-6
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    • 2006
  • 본 연구에서는 열차 추진 장치 시스템에 엔진의 중심부를 모의할 수 있는 Simplorer의 프로그램을 개발하여 M-G Set으로 모사한다. 열차의 엔진부와 발전기 구동에서의 제어는 DTC(Direct Torque Control) 제어로 모사 하였다. M-G Set을 구성은 견인력 토크지령을 받아 엔진부에서 DTC제어를 하였고, 발전기 구동 부는 속도지령을 받는 DTC제어로 하여 추진 장치 성능시험설비 열차운행모의에 의한 전력 조류 해석, 소비 및 회생전력을 분석할 수 있도록 하였다.

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Model-Based Loss Minimization Control for Induction Generators - in Wind Power Generation Systems (모델 기반의 풍력발전용 유도발전기의 최소 손실 제어)

  • Abo-Khalil, Ahmed G.;Lee, Dong-Choon
    • The Transactions of the Korean Institute of Electrical Engineers B
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    • v.55 no.7
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    • pp.380-388
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    • 2006
  • In this paper, a novel control algorithm to minimize the power loss of the induction generator for wind power generation system is presented. The proposed method is based on the flux level reduction, where the flux level is computed from the machine model for the optimum d-axis current of the generator. For the vector-controlled induction generator, the d-axis current controls the excitation level in order to minimize the generator loss while the q-axis current controls the generator torque, by which the speed of the induction generator is controlled according to the variation of the wind speed in order to produce the maximum output power. Wind turbine simulator has been implemented in laboratory to validate the theoretical development. The experimental results show that the loss minimization process is more effective at low wind speed and that the percent of power loss saving can approach to 25%. Experimental results are shown to verify the validity of the proposed scheme.

Control of an above-knee prosthesis using MR damper (MR 감쇠기를 이용한 무릎 관절 의족의 제어)

  • 김정훈;오준호
    • 제어로봇시스템학회:학술대회논문집
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    • 2000.10a
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    • pp.244-244
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    • 2000
  • We proposed the above-knee prosthesis using rotary MR damper in which knee joint is semi-actively controlled by microprocessor. Dissipation torque in the knee joint can be controlled by the magnetic field which is induced by applying current to a solenoid, Tracking control of knee joint angle was tested by 3-DOF Leg simulator. The experimental results show that the proposed above-knee prosthesis system had good performance in swing phase tracking and repetitive controller in conjunction with a computed control law and PD control law, reduced RMS tracking error as the repetitions of tracking. Moreover, desired knee angle trajectory was generated based on the estimation of gait period with the gyro signal and the tracking control was performed.

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Performance Simulation for a Dual Mass Flywheel using Discrete Model of Arcspring (아크스프링의 이산화 모델을 사용한 DMF 성능 시뮬레이션)

  • 김태현;김민성;송한림;어순기;김현수
    • Transactions of the Korean Society of Automotive Engineers
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    • v.12 no.4
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    • pp.146-153
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    • 2004
  • This paper presents a discrete analysis approach to investigate the performance of dual mass flywheel (DMF). In the discrete analysis, arcspring installed between the flywheels is modeled as N- discrete elements. Each element consists of mass, spring and nonlinear friction element. LuGre friction model is used to describe nonlinear friction characteristic. Based on the dynamic models of the DMF, clutch, engine, manual transmission and vehicle, a DMF performance simulator is developed using MATLAB Simulink. Simulation results of the engine speed, driveshaft torque and vehicle velocity are compared with test results. It is found that the discrete DMF model describes the vehicle behavior closely, especially during the clutch actuation period.

An Evaluation of Reliability of the Spur Gear Using the Accelerated Durability Analysis (가속내구해석을 이용한 평기어의 신뢰성 평가)

  • Kim Chul-Su;Kim Jung-Kyu;Kwon Yeo-Hyoun
    • Proceedings of the KSR Conference
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    • 2004.10a
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    • pp.722-727
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    • 2004
  • The gear that is used in various mechanical components occurs easily damages due to the repeated torque and the high oil temperature. The main failure mode of the gear is the surface deterioration with the tooth surface fatigue. Therefore, the life evaluation and the failure analysis of the gear were very important since it may cause fatal damage of entire gear box system. In this paper, the failure mechanism and the life of the gear were evaluated using the durability analysis simulator such as MSC.FATIGUE. Moreover, the reliability analysis model of the spur gear with the accelerated life testing technique was proposed.

