• Title/Summary/Keyword: 저속 회전

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Horizontal-Axis Wind Turbine System Modeling using Multi-body Dynamics (다몸체 역학을 이용한 수평축 풍력발전 시스템 모델링)

  • 민병문;노태수;송승호;최석우
    • The Transactions of the Korean Institute of Power Electronics
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    • v.9 no.1
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    • pp.1-9
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    • 2004
  • In this paper, an efficient modeling method of Horizontal-Axis Wind Turbine(HAWT) system is proposed. This method Is based on representing a HAWT system as a multi-body system with several rigid bodies i.e. rotor blade, low/high speed shaft, gear system, md generator. Also, simulation software WINSIM is developed to evaluate performance of wind turbine system. Simulation results show that the proposed modeling method and simulation software are efficient and reliable.

Sensorless Control of BLDC Motor Using Novel RPEPA (새로운 회전자 위치 오차예측 알고리즘을 이용한 BLDC 전동기의 센서리스 제어)

  • Park, Hyung-Joon;Jang, Jae-Hoon;Kim, Jong-Sun;Lee, Sang-Bin;Yoo, Ji-Yoon
    • Proceedings of the KIPE Conference
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    • 2005.07a
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    • pp.224-226
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    • 2005
  • 본 논문에서는 새로운 회전자 위치 오차 예측 알고리즘(RPEPA)를 이용한 BLDC 전동기의 센서리스 제어 방법을 제안한다. 회전자 위치 정보는 3상 단자 전압으로부터 간접적인 Back-EMF 검출에 의해 추정되고, 저역통과 필터는 스위칭 노이즈 제거를 위해 사용된다. 제안한 방법은 저속 영역에서 기존 방법들 보다 향상된 성능을 갖고 있다. 필터에 의해 발생되는 위상 오차는 새로운 RPEPA에 의해 실시간 보상되어 정확한 전환시점을 결정한다. RPEPA를 이용한 센서리스 방법은 넓은 속도범위와 전동기의 효율을 개선시킨다. 제안한 방법은 실험을 통하여 타당성과 효율성을 검증한다.

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Verification of Navigation System of Guided Munition by Flight Experiment (비행 실험을 통한 유도형 탄약 항법 시스템 검증)

  • Kim, Youngjoo;Lim, Seunghan;Bang, Hyochoong;Kim, Jaeho;Pak, Changho
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.44 no.11
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    • pp.965-972
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    • 2016
  • This paper presents results of flight experiments on a navigation algorithm including multiplicative extended Kalman filter for estimating attitude of the guided munition. The filter describes orientation of aircraft by data fusion with low-cost sensors where measurement update is done by multiplication, rather than addition, which is suitable for quaternion representation. In determining attitude from vector observations, the existing approach utilizes a 3-axis accelerometer as a 2-axis inclinometer by measuring gravity to estimate pitch and roll angles, while GNSS velocity is used to derive heading of the vehicle. However, during accelerated maneuvers such as coordinated flight, the accelerometer provides inadequate inclinometer measurements. In this paper, the measurement update process is newly defined to complement the vulnerability by using different vector observations. The acceleration measurement is considered as a result of a centrifugal force and gravity during turning maneuvers and used to estimate roll angle. The effectiveness of the proposed method is verified through flight experiments.

A novel indirect rotor position sensing method to improve the performance of sensorless drive for brushless DC motors (브러시리스 직류 전동기 센서리스 드라이브의 성능 향상을 위한 새로운 회전자 위치 간접 검출 방식)

  • 조현민;박정배;이광운;여형기;유지윤
    • The Transactions of the Korean Institute of Power Electronics
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    • v.5 no.1
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    • pp.95-103
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    • 2000
  • In this paper, a novel indirect rotor position sensing method is proposed to improve the performClIlce of sensorless drive of brushless DC motors. The fast mode change to the sensorless operation is difficult in the existing indirect rotor position sensing methods because a precise rotor position can not be obtained when an excessive input is applied to the drive during synchronous operation mode. To cope with this problem, the relationship between terminal voltage and back-emf waveform is analyzed in this paper, also a novel indirect position sensing method which can detect a precise rotor position at low speed range is proposed. The effectiveness of the proposed method is verified through the experimental results.

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Development of Magnus Effect Measurement Technique for Spinning Projectile (회전 발사체용 마그너스 효과 특정기법의 개발)

  • Oh, Se-Yoon;Kim, Sung-Cheol;Lee, Do-Kwan;Choi, Joon-Ho;Ahn, Seung-Ki
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.35 no.1
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    • pp.79-86
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    • 2007
  • The Magnus effect measurement apparatus was designed and built for spinning wind tunnel model which would simulate the rotation of projectiles. Prior to the high speed test, the ground functional test and the low speed test were carried out in the Agency for Defense Development's Low Speed Wind Tunnel(ADD-LSWT) at spin rates from about 6,000 to 10,000 rpm. Magnus force and moment were measured on the spinning projectile model at velocity of 100 m/s. It was shown that the Magnus force and moment were linear function of spin parameter. The test results were compared with Magnus test run on the same configuration in the Arnold Engineering Development Center's Propulsion Tunnel 4T(AEDC-4T).

