• Title/Summary/Keyword: 유도기법

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Adaptive Fuzzy based Sliding Mode Control for an Induction Motor Drive fed by a Matrix Converter (매트릭스 컨버터로 구동되는 유도전동기 구동장치를 위한 적응 퍼지 기법 기반의 슬라이딩 모드 제어기)

  • Park, Ki-Woo;Jou, Sung-Tak;Park, Mun-Soo;Lee, Kyo-Beum
    • Proceedings of the KIPE Conference
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    • 2008.10a
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    • pp.224-226
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    • 2008
  • 본 논문에서는 매트릭스 컨버터로 구동되는 유도전동기의 속도제어 성능을 향상시키기 위한 적응제어 기법을 제안한다. 유도 전동기는 비선형적 마찰력 등으로 인한 비선형적 특성을 가진다. 이러한 비선형적 특성으로 인해 야기되는 왜곡을 보상하고 속도제어 성능을 개선하기 위해 슬라이딩 모드 제어 기법을 적용한다. 슬라이딩 모드에서 발생하는 채터링 현상과 모델링되지 않은 유도 전동기의 불확실성에 의한 제어 성능 저하를 개선하기 위해, 불확실성 추정을 위한 퍼지 기반 불확실성 추정기를 적용한다. 시뮬레이션을 통해 제안한 제어기법의 타당성을 검증한다.

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Homing Guidance Law and Spiral Descending Path Design for UAV Automatic Landing (무인항공기 자동착륙을 위한 나선형 강하궤적 및 종말유도 설계)

  • Yoon, Seung-Ho;Kim, H.-Jin;Kim, You-Dan
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.38 no.3
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    • pp.207-212
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    • 2010
  • This paper presents a spiral descending path and a landing guidance law for net-recovery of a fixed-wing unmanned aerial vehicle. The net-recovery landing flight is divided into two phases. In the first phase, a spiral descending path is designed from an arbitrary initial position to a final approaching waypoint toward the recovery net. The flight path angle is controlled to be aligned to the approaching direction at the end of the spiral descent. In the second phase, the aircraft is guided from the approaching waypoint to the recovery net using a pseudo pursuit landing guidance law. Six degree-of-freedom simulation is performed to verify the performance of the proposed landing guidance law.

Sensorless Vector Control with On-Line Stator Resistance Tuning of Wound Induction Motor Using a MRAS (MRAS를 이용한 권선형 유도전동기의 온-라인 고정자 저항 조정에 의한 속도센서리스 벡터제어)

  • Lee Jae-Hak;Kim Yoon-Ho
    • Proceedings of the KIPE Conference
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    • 2001.07a
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    • pp.422-425
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    • 2001
  • 권선형 유도전동기는 기동시에 충분히 큰 저항을 외부에서 삽입하여 기동전류를 작게하는 동시에 기동 토크를 크게 할 수 있다. 또한, 유도전동기의 각 기동 방식중에서 가장 우수한 시동특성을 가지고 있으며 크레인, 시멘트공장 등 중부하 시동이 요구되는 경우 널리 사용되고 있다. 권선형 유도전동기 드라이브 시스템의 전류, 토크, 위치 및 속도 등의 제어를 위하여 일반적으로 산업현장에서는 Pl 제어기가 많이 적용되고 있다. 그러나 이러한 시스템은 센서 부착시 여러가지 환경적 제약으로 인한 전체시스템의 성능 저하를 가져올 수 있어 이를 개선하기 위한 센서리스 벡터제어가 활발히 연구되고 있다. 본 논문은 권선형 유도 전동기의 센서리스 벡터제어를 위해 MRAS 기법을 적용하였고, 기존의 MRAS 기법 적용시 발생하는 파라미터 변동에 따른 속도추정오차를 개선하기 위해 센서리스 벡터제어의 속도제어에 크게 영향을 미치는 고정자 저항을 온라인으로 튜닝함으로서 파라미터 변화에 강인한 센서리스 속도제어를 구현하였다. 제안된 기법의 타당성 및 유효성을 디지털 컴퓨터에 의한 시뮬레이션에 의해 확인하였다.

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A Control Strategy for Flywheel Energy Storage / Recovery System with Induction Machine (유도기를 이용한 플라이휠 에너지 저장 및 재생 시스템 제어 기법)

  • Son Jang-Kyung;Lee Hong-Hee;Nho Eui-Cheol;Kim Heung-Gun;Chun Tae-Won
    • The Transactions of the Korean Institute of Power Electronics
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    • v.10 no.5
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    • pp.494-500
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    • 2005
  • The paper proposed a control strategy for flywheel energy/recovery system with induction machine at the dynamic UPS system using the flywheel stored mechanical energy. The performances for the vector controlled induction generator are compared with those for the induction generator using slip control method. The strategy to improve the transient responses for dc link capacitor voltage is suggested at the transition from the motoring mode to the generating mode. The strategy Proposed by the paper is verified with experiment results using 32bit DSP.

