• Title/Summary/Keyword: PID control gain

검색결과 270건 처리시간 0.023초

CONTROL PERFORMANCE IMPROVEMENT OF AN EMV SYSTEM USING A PM/EM HYBRID ACTUATOR

  • Ahn, H.J.;Chang, J.U.;Han, D.C.
    • International Journal of Automotive Technology
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    • 제8권4호
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    • pp.429-436
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    • 2007
  • In this study, we improved control performance of an EMV (electromechanical valve) system using a PM/EM (permanent magnet/electromagnet) hybrid EMA (electromagnetic actuator) and showed the feasibilities of both soft landing and fast transition of the EMV system using a simple PID control. The conventional EMV systems using only EM show significant nonlinear characteristics. Therefore, it is very difficult to control the valve position and several complex control schemes are used. This paper focused on the control performance improvement using a PM/EM hybrid actuator. In particular, a PM is used as a key design parameter such as a bias current of a magnetic bearing in order to improve the linear characteristic of the actuator, although most PM/EM hybrid actuators use a PM as a power saver during valve-open and -closed states. First, a FE (finite element) analysis was performed to confirm its linear static force characteristics. Then, both a test rig and a valve control system were built in order to prove experimentally the control performance improvement of the actuator. Finally, feasibilities of both soft landing and fast transition of the system were shown experimentally through gain-scheduled PID (proportional derivative integral) control.

바람센서가 없는 무추력 비행체의 활공 시 대기속도 추정을 통한 유도성능 향상 (Optimization of Glide Performance using Wind Estimator for Unpowerd Air Vehicle without Pitot-Tube)

  • 김부민;진재현;박정호;김병수
    • 제어로봇시스템학회논문지
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    • 제15권1호
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    • pp.1-7
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    • 2009
  • As designing PID control on aircraft, we consider a gain scheduling on altitude and velocity. If pitot tube is not installed in the unpowered air vehicle, the control performance is reduced by the difference between ground speed and air speed with a wind considered. In this paper, a simple guidance controller (LOS: Line of Sight) and the wind estimator using Kalman filter are designed. And we minimize the wind effect through the estimator. Finally, we perform the 6-DOF nonlinear simulation with the wind model to verify the performance of the controller with the wind estimator.

초정밀 스테이지 설계 및 제어 시스템에 관한 연구 (A study of the design and control system for the ultra-precision stage)

  • 박종성;정규원
    • 한국공작기계학회:학술대회논문집
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    • 한국공작기계학회 2005년도 춘계학술대회 논문집
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    • pp.54-59
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    • 2005
  • Recently, the ultra-precision stage is widely used in the fields of the nano-technology, specially in AFMs(Atomic Force Microscope) and STMs(Scanning Tunneling Microscope). In this paper, the ultra-precision stage which consists of flexure hinges, piezoelectric actuator, and ultra-precision linear encoder, is designed and developed. The guide mechanism which consisted of flexure hinges is analyzed by Finite Element Method. And we derived the transfer function of the system in 1st order system from step responses according to the magnitude. We performed simulation for the model to tune the control gain and applied the gains to the developed system. Experimental results found that the stage can be controlled in 5 nm resolution by PID controller.

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Design and experiment of fuzzy PID yaw rate controller for an electrically driven four wheel vehicle without steering mechanism

  • I, H
    • 한국지능시스템학회논문지
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    • 제9권5호
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    • pp.480-489
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    • 1999
  • Design and experimental results of yaw rate controller is described for electricallydriven four wheel vehicle without steering mechanism. Yaw rate controller has been known to be necessary to cope with nonlinear char-acteristics of the wheel/road conditions with respect to different road condition and steering angle. For an effective yaw rate control, a fuzzy PID gain scheduler is considered with changing control parameters. In order to apply proposed algorithm to the system a downsized four wheel drive electrically driven vehicle without steering mechanism was manufactured. With these techniques the proposed yaw rate controller is shown by experiment results to be obtained suficient performance in the whole steering regions.

