• Title/Summary/Keyword: 롤진동

검색결과 23건 처리시간 0.231초

Roll Motion Control of a Mover in Bearingless Linear Motor by Using One-sided Active Magnetic Bearings (베어링리스 리니어 모터에서의 편측식 전자기 베어링을 이용한 이동자의 롤 운동 제어)

  • Kim, Woo-Yeon;Lee, Jong-Min;Kim, Seung-Jong
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • 제19권11호
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    • pp.1184-1191
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    • 2009
  • A bearingless linear motor(BLLM) which consists of two stators and a common mover is able to levitate and move its mover without any linear bearing or even additive windings. In the previous study, BLLM was actively controlled on the translation and pitch motion, while the roll motion is passively stable. In order to control the roll motion, this paper suggests adding active magnetic bearings(AMBs) at bottom of the mover in BLLM. The AMBs control the roll motion and also partially supports the weight of the mover. In this paper, magnetic forces generated by the AMBs are estimated by using an FEM model. Based on the analysis results, the bias current of the AMBs is determined and a PD controller is designed. Through an experimental levitation test, it was verified that roll motion is well controlled by AMB during levitation.

Measurement of Dynamic Stability Derivatives of Tailless Lamda-shape UAV using Forced Oscillation Method (강제진동 기법을 이용한 무미익 비행체의 동안정 미계수 측정)

  • Yang, Kwangjin;Chung, Hyoungseog;Cho, Donghyun;An, Eunhye;Ko, Joonsoo;Hong, JinSung;Kim, Yongduk;Lee, MyungSup;Hur, Gi-Bong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • 제44권7호
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    • pp.552-561
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    • 2016
  • In this experimental study, the dynamic stability derivatives of a tailless lambda-shape UAV are estimated from time history data of aerodynamic moments measured from the internal balance while the test model is forced to oscillate at given frequencies and amplitudes. A 3-axis forced oscillation apparatus is designed to induce decoupled roll, yaw, pitch oscillations respectively. The results show that the roll damping derivatives remain stable at the entire range of angle of attack tested, whereas the pitch damping derivatives become unstable beyond $15^{\circ}$ angle of attack. The amplitude and frequency have little impact on roll damping derivatives while the smaller amplitude and frequency of oscillation improves the pitch stability. The yaw damping derivative values are fairly small as expected for a tailless configuration. The results indicate that the proposed methodology and test apparatus area valid for estimating the dynamic stability derivatives of a tailless UAV.

Development of R-Management Support System for detecting railway risk and reducing damage in Residential Areas (주거지역에서 철도위험상황 감지 및 피해 감소를 위한 R-운영지원 시스템 개발)

  • SuMan Lee;Moonho Chae;Fayzullayev mirjalol;Ryumduck Oh
    • Proceedings of the Korean Society of Computer Information Conference
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    • 한국컴퓨터정보학회 2023년도 제68차 하계학술대회논문집 31권2호
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    • pp.233-236
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    • 2023
  • 본 논문에서는 주거지역에서 철도 운행으로 발생하는 소음, 진동, 미세먼지가 거주민들에게 입히는 피해를 최소화 하기 위해 소음, 진동, 미세먼지의 수치 위험도 기준을 정하고, 아두이노 센서와 모듈로 스마트 창문 및 공기 청정기를 제작한다. 센서를 통해 수집한 데이터가 기준치를 초과할 경우 창문의 개폐 또는 공기 청정기 시스템이 작동을 하도록 구현하여 소음, 진동, 미세먼지 피해를 최소화 하도록 구현하였다.

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Flutter Mechanism Analysis for Firefly Export Model (반디호 수출형 시제기에 대한 플러터 매커니즘 분석)

  • Paek, Seung-Kil;Lee, Sang-Wook
    • Aerospace Engineering and Technology
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    • 제6권1호
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    • pp.35-44
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    • 2007
  • In this study was made the flutter analysis for the export model of Firefly(Bandi-ho), the small canard aircraft. Stiffness model based on internal load generation finite element model was generated. Mass model based on the weight DB for weight control was generated. Aerodynamic model based on Doublet Lattice Method was generated. Preliminary flutter analysis was made. Based on it, major vibration modes are identified and experimentally obtained via the ground vibration test. The obtained normal mode frequencies were used to correlate the finite element model. Flutter analysis was made again and major flutter mechanisms were summarized. The most important flutter root was identified as a coupled root between rigid body roll mode and anti-symmetric wing pitching mode.

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Ground-Roll Suppression of the Land Seismic Data using the Singular Value Decomposition (SVD) (특이값 분해를 이용한 육상 탄성파자료의 그라운드롤 제거)

  • Sa, Jin-Hyeon;Kim, Sung-Soo;Kim, Ji-Soo
    • The Journal of Engineering Geology
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    • 제28권3호
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    • pp.465-473
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    • 2018
  • The application of singular value decomposition (SVD) filtering is examined for attenuation of the ground-roll in land seismic data. Prior to the SVD computation to seek singular values containing the highly correlatable reflection energy, processing steps such as automatic gain control, elevation and refraction statics, NMO correction, and residual statics are performed to enhance the horizontal correlationships and continuities of reflections. Optimal parameters of SVD filtering are effectively chosen with diagnostic display of inverse NMO (INMO) corrected CSP (common shot point) gather. On the field data with dispersion of ground-roll overwhelmed, continuities of reflection events are much improved by SVD filtering than f-k filtering by eliminating the ground-roll with preserving the low-frequency reflections. This is well explained in the average amplitude spectra of the f-k and SVD filtered data. The reflectors including horizontal layer of the reservoir are much clearer on the stack section, with laminated events by SVD filtering and subsequent processing steps of spiking deconvolution and time-variant spectral whitening.