A Study on ADS-33E with Application to the Assessment of Handling Quality for Unmanned Rotorcraft (회전익 무인항공기의 비행안정성 규명을 위한ADS-33E 적용기법 연구)

  • Jeong, Hwan-Ho;Suk, Jin-Young;Kim, Byoung-Su;Lee, Sang-Kee
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.40 no.3
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    • pp.243-250
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    • 2012
  • In this paper, a systematic consequence of evaluation method, procedure, and flight data analysis is investigated for application of ADS-33E-PRF to UAV. And it is applied to unmanned rotorcraft for evaluation. CNUHELI-020, which is developed in Chungnam National University, is used for assessment of handling quality: decoupled longitudinal and lateral/directional model were used to assess handling qualities. Evaluation flight maneuvers are categorized as hover/low-speed requirements, small-amplitude attitude change, and moderate-amplitude attitude change requirements.

Initial Rotor Position Detection of Single-phase Permanent Magnet Synchronous Motor using Offset Voltage (옵셋 전압을 이용한 단상 영구자석 동기 전동기의 초기 회전자 위치 검출)

  • Hwang, Seon-Hwan;Seo, Sung-Woo;Jung, Tae-Uk
    • Journal of IKEEE
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    • v.23 no.2
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    • pp.622-627
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    • 2019
  • This paper propose an initial rotor position detection method for sensorless operation of a single-phase permanent magnet synchronous motor(SP-PMSM) with asymmetric air-gap. In general, the sensorless control based on back-emf estimation is difficult to estimate the back-emf at the zero and low speed regions. For this reason, an open loop start-up technique is indispensable, and it is also necessary to detect the initial position of the rotor in order to rotate in a certain direction. In this paper, we propose a method to detect rotor polarity by adding offset voltage to high frequency voltage signal based on the magnetic characteristics of SP-PMSM. The validity and usefulness of the proposed algorithm are verified through several experimental results.

Enhanced Motor Speed Estimation in Low Speed Range Based on the Observer Theory (관측기 이론에 기초한 저속 모터 속도 추정 및 성능 개선)

  • Baek, Lin;Ahn, Hyun-Sik
    • Proceedings of the IEEK Conference
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    • 2003.07c
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    • pp.2497-2500
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    • 2003
  • 본 논문에서는 저속으로 회전하는 모터의 속도를 추정함에 있어서 속도 관측기를 이용하고 적절한 보상을 통해 가속/감속 운전 시에도 속도 추정 성능을 개선시킨다. 가속도 정보를 이용한 보상을 통해, 모터 인코더카운터 값으로부터 발생하는 양자화 오차를 줄인다. 가속/감속 운전시 인코더 펄스에 의한 평균속도는 펄스가 발생한 시점에서 불연속일 수밖에 없게 된다. 제안된 방식은 이 불연속적인 평균속도를 가속도 보상을 통해 연속적으로 증감하는 보상된 속도를 얻고 이를 다시 관측기 입력에 보상하여 양자화 오차를 감소시킨다.

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The comparison of AE and Acceleration transducer for the early detection on the low-speed bearing (저속 회전 베어링 결함 검출을 위한 AE와 가속도계 변환기 비교)

  • Kim, H.J.;Gu, D.S.;Jeong, H.E.;Tan, Andy;Kim, Eric;Choi, B.K.
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2007.05a
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    • pp.324-328
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    • 2007
  • Vibration monitoring of rolling element bearings is probably the most established diagnostic technique for rotating machinery. Acoustic Emission (AE) Analysis is an extremely powerful technology that can be used within a wide range of applications of non destructive testing. Therefor, this paper investigates the detection methods using AE for rolling element bearings about low-speed. Two transducers, the accelerometer and acoustic emission sensor, are used to acquire data and the results are compared for the capacity of early fault detection.

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Analysis of Flux Weakening Operating Regions for IPMSM (매입형 영구자석 동기전동기의 약자속 운전영역 특성 분석)

  • Oh, Ye-Jun;Ahn, Han-Woong;Kim, In-Gun;Lim, Dong-Gun;Cho, Su-Yeon;Lee, Ju
    • Proceedings of the KIEE Conference
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    • 2015.07a
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    • pp.676-677
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    • 2015
  • 본 논문에서는 매입형 영구자석 동기전동기로 Belt-Type ISG(Integrated Starter Generator)를 설계하였다. 전동기는 저속영역에서 동손이 크고, 고속 영역에서는 철손의 비중이 크게 나타난다. ISG의 경우 전동기로 동작하는 저속영역은 동작시간이 짧기에 효율이 크게 중요하지 않지만 발전기동작은 고속영역에서 장기간 이루어지기에 이 구간에서 효율을 높이는 것이 중요하다. 특히 분포권에서는 전체 손실성분 중에서 회전자의 영구자석 기본파와 고조파 기자력에 의해 발생하는 치에서의 철손이 가장 큰 비중을 차지한다. 본 논문에서는 분포권에서의 철손에 대해서 분석하고 주된 손실의 원인인 치에서의 철손을 저감하는 설계를 수행하여 효율을 향상시켰다.

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