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전자(電子) 팽창밸브를 이용(利用)한 증발기(蒸發器)의 냉매(冷媒) 流量(유량) 제어(制御) 및 과열도(過熱度) 특성(特性)에 관한 연구(硏究) (Study on Control of Refrigerant Flow Rate and Characteristics of Superheat in Evaporator using Electronic Expansion Valve)

  • 최순오;김정훈;양현석;김종수
    • 설비공학논문집
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    • 제6권4호
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    • pp.380-387
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    • 1994
  • An experimental study was performed to investigate the characteristics of refrigerant flow rate control and superheat in an evaporator with an electronic expansion valve(EEV). The EEV used in this study was devised using a needle valve coupled with a stepping motor controlled by a personal computer. A Pill control equation was used to control the superheat of the evaporator and to set the superheat to $5^{\circ}C$. In order to determine an optimum running condition for the system, Pill parameters were varied for the wide range of values. The running condition of an air conditioning system with a PI control was reasonably stable compared with that of the Pill control. Experimental results for the PI control using parameter values, $K_p=1.5$, $T_i=400(sec)$ and $T_s=6(sec)$ show that the superheat reached its target value. When external disturbances were introduced to the system, the superheat target value was reached within about 3 minutes. When the EEV was applied to the air conditioning system driven by an inverter, room temperature control was excellent.

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기계학습 알고리즘을 이용한 UAS 제어계수 실시간 자동 조정 시스템 (UAS Automatic Control Parameter Tuning System using Machine Learning Module)

  • 문미선;송강;송동호
    • 한국항행학회논문지
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    • 제14권6호
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    • pp.874-881
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    • 2010
  • 무인기의 자동 비행 제어 시스템은 기체의 형태, 크기, 무게 등의 정적 및 동적 변화에 따라 스스로 비행계수를 조정하여 목표 비행궤적을 정확히 따라가도록 제어할 필요가 있다. 본 논문에서는 PID 제어 기법을 이용하는 비행제어시스템에 기계학습모듈(MLM)을 추가하여 기체의 특성 변화에 따라 제어계수를 비행중 실시간 자동으로 조정하는 시스템을 제안한다. MLM은 선형회귀분석과 보정학습을 이용하여 설계되었으며 MLM을 통해 학습된 제어계수의 적합성을 평가하는 평가모듈(EvM)을 함께 모델링 하였다. 이 시스템은 FDC 비버 시뮬레이터를 기반으로 실험하였으며 그 결과를 분석 제시하였다.

두 개의 거리 센서를 이용한 차륜형 로봇의 이동물체 추종제어 (Moving Object Following Control for Differential Drive Robot Based on Two Distance Sensors)

  • 서동진;노성우;고낙용
    • 한국전자통신학회논문지
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    • 제6권5호
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    • pp.765-773
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    • 2011
  • 본 논문에서는 거리센서기반의 차륜형 로봇의 물체추적과 추종에 대한 로봇의 구동제어방법을 제안한다. 물체 추종을 위해 1개의 초음파 송신부와 2개의 초음파 수신부를 사용하여 추종하고자 하는 물체로부터 2개의 거리데이터를 생성한다. 생성된 거리데이터를 기반으로 로봇의 물체까지의 직진오차와, 회전오차를 산출한 뒤, 물체 추종을 위해 PID제어기 기반의 조작량을 계산하여 로봇의 동작제어에 사용한다. 제안된 방법의 특징을 확인하기 위해 3가지 경우에서 실험을 수행하였으며 PID게인이 로봇의 움직임에 미치는 영향과 직진오차게인과 회전오차게인이 로봇의 움직임에 미치는 영향을 각각 확인해 보았다. 제안된 방법은 항상 추종물체를 로봇에 대하여 일정위치에 존재하도록 하는 기법으로 물체추종 어플리케이션 이외에도, 여러 대의 로봇이 특정한 대형을 이루어 움직이게 하는 군집형 제어 문제에 적용될 수 있다.

