• 제목/요약/키워드: External disturbance

검색결과 405건 처리시간 0.028초

공동을 고려한 원주방향 급유홈 저널 베어링의 비선형 진동 해석 (Nonlinear Frequency Response Analysis of Circumferentially Grooved Journal Bearing Considering Cavitation)

  • 노병후;김경웅
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 1999년도 제30회 추계학술대회
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    • pp.160-166
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    • 1999
  • Nonlinear characteristics of the hydrodynamic journal bearing with circumferentially groove are analyzed numerically considering cavitation region, when an external sinusoidal shock is given to the system. The oil film force is obtained by solving the finite width universal Reynolds equation at each time step. Frequency response function and journal orbit obtained from both linear and nonlinear bearing simulations are compared with each other. The vibration response of the journal is different from the expectation obtained from the linear analysis as increase the vibration amplitude of external disturbance. Therefore, the linear theory is not adequate, and the nonlinear calculation such as used in this research is needed to design safety rotor systems.

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비선형 비행 시스템을 위한 H 접근법 기반 적응 신경망 동적 표면 제어 (Adaptive Neural Dynamic Surface Control via H Approach for Nonlinear Flight Systems)

  • 유성진;최윤호
    • 제어로봇시스템학회논문지
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    • 제14권3호
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    • pp.254-262
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    • 2008
  • In this paper, we propose an adaptive neural dynamic surface control (DSC) approach with $H_{\infty}$ tracking performance for full dynamics of nonlinear flight systems. It is assumed that the model uncertainties such as structured and unstrutured uncertainties, and external disturbances influence the nonlinear aircraft model. In our control system, self recurrent wavelet neural networks (SRWNNs) are used to compensate the model uncertainties of nonlinear flight systems, and an adaptive DSC technique is extended for the disturbance attenuation of nonlinear flight systems. All weights of SRWNNs are trained on-line by the smooth projection algorithm. From Lyapunov stability theorem, it is shown that $H_{\infty}$ performance nom external disturbances can be obtained. Finally, we present the simulation results for a nonlinear six-degree-of-freedom F-16 aircraft model to confirm the effectiveness of the proposed control system.

Adaptive Control of a Single Rod Hydraulic Cylinder - Load System under Unknown Nonlinear Friction

  • Lee Myeong-Ho;Park Hyung-Bae
    • Journal of Advanced Marine Engineering and Technology
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    • 제29권3호
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    • pp.251-259
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    • 2005
  • A discrete time model reference adaptive control has been applied in order to compensate the nonlinear friction characteristics in a hydraulic proportional position control system. As nonlinear friction, static and coulomb friction forces are considered and modeled as dead zone and external disturbance respectively. The model reference adaptive control system consists of a cascade combination of the dead zone. external disturbance and linear dynamic block. For adaptive control experiment. the DSP(Digital Signal Processor) board has been interfaced the hydraulic proportional position control system. The experimental results show that the MRAC(Model Reference Adaptive Control) for compensation of static and coulomb friction are very effective.

슬라이딩 모드 제어를 이용한 3축 안정화 위성의 자세 제어및 강건성 해석 (Robust attitude control and analysis for 3-axis stabilized spacecraft using sliding mode control)

  • 신동준;김진호
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1997년도 한국자동제어학술회의논문집; 한국전력공사 서울연수원; 17-18 Oct. 1997
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    • pp.692-695
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    • 1997
  • Nonlinear robust attitude controller for 3-axis stabilized spacecraft is designed. Robust stability analysis for nonlinear spacecraft system with disturbance is conducted. External disturbances and parametric uncertainties decrease Spacecraft's attitude pointing accuracy. Sliding Mode Control(SMC) provides stability of system in the face of these disturbances and uncertainties. The concept of quadratic boundedness and quadratic stability are applied to the robust analysis for the nonlinear spacecraft system subject to bounded disturbance torques. Numerical simulation is conducted to compare the analysis result and actual nonlinear simulation. The simulation show that analysis result is valid.

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고전류밀도 초전도선의 안전성 (Stability of a high current density superconducting wire)

  • 김대선;류경우;최병주
    • 한국초전도저온공학회:학술대회논문집
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    • 한국초전도저온공학회 1999년도 제1회 학술대회논문집(KIASC 1st conference 99)
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    • pp.61-64
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    • 1999
  • Dry winding is generally adopted in superconducting coils of an UPS system. In these kinds of coils a quench is often initiated by a disturbance such as wire motion that generates a highly localized normal zone in a superconducting wire. To fabricate the stable coils, stability of the superconducting wire should be touched. In this paper, a model for a transient stability analysis of the wire is suggested. The influence of a local disturbance, cooling, an external field and a stabilizer to superconductor ratio on the wire stability is investigated and discussed.