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A Study on the Simulator for the Train Propulsin System of SVM-DTC (SVM-DTC 방식의 열차 추진 장치 모사를 위한 시뮬레이터 개발)

  • Kim, Young-Chan;Seo, Young-Ger;Bae, Chang-Han;Lee, Byung-Song;Hong, Soon-Chan;Ko, Jung-Sun
    • Proceedings of the KIPE Conference
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    • 2007.07a
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    • pp.406-408
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    • 2007
  • 현재 국가물류 수송의 경쟁력 향상과 증가되는 교통수요에 부응하기 위해 경부 고속철도의 건설 등 철도의 고속화와 수송량 증대에 많은 관심과 투자가 이루어지고 있지만, 점점 상승하는 유가 에너지 비용에 대한 문제가 발생하고 있어 전기 철도차량의 개발이 시급하다. 본 논문은 Simplorer 프로그램을 이용하여 열차 추진 장치에 관한 연구와 추후 열차 회생 에너지에 관한 연구를 하기 위해 추진 장치를 M-G set으로 구성 하였고 모터는 SVM(Space Vector PWM)방식으로, 제너레이터는 DTC(Direct Torque Control) 방식으로 제어하였다.

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A Study on Brushless Motor Design Algorithm Using Rotor Volume Ratio (회전자 체적비를 이용한 브러시레스 전동기 설계 알고리즘 연구)

  • Lee, Jeong-Jong;Ha, Jea-Pyong;Hong, Jung-Pyo;Lim, Yang-Su;Hur, Yun
    • Proceedings of the KIEE Conference
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    • 2003.07b
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    • pp.894-896
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    • 2003
  • This paper present the design algorithm using torque and rotor volume(TRV). And, this paper introduce that how to applying the 3-Dimensional Equivalent Magnetic Circuit Network(3D EMCN) and brushless motor circuit simulator. This algorithm is applied the design program, the design shape is compared with existed brushless motor.

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Torque Control System of DC-MOTOR for a Wind Turbine Simulator using Wind Generation Systems on Real Time (실시간 바람데이터 생성을 적용한 풍력터빈 시뮬레이터용 DC MOTOR의 토크 제어시스템)

  • Oh, Sung-Nam;Yun, Ki-Don;Kim, Gab-Il;Son, Young-Ik
    • Proceedings of the KIEE Conference
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    • 2003.11c
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    • pp.954-958
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    • 2003
  • 새로운 에너지원인 풍력 발전에 대한 연구가 세계적으로 활발히 진행되고 있는 가운데 본 논문에서는 풍력 발전의 핵심 부분인 풍력 터빈에 관한 모의실험을 다루고자 한다. 실제 기상조건과 유사한 바람데이터를 실시간으로 생성, 이를 이용하여 풍력터빈 시뮬레이터용 DC motor의 토크제어 시스뎀을 설계 구현하였다. 본 연구는 기존의 단순 토크제어 시스템과는 달리 실시간으로 생성되는 데이터를 이용하여 보다 실제 풍력발전에 가까운 모의실험을 가능하게 한다. M/G Set를 기반으로한 DC motor 토크 제어 시스템은 바람데이터의 변화에 따른 풍력터빈의 토크와 발전단의 부하의 상관관계를 명확히 하는데 크게 이바지 할 것이며 더 나아가 발전기로의 정확한 토크 전달로써 계통 연계 연구에 많은 기여를 하고자 한다.

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Constitutive Relation of Alloy Steels at High Temperatures

  • Lee, Young-Seog
    • International Journal of Precision Engineering and Manufacturing
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    • v.6 no.4
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    • pp.55-59
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    • 2005
  • This paper presents a feasibility study whether Shida's constitutive equation being widely used for plain carbon steel in steel manufacturing industry can be extended to alloy steels with a due carbon equivalent model. T,he constitutive relation of the alloy steels (SAE9254, AISI52100 and AISI4140) is measured using hot deformation simulator (GLEEBLE 3500C) at high temperatures ($800^{\circ}C{\~}1000^{\circ}C$) within strain rates of $0.05{\~}40\;s^{-1}$. It has been found the predicted flow stress behavior (constitutive relation) of AISI52100 steel is in agreement with the measured one. On the other hand, the measured flow stress behavior of SAE9254 and AISI4140 steel partly concords with the predicted one when material experiences relatively high strain rate ($10{\~}40\;s^{-1}$) deformation at low temperature ($800^{\circ}C$). It can be deduced that, for AISI52100 steel, Shida's equation with the carbon equivalent model can be applicable directly to the roughing and intermediate finishing stand in hot rolling process for calculating the roll force and torque.

Design of a Simulator and a Controller for ABS of Airplane

  • J.W. Jeon;J.H. Shin;Lee, K.C.;D.H. Hwang;Park, D.Y.;Kim, Y.J.
    • 제어로봇시스템학회:학술대회논문집
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    • 2001.10a
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    • pp.162.3-162
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    • 2001
  • The essence of ABS(Anti-skid Brake System) control is to continuously adjust brake pressure to maintain optimum brake torque. This optimum level should balance tire and runway friction its peak value, yielding maximum braking deceleration. It influences not only the deceleration and the taxing distance of an aircraft, but also the strength and the fatigue life of the landing gear. In this paper, an ABS control algorithm is developed with a dynamics model of 5-DOFD(Degree of Freedom). The algorithm is verified by simulations and the simulation results are presented. The dynamics model is simulated by the computer.

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