드릴쉽에 대한 DPS 모형시험 기법개발 (An Experimental Method of Model Installed Dynamic Positioning System for Drillship)

  • 이동연;하문근
    • 대한조선학회논문집
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    • 제38권2호
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    • pp.33-43
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    • 2001
  • 드릴쉽과 셔틀탱커등 특수선의 건조가 활발해지면서 정해진 위치에서 장시간 작업해야 할 목적으로 동적 자기위치 유지시스템(Dynamic Positioning System)을 장착하는 선박이 늘어나고 있다. 본 논문에서는 DP 시스템의 구성 요소를 소개하고, 수조에서 실험한 결과를 바탕으로 제어이론과 필터이론에 따른 DP성능을 비교하였다. 실험에 사용한 선박은 10만톤급 드릴쉽으로 모델의 길이가 4m이며, 방향이 고정된 3개의 추진기를 사용하였다. 실험 내용은 명령에 따라 주어진 궤적을 이동하는 능력과 파도가 있는 외란조건에서 원하는 선수각을 유지할 수 있는지를 살펴보았다. 추진력을 구하기 위하여 PID 이론을 적용하였고, 제어게인의 변화에 따른 제어특성을 살펴보았다. 선형운동성분과 계측잡음을 제거하기 위하여 칼만 필터와 디지털 필터를 적용하였고, 각각의 필터성능을 비교 검토하였다.

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광디스크 드라이브 시스템을 위한 비선형 Anti-shock 제어기 설계 (Anti-shock Controller Design for Optical Disk Drive Systems with a Nonlinear Controller)

  • 백종식;정정주
    • 제어로봇시스템학회논문지
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    • 제11권9호
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    • pp.741-749
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    • 2005
  • This paper presents a nonlinear controller design for optical disk drive systems to improve anti-shock performance. The nonlinear anti-shock controller is added parallel to the original linear servo control loop. In the previous work, a dead-zone nonlinear element is used for the nonlinear controller and a PID control method is used for the linear controller. Although this parallel structure of the controller improves anti-shock performance, it has a narrow stability bound. In this paper, the dead-zone with saturation nonlinear element is proposed for the nonlinear controller. Since this nonlinear element improves stability margin, we can use higher slope gain of dead-zone than that of nonlinear controller using dead-zone only. In the linear controller design, it is shown that the lead-lag control has an improved stability margin over PID control. Numerical simulation results and experimental results show that the proposed method can get better performance to the external shock than previously proposed methods.

유가식 생물반응기에서의 용존산소농도 및 비성장속도의 제어 (Control of dissolved Oxygen Concentration and Specific Growth Rate in Fed-batch Fermentation)

  • 김창겸;이태호;이승철;장용근;장호남
    • 한국미생물·생명공학회지
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    • 제21권4호
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    • pp.354-365
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    • 1993
  • A novel control method with automatic tuning of PID controller parameters has been developed for efficient regulation of dissolved oxygen concentration in fed-batch fermentations of Escherichia coli. Agitation speed and oxygen partial pressure in the inlet gas stream were chosen to be the manipulated variables. A heuristic reasoning allowed improved tuning decisions from the supervision of control performance indices and it coule obviate the needs for process assumptions or disturbance patterns. The control input consisted of feedback and feedforword parts. The feedback part was determined by PID control and the feedforward part is determined from the feed rate. The proportional gain was updated on-line by a set of heuristics rules based on the supervision of three performance indices. These indices were output error covariance, the average value of output error, and input covariance, which were calculated on-line using a moving window. The integral and derivative time constants were determined from the period of output response. The specific growth rate was maintained at a low level to avoid acetic acid accumulation and thus to achieve a high cell density. The specific growthe rate was estimated from the carbon dioxide evolution rate. In fed-batch fermentation, the simutaneous control of dissolved oxygen concentration (at 0.2; fraction of saturated value) and specific growth rate (at 0.25$hr^{-1}$) was satisfactory for the entire culture period in spite of the changes in the feed rate and the switching of control input.

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