• Title/Summary/Keyword: oscillation control

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Control of Sound Pressure Inside a Flow Excited Resonator (유동가진 공명기 내부의 음압 제어)

  • Hwang, Cheol-Ho;Park, Jong-Beom
    • Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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    • 2005.11a
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    • pp.196-199
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    • 2005
  • Flow traveling over a cavity opening forms a vortex due to unstable shear layer and induces an aerodynamic pressure excitation from the diffusion of the vortex convecting out of the trailing edge of the opening. The interaction between the excitation force and the cavity response sustains resonance in the resonator(cavity) and locked-in vortex shedding at the leading edge of the opening. The aerodynamic excitation force can be described from the diffusion of the vortex over the trailing edge and the level of its diffusivity is related to the strength of vorticity seeded at the loading edge. In this study, the control scheme of the internal pressure oscillation was proposed from regulating the vorticity at the leading edge by use of an oscillating spoiler. It was found that the relative motion between the spoiler and the air mass at the cavity opening influenced vorticity strength and the control was achieved by direct feedback of the cavity pressure fluctuation to the actuator.

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Stable Load Control in Multipath Packet Forwarding (다중경로 패킷 전달환경에서의 안정적인 부하제어 기법)

  • Park, Il-Kyu;Kim, Jong-Sung;Lee, Youn-Seok;Choi, Yang-Hee
    • Journal of KIISE:Information Networking
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    • v.29 no.2
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    • pp.174-180
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    • 2002
  • With the invention of MPLS and the Improvement in traffic engineering, multipath packet forwarding and dynamic load control has become a reality. A dynamic load control, while it can improve network efficiency by controlling loads between paths according to the network state, can lead to unstable and oscillating state because of the staleness of the state information. In this paper, we propose a efficient load control scheme which remains stable. The proposed scheme introduces prediction to reduce the staleness of state message and to prevent oscillation.

An Adaptive Reclosing Algorithm Considering Distributed Generation

  • Seo, Hun-Chul;Kim, Chul-Hwan
    • International Journal of Control, Automation, and Systems
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    • v.6 no.5
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    • pp.651-659
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    • 2008
  • Autoreclosing techniques have been used in power systems to maintain system stability and continuity of supply. Environmental and economical issues have driven significant increases in the development of distributed generation (DG). DG connected to distribution systems, however, may impose negative influences with respect to power quality, protection, and stability, because DG can cause some challenges to protection, especially to reclosing. For this reason, in order to improve the reliability and safety of the distribution system, the rules and guidelines suggest that the DG system needs to be rapidly disconnected from the system before reclosing. We present, in this paper, an adaptive reclosing algorithm considering the DG. The algorithm consists of an angle oscillation's judgment, the emergency extended equal-area criterion (EEEAC), the calculation of an optimal reclosing time, and a reconnection algorithm. Our simulation results for three different DG technologies with Electromagnetic Transient Program (EMTP) indicate that we can maintain transient stability while the DG is protected against disturbances.

Aeroelastic Analysis of a Wing with Freeplay Considering Effects of Angle-of-Attack (받음각 효과를 고려한 유격이 있는 날개의 공탄성 해석)

  • Kim Jong-Yun;Yoo Jae-Han;Park Young-Keun;Lee In
    • Proceedings of the Computational Structural Engineering Institute Conference
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    • 2005.04a
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    • pp.295-300
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    • 2005
  • The freeplay, one of the concentrated structural nonlinearities, is inevitable for control surfaces of a real air vehicle due to normal wear of components and manufacturing mismatches. Also aerodynamic nonlinearities caused by a shock wave occur in transonic region. In practice, these nonlinearities induce the limit cycle oscillation (LCO) and decrease the transonic flutter speed. In this study, the fictitious mass method is used to apply a modal approach to nonlinear structural models due to freeplay. The transonic small-disturbance (TSD) equation is used to calculate unsteady aerodynamic forces in transonic region. Nonlinear aeroelastic time responses are predicted by the coupled time integration method (CTIM). This method was also applied to a 3D all-movable control wing to investigate its nonlinear aeroelastic responses. The angle of attack effect on the LCO characteristics has been found to be closely related with the initial pitching moment.