Process Analysis and Test for Manufacturing the Sleeve Spring Type-Torsional Vibration Damper (슬리브 스프링 형식 비틀림 진동감쇠기 제조를 위한 공정해석 및 시험)

  • Hwang, Beom-Cheol;Bae, Won-Byong;Jang, Young-Jun;Kim, Chul
    • Transactions of the Korean Society of Mechanical Engineers A
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    • 제33권12호
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    • pp.1471-1481
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    • 2009
  • In diesel engines, it is inevitable that the torsional vibration is produced by the fluctuation of engine torque. Therefore, it is necessary to establish preventive measures to diminish the torsional vibration. The sleeve spring type damper is one of the preventive measures for reducing the torsional vibration. In this study, the closed form equations to predict the spring constant of a sleeve spring and the torsional characteristics of the torsional vibration damper are proposed to calculate stiffness of the damper and verified their availability through the finite element analysis and experiments. And the stability of the sleeve spring torsional vibration damper is verified by analyzing the inner star and outer star, which are the core parts of the damper, and 2-roll bending process is proposed to manufacture sleeve spring. The program to calculate the initial radius including spring-back effect is developed, and the FEA method to analyze elasto-plastic problem was verified through analysis of 90$^{\circ}$bending process. The results of the analysis are in good agreements with those of the experiments. The newly proposed method can be used as an advanced technique that remarkably curtails cost of production and replaces the conventional forming.

Prediction of Pitch and Roll Dynamic Derivatives for Flight Vehicle using CFD (전산유체역학을 이용한 비행체의 피치와 롤 동안정 미계수 예측)

  • Lee, Hyung-Ro;Gong, Hyo-Joon;Kim, Beom-Soo;Lee, Seung-Soo
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • 제40권5호
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    • pp.395-404
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    • 2012
  • This paper presents computations of the dynamic derivatives of three dimensional flight vehicle configurations using CFD. The pitch dynamic derivatives are computed from the pitch sinusoidal motion, while the roll damping is computed based on steady state calculation using a non-inertial frame method. The Basic Finner and the SDM(Standard Dynamic Model) are chosen for the benchmark tests against other numerical and experimental results. For the flow calculations, a 3-D Euler solver that can be run both on the non-inertial frame and on the inertial frame is developed. A dual-time stepping method is applied for the unsteady time accurate simulations. A good agreement of pitch-roll dynamic derivatives with previously published numerical results and the experimental results is observed.

A Measurement of Sea Transportation Load (해상운송 하중측정)

  • Jeon, Yeong-Du;Park, Jong-Chan;Jo, Cheol-Hun;Park, Dong-Su;Jeong, Ui-Seung
    • Aerospace Engineering and Technology
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    • 제5권2호
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    • pp.143-148
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    • 2006
  • This article summarizes the results of sea transportation load measurements, which will be used as the reference to the sea transportation environment condition for the launch vehicle of KSLV-I. KSLV-I will be transported by Sea from Pusan to the NARO space center in Gohung, Chunnam province. Since the vibration load condition during sea transportation is considered as one of the important design parameters of KSLV-I and its transportation means, it is necessary to directly measure the environmental condition of sea transportation loads prior to establish the sea transportation plan in detail. This material includes the measured data of 3-axis linear accelerations and 3-axis angular rates on the board of a barge-ship, which is towed by a tug boat during shipping operation. This barge-ship is same class with one which will actually carry KSLV-I. The results show that the measured load condition during sea transportation is not severer than the reference data of MIL-STD-810F and Zenit-3SL launch system.

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Piezoelectric and Dielectric Characteristics of Low Temperature Sintering PMS-PNN-PZT Ceramics According to the Amount of PNN Substitution (PNN 치환에 따른 저온소결 PMS-PMN-PZT계 세라믹스의 압전 및 유전특성)

  • Lee, Snag-Ho;Kim, Kook-Jin;Yoo, Ju-Hyun;Hong, Jae-Il
    • Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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    • 한국전기전자재료학회 2007년도 하계학술대회 논문집 Vol.8
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    • pp.253-253
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    • 2007
  • 압전 액츄에이터 및 초음파진동자의 응용범위가 넒어짐에 따라 변위량, 응력 등을 개선시키기 위해 전기기계결합계수 kp 및 압전 d상수가 종전보다 큰 재료가 요구되고 있으며, 초음파진동자나 압전 모터와 같이 마찰에 의한 열손실이 많이 발생하는 액츄에이터에 적용할 큰 기계적품질계수롤 가지는 저손실 압전 액츄에이터 및 초음파진동자용 재료가 필요한 실정이다. PZT계 세라믹스는 높은 유전상수와 압전특성으로 전자세라믹스분야에서 가장 널리 사용되어지고 있지만, $1200^{\circ}C$이상의 높은 소결온도 때문에 $1000^{\circ}C$ 부근에서 급격히 휘발되는 PbO로 인한 환경오염과 기본조성의 변화로 인한 압전특성의 저하가 문제시 되고 있다. $Pb(Ni_{1/3}Nb_{2/3})O_3$는 약 $-120^{\circ}C$정도의 큐리온도룰 가지는 강유전체로 Pb(Zr, Ti)$O_3$계 세라믹스에 치환 시 유전상수와 전기기계결합계수를 개선시키는 대표적인 성분이다. 따라서 본 연구에서는 저온소결 저손실의 적층형 압전 액츄에이터를 개발하기 위해 PMS-PMN-PZT계 세라믹스에 $Pb(Ni_{1/3}Nb_{2/3})O_3$ 세라믹스를 치환하고 $Li_2CO_3$$Na_2CO_3$ ZnO를 소결조재로 사용하여 저온소결 하였으며 PNN 치환량에 따른 결과를 관찰 하였다.

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