Guided Wave Tomographic Imaging Using Boundary Element Method (경계요소법을 이용한 유도초음파 토모그래피 영상화 기법)

  • Piao, Yunri;Cho, Youn-Ho;Jin, Lianji;Ahn, Bong-Young;Kim, Noh-Yu;Cho, Seung-Hyun
    • Journal of the Korean Society for Nondestructive Testing
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    • v.29 no.4
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    • pp.338-343
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    • 2009
  • Tomography is the imaging method of cross sectional area using multi beam signals and is mainly applied to the medical diagnosis to acquire the image of the inside human body. This method is pretty meaningful in nondestructive evaluation field since the imaging of the inspection region can enhance the comprehension of the inspector. Recently, much attention has been paid to the guided wave for the diagnosis of platelike structures. So, in this work, a study on the imaging of the damage location in a plate was carried out on the basis of computer aided analysis of guided waves and tomographic imaging. To this end, boundary element method was employed to analyze the effect of the damage in plate on the propagation of the guided waves and the analytic results were applied to the tomographic imaging method to identify the damage location. Consequently, it was shown that the number of sensors heavily affect the inspection performance of the damage location.

Non-contact Ultrasonic Technique for the Evaluation Wall Thinning of the Plate (박판의 두께감육 평가를 위한 비접촉 유도초음파 검사 기법)

  • Park, Ik-Keun;Kim, Hyun-Mook;Kim, Tae-Hyung;Kim, Yong-Kwon;Cho, Yong-Sang;Song, Won-Joon
    • Journal of the Korean Society for Nondestructive Testing
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    • v.25 no.4
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    • pp.287-293
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    • 2005
  • Ultrasonic guided waves are gaining increasing attention for the inspection of platelike and rodlike structures. At the same time, inspection methods that do not require contact with the test piece are being developed for advanced applications. This paper capitalizes on recent advances in the areas of guided wave ultrasonics and noncontact ultrasonics to demonstrate a superior method for the nondestructive detection of defects thinning simulating hidden corrosion in thin aluminum plates. The proposed approach uses EMAT(electro-magnetic acoustic transducer) for the noncontact generation and detection of guided waves. Interesting features in the dispersive behavior of selected guided modes are used for the detection of plate thinning. It is shown that mode cutoff measurements provide a qualitative detection of defects thinning. Measurement of the mode group velocity can be also used to quantify depth thinning.

Aerodynamic Simulation of Air-Launched Missiles from a Complete Helicopter (헬리콥터 전기체에서 발사되는 유도무기 공력 모사)

  • Lee, Hee-Dong;Kwon, Oh-Joon;Lee, Bum-Seok;Noh, Kyung-Ho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.39 no.12
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    • pp.1097-1106
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    • 2011
  • Unsteady numerical analysis was performed to simulate air-launched missiles from a complete helicopter in hover by using an unstructured overset mesh flow solver coupled with a module of six degree-of-freedom motion of equations. The unsteady computations have been performed to obtain flow fields around the complete helicopter including main rotor, tail rotor, and fuselage equipped with multiple missiles, and six-DOF simulation has been performed to predict the behavior of the air-launched missile. The effects of the launching position and the missile thrust on the trajectory of the missile were investigated as well as the aerodynamic interference of the air-launched missile under the unsteady downwash produced by main rotor.

A Guidance Law Study for Anti-Ballistic Missile Defense (대탄도탄 방어용 유도기법 연구)

  • Jung, Ho Lac;Song, Taek Lyul
    • Journal of Advanced Navigation Technology
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    • v.2 no.2
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    • pp.84-99
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    • 1998
  • As a part of closed-loop guidance law studies for anti-ballistic missile defense, a mid-course guidance law is proposed to engage the target with the predetermined attitude for increased terminal effectiveness. The proposed guidance law is based on the predicted target position calculated from a simplified solution of target motion and the estimates of an extended Kalman filter utilizing noisy nonlinear radar measurements. Extension of the proposed mid-course guidance to 3 dimensional engagements are also studied. Performance of the proposed mid-course guidance law together with a terminal guidance law in the form of conventional proportional navigation guidance is evaluated by a series of simulation studies.

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Induction Motor Diagnosis System by Effective Frequency Selection and Linear Discriminant Analysis (유효 주파수 선택과 선형판별분석기법을 이용한 유도전동기 고장진단 시스템)

  • Lee, Dae-Jong;Cho, Jae-Hoon;Yun, Jong-Hwan;Chun, Myung-Geun
    • Journal of the Korean Institute of Intelligent Systems
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    • v.20 no.3
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    • pp.380-387
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    • 2010
  • For the fault diagnosis of three-phase induction motors, we propose a diagnosis algorithm based on mutual information and linear discriminant analysis (LDA). The experimental unit consists of machinery module for induction motor drive and data acquisition module to obtain the fault signal. As the first step for diagnosis procedure, DFT is performed to transform the acquired current signal into frequency domain. And then, frequency components are selected according to discriminate order calculated by mutual information As the next step, feature extraction is performed by LDA, and then diagnosis is evaluated by k-NN classifier. The results to verify the usability of the proposed algorithm showed better performance than various conventional methods.

Design of Current Controller for an Induction Motor using Robust Stability Theory (강인안정도 기법을 이용한 유도전동기의 전류 제어기 설계)

  • 박태식;유지윤
    • The Transactions of the Korean Institute of Power Electronics
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    • v.8 no.2
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    • pp.165-172
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    • 2003
  • In this paper, the new robust current control scheme is proposed for an Induction motor. The proposed design scheme of current controller tan obtain a specified stability margin through electrical parameter variation by using Kharitonov robust stability theory. The characteristics of the proposed design scheme are compared with those of a conventional scheme by computer simulation and its effectiveness and usefulness is verified by experiments on the 0.75kW induction motor drive.