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The Development of Vibration Exciter Using Strain Displacement Estimator for Flow Resonance (스트레인 게이지 변위 추정기를 사용한 유동공진 가진기 개발)

  • Choi, Jae-hyuck;Nam, Yoon-su
    • Journal of Industrial Technology
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    • v.21 no.B
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    • pp.125-132
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    • 2001
  • Heat dissipation technology using flow resonant phenomenon is a kind of new concept in heat transfer area. A vibration exciter is needed to generate air turbulence which has the natural shedding frequency of heat system. A mechanical vibrating device for the air flow oscillation is introduced, which is driven by a moving coil actuator. An analytical dynamic model for this mechanical vibration exciter is presented and its' validity is verified by the comparison with experimental data. Values of some unknown system parameters in the analytic model are estimated through the system identification approach. Based on this mathematical model, the vibration exciter using strain displacement estimator is developed. And in the experiment, the feedback control is used. During the experimental verification phase, it turns out the high modal resonant characteristics of vibrating plate are the major barrier against obtaining a high bandwidth vibration exciter.

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Design and Evaluation of a Vibration Exciter for the Flow Resonance (유동공진을 위한 가진기 설계 및 평가)

  • Nam, Yoon-Su;Choi, Jae-Hyuck
    • Journal of the Korean Society for Precision Engineering
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    • v.18 no.6
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    • pp.141-147
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    • 2001
  • A heat dissipation technology using flow resonant phenomenon is a kind of new concept in heat transfer area. A vibration exciter is needed to generate an air turbulence which has the natural shedding frequency of a heat system. A mechanical vibrating device for the air flow oscillation is introduced, which is driven by a moving coil actuator. An analytical dynamic model for this mechanical vibration exciter is presented and its validity is verified by the comparison with experimental data. Values of some unko주 system parameters in the analytic model are estimated through the system identification approach. based on this mathematical model, a high bandwidth vibration exciter is designed using feedback control. During the experimental verification phased, it turns out the high frequency modal resonant characteristics of vibrating plate are the major barrier against obtaining a high bandwidth vibration exciter.

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Control of Ultrasonic Motor Using Two-Phase High Frequency Inverter (2상 고주파 인버터에 의한 초음파 모터 제어)

  • Heo, J.Y.;Cho, G.B.;Baek, H.L.;Oh, K.G.;Jeung, H.S.;Yu, K.J.
    • Proceedings of the KIEE Conference
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    • 1994.07a
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    • pp.462-464
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    • 1994
  • In this paper, noble electrical equivalent circuit ultrasonic motor is applied by model of parallel one from mechanical equation of piezoelectric device and characteristics estimation is done by equivalent converter. Uitrasonic motor is driven by oscillation circuit of two-phase high frequency inverter. Operating frequency of inverter is described by tracking control method of resonance frequency, according to change of load, temperature etc.

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A Study on Improving Characteristics in the Parallel Resonant DC Link Inverter (병렬공진형 직류 링크 인버터의 특성 개선에 관한 연구)

  • Beak, J.W.;Yoo, D.W.;Kim, J.S.;Lim, G.H.
    • Proceedings of the KIEE Conference
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    • 1994.07a
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    • pp.429-431
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    • 1994
  • A parallel resonant dc link inverter, one of the many resonant inverters, has some superior characteristics in camparision with other resonant inverters. But loss of the resonant oscillation and occurrence of high peak voltage in the resonant capacitor of these inverters are serious problems. In this paper, we investigate a control method for resonant dc link inverters which can overcome these problems. Experimental results are presented to show superior operation of the resonant dc link inverter using the proposed control method.

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A Stabilization Scheme of a Dynamic FOG Compass using the Fuzzy Control (퍼지제어에 의한 동적방식 광파이버 자이로콤파스의 구동시스템 안정화)

  • 권용수;김상우
    • Journal of the Korea Institute of Military Science and Technology
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    • v.2 no.1
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    • pp.150-158
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    • 1999
  • A driving system of a dynamic FOG compass with a stabilized platform is described. A stepping motor adopted as a driving motor is required to maintain a stable operation with constant speed and low oscillation for the proper operation of the FOG compass itself. The previous stabilization scheme operated on frequency-modulated supply is modified to include fuzzy control algorithm. The proposed scheme has advantages, particularly in the size, weight and flexibility of the driving system.

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MATHEMATICAL PHASE NOISE MODEL FOR A PHASE-LOCKED-LOOP

  • Limkumnerd, Sethapong;Eungdamrong, Duangrat
    • 제어로봇시스템학회:학술대회논문집
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    • 2005.06a
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    • pp.233-236
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    • 2005
  • Phase noise in a phase-locked-loop (PLL) is unwanted and unavoidable. It is a main concern in oscillation system especially PLL. The phase noise is derived in term of power spectrum density by using a reliable phase noise model. There are four noise sources being considered in this paper, which are generated by reference oscillator, voltage controlled oscillator, filter, and main divider. The major concern for this paper is the noise from the filter. Two types of second order low pass filter are used in the PLL system. Applying the mathematical phase noise model, the output noises are compared. The total noise from the passive filter is lower than the active filter at the offset frequency range between 1 Hz to 33 kHz.

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