• Title/Summary/Keyword: 극점 배치법

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Design af a Flight Controller Using Parameter Space Graph Method (제어상수 영역 그래프 법을 이용한 비행제어기 설계)

  • 정익상;곽병철;박양배
    • 제어로봇시스템학회:학술대회논문집
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    • 1986.10a
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    • pp.266-268
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    • 1986
  • 최근에 측정할 수 있는 상태만을 피드백하여 시스템의 극점을 의도한 영역에 배치하는 상수들의 영역을 찾아내는 방법이 제시되었고, 비행체의 제어에 적용한 결과가 발표되었다. 이 방법은 근궤적법과 극점배치법의 단점을 상호 보완하며 견실성(Robustness)에 대한 판단을 용이하게 할 뿐 아니라 컴퓨터를 사용하여 쉽게 설계에 이용될 수 있는 장점이 있다. 그러나 S 평면상에 배치되는 각각의 극점쌍의 위치를 제어 상수들의 조합으로 부터 유추해내기 어렵고, 중요하지 않은 극점이 의도하는 영역밖에 있는 경우에는 적용하는데 난점이 있었다. 본 논문에서는 이 방법을 확장하여 S 평면상에 배치되는 복소극점쌍의 위치를 제어상수 평면에서 간단하게 유추할 수 있고, 이득여유 위상여유를 동시에 고려할 수 있는 제어상수 영역 그래프법을 제시하고 노드롭(Northrop) 항공사의 시험용 비행기를 대상으로 하여 종방향운동 제어기의 설계 예를 보인다.

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Vibration-free Control of Double Integrator Typed Motor via Loop Transfer Recovery (루프 전달 회복을 통한 이중 적분 모터의 무진동 제어)

  • Suh, Sang-Min
    • Transactions of the Korean Society for Noise and Vibration Engineering
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    • v.20 no.10
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    • pp.900-906
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    • 2010
  • This note proposes vibration-free motor control through modified LQG/LTR methodology. A conventional LQG/LTR method is a design tool in the frequency domain. However, unlike the conventional one, the proposed one is a time response based design method. This feature is firstly designed by parameterized settling time control gain through the target loop design procedure and the feature is secondly realized by loop transfer recovery. In order to show convergence to the target loop transfer functions, asymptotic behaviors of the open and the closed loop transfer functions are shown. At the conclusion, it is verified that the proposed method is robustly stable to parametric uncertainties through ${\mu}$-plot.

A Study on the efficient control of an elastic manipulator moving in a vertical plane (수직면에서 작동하는 탄성 매니퓰레이터의 효율적인 제어에 관한 연구)

  • 강준원;이중섭;권혁조;오재윤;정재욱
    • Proceedings of the Korean Society of Precision Engineering Conference
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    • 1996.11a
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    • pp.318-322
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    • 1996
  • This paper presents a technique to control a robot which has a flexible manipulator moving in a vertical plane. The flexible manipulator is modeled as an Euler-Bernoulli beam. Elastic deformation is represented using the assumed modes method. A comparison function which satisfies all geometric and natural boundary conditions of a cantilever beam with an end mass is used as an assumed mode shape. Lagrange's equation is utilized for the development of a discretized model. A control algorithm is developed using a simple PID control technique. The proportional, integral and derivative control gains are determined based on the dominant pole placement method and tuned to show no overshoot and having a short settling time. The effectiveness of the developed control scheme is showed experimentally. In the position control experiment, three different end masses are used. The experimental results shows little overshoot, no steady state error, and less than 2.5 second settling time in case of having an end mass which is equivalent to 45% of the total system weight. Also the residual vibration of the end point is effectively controlled.

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PID Control of a flexible robot rotating in vertical plane (수직면에서 회전운동을 하는 탄성로봇의 PID 제어)

  • Kang, Junwon;Oh, Chaeyoun;Kim, Kiho
    • Journal of the Korean Society for Precision Engineering
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    • v.14 no.11
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    • pp.34-41
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    • 1997
  • This paper presents a technique to control a very flexible robot moving in a vertical plane. The flexible robot is modeled as an Euler-Bernoulli beam. Elastic deformation is approximated using the assmed modes method. A comparison function which satisfies all geometric and natural boundary conditions of a cantilever beam with an end mass is used as an assumed mode shape. Lagrange's equation is utilized for the development of a discretized model. A control algorithm is developed using a simple PID cnotrol tech- nique. The proportional, integral and deivative control gains are determined based on the dominant pole placement method and tuned to show no overshoot and no steady state error, and short settling time. The effectiveness of the developed control scheme is showed in the hub angular diaplacement control experiment. Three different end masses are uned in the experiment. The experimental results show that developed control algorithm is very effective showing little overshoot, no steady state error, and less than 2.5 second settl- ing time in case of having an end mass which is equivalent to 45% of the manipulator mass. Also the experimental results show that the residual vibration fo the end point is effectively controlled.

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