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Quantitative Feedback Theory를 이용한 능동 자기베어링의 적용 연구 (A Study for Application of Active Magnetic Bearing using Quantitative Feedback Theory)

  • 이관열;이형복;김영배
    • 한국정밀공학회지
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    • 제18권11호
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    • pp.107-115
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    • 2001
  • Most of rotating machineries supported by contact bearing accompany lowering efficiency, vibration and wear. Moreover, because of vibration, which is occurred in rotating shaft, they have the limits of driving speed and precision. The rotor system has parametric variations or external disturbances such as mass unbalance variations in long operation. Therefore, it is necessary to research about magnetic bearing, which is able to support the shaft without mechanical contact and to control rotor vibration without being affected by external disturbances or parametric changes. Magnetic bearing system in the paper is composed of position sensor, digital controller, actuating amplifier and electromagnet. This paper applied the robust control method using quantitative feedback theory (QFT) to control the magnetic bearing. It also proposed design skill of optimal controller, in case the system has structured uncertainty, unstructured uncertainty and disturbance. Reduction of vibration is verified at critical rotating speed even external disturbance exists. Unbalance response, a serious problem in rotating machinery, is improved by magnetic bearing using QFT algorithm.

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외란을 갖는 전기유압 서보시스템의 위치제어 (Position Control of an Electro-hydraulic Servo System with Disturbance)

  • 허준영
    • 드라이브 ㆍ 컨트롤
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    • 제18권3호
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    • pp.1-7
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    • 2021
  • In a hydraulic control system, since a hydraulic cylinder drives a relatively large mass of an object, an external load force acts as a disturbance on the control performance of the system. Additionally, as the hydraulic system is used for a long period, there are disturbances that occur gradually, such as a drop in supply pressure because of abrasion of the pump, oil leakage from a valve, and oil leakage from a cylinder. In this study, a state feedback controller based on a linearization technique is applied. To prevent the performance degradation of the controller from the load disturbance, an Extended Luenberger observer (ELO) is used for the Extended system. The case of using the proportional controller, which is a representative linear controller, and the result of using the controller designed in this study are compared and reviewed through simulation. Also, we propose an experimental gain-setting method for a state feedback controller that can be used at industrial sites, and examine how the stability and control performance of the system changes because of the disturbance inputs through the experimental results.

교란성분 모델링이 IMMU기반 자세추정 정확성에 미치는 영향 (Effect of Disturbance Modeling on IMMU-Based Orientation Estimation Accuracy)

  • 최미진;이정근
    • 대한기계학회논문집A
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    • 제41권8호
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    • pp.783-789
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    • 2017
  • 9축 IMMU기반의 3차원 자세추정에 있어 대표적인 정확성 저하요인은 가속도계 신호를 교란시키는 외부가속도와 지자기센서 신호와 관련된 자기교란이라는 두 가지 교란성분이다. 교란성분에 의한 영향을 최소화하기 위해 모델링기반 기법과 스위칭 기법이 제안되어 왔고, 이를 비교한 연구도 진행된 바 있다. 그러나 모델링기반 기법에서 모델링의 차이가 자세추정 성능에 미치는 영향에 대한 연구는 현재까지 발표된 바 없다. 본 논문은 교란성분 모델링이 IMMU기반 자세추정 정확성에 미치는 영향을 확인하기 위해, 모델링에 차이가 있는 최근 발표된 두 알고리즘을 다양한 시험조건에서 비교하였다. 이를 통해 교란성분 모델링의 차이는 진행잡음 공분산 행렬에 차이를 발생시키며, 이로 인해 자세추정 성능에 영향을 끼칠 수 있음을 확인할 수 있었다. 시험결과 두 알고리즘은 평균제곱근오차에서 롤 피치 요평균 $1.35^{\circ}$ 및 요성분 $3.63^{\circ}$의 차이를 발생시켰다.

비선형 성분을 외한으로 간주했을때의 매니퓰레이터의 슬라이딩 모드제어 (Sliding mode control of manipulator whose nonlinear components are regarded as external disturbance)

  • 이민철
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1991년도 한국자동제어학술회의논문집(국내학술편); KOEX, Seoul; 22-24 Oct. 1991
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    • pp.286-291
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    • 1991
  • This paper discusses sliding made control of robot manipurators assuming that nonlinear terms, which are inertia term, Coriolis force term and centrifugal taffn, are external disturbances. We obtained the unknown parameter of its linear terms by Signal Compression Method. We propose a new control input algorithm to decrease chattering in the application of sliding mode control of manipulator whose nonlinear components are regarded as disturbances. In this experiments, we used DSP(Digital Signal Processor) controller to suppress chattering by obtaining a quick switching speed.

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