• Title/Summary/Keyword: 2-자유도 시스템

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Performance Analyses of TDF $H_\infty$ Controllers for Uncertain Systems (불확실한 시스템에 대한 2-자유도 $H_\infty$ 제어기의 성능해석)

  • 강영중;이군석;권오규
    • 제어로봇시스템학회:학술대회논문집
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    • 1993.10a
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    • pp.477-481
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    • 1993
  • The aim of this paper is to analyze via computer simulation the robust performance of TDF(Two Degree of Freedom) H.$_{\infty}$ controller for uncertain systems having parameter uncertainty. We apply the TDF H$_{\infty}$ controller to autopilot design. We evaluate the robust performance of the TDF H$_{\infty}$ controller for uncertain systems and present the guaranteed bound of robust performance via computer simulation.on.

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극점 배치를 이용한 제어기 설계

  • Gang, Tae-Sam
    • ICROS
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    • v.21 no.2
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    • pp.47-51
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    • 2015
  • 극점은 제어시스템의 안정성, 수렴속도를 결정하는 중요한 요소이다. 본고에서는 출력 되먹임을 이용하여 임의의 원하는 극점을 배치하고, 또한 외란을 극복하면서 기준 명령을 추종할 수 있는 제어기를 설계하는 방법을 살펴 보았다. 이를 위해서는 기준 입력 또는 외란의 불안정한 극점들이 제어루프에 포함되도록 한다. 즉, 불안정한 극점들이 마치 플랜트에 첨가된 것처럼 간주하고 제어기를 설계하면 된다. 제어기 차수를 줄이기 위해서는 제어기 설계과정에서 남는 자유도를 이용하여 불안정한 극점들이 제어기에 포함되도록 하면 된다.

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Animation Support for Networked Virtual Environments (네트웍으로 연결된 가상환경을 위한 애니메이션 지원)

  • Ko, Hyeongseok;Lee, Ee-Taek;Jang, Ho-Wook
    • Journal of the Korea Computer Graphics Society
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    • v.2 no.2
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    • pp.29-36
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    • 1996
  • This paper presents animation techniques and issues involved in virtual environments where the participants interact with each other through a network. The state of the participant should be collected at each local site, and broadcasted to the other sites. Because information exchange is minimal, animation techniques are applied to convert the incoming low DOF parameters into high DOF joint angles that completely determine the configuration of the agents at each frame. As a case study, a software system VRLOCO is introduced, which has been developed by the author over the last five years.

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Robust 2 D.O.F. Controller for the Precesses with dead-time (시간지연을 갖는 프로세서의 견실한 2자유도 제어기)

  • 최주용;배종일;이만형
    • 제어로봇시스템학회:학술대회논문집
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    • 2000.10a
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    • pp.319-319
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    • 2000
  • In this paper, A dead-time compensator (DTC) for the processes with long dead-time is proposed. The processes which consist of dead-time, time-constant, gain are estimated by the linear least squares method in the frequency domain. A Smith predictor(SP) modified by including a filter becomes a two degree of freedom DTC. So the proposed DTC can yield the desirable setpoint and load disturbance responses separately. PI controller is used for the primary controller and the filter is tuned to be robust. Simulation examples demonstrate the properties of the proposed DTC.

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Investigating the Effect of Open Skies Policies (항공자유화의 추진이 미치는 영향에 대한 연구)

  • Park, Jin-Woo;Kim, Mi-Kyoung
    • The Journal of the Korea Contents Association
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    • v.9 no.2
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    • pp.350-358
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    • 2009
  • As open skies polices have permeated all over the world, Korea's basic direction of aviation policy is promoting the benefit of the public and the national carriers' competitive power by establishing open skies agreements between the countries. The open skies' directions should be promoted by considering the relationships of various attributes such as governments, airlines, and passengers. To decide the right directions of open skies, we should investigate the economic effects of open skies policies. This research develops a simulation model to analyze the dynamic characteristics of open skies. By using the developed model, this research analyzes the economic effects of open skies. The results showed that open skies have direct impacts on not only frequencies, airfare, consumer welfare but also air transport industry and regional economy. Therefore, it is necessary to take suitable aviation policy that can increase the effects of open skies.

Output feedback control for robot manipulator using variable structure control (위치만을 이용한 가변 구조 제어 방법에 의한 로봇 동작부 제어기 설계)

  • O, Seung-Rok
    • Journal of Institute of Control, Robotics and Systems
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    • v.3 no.6
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    • pp.569-575
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    • 1997
  • 모델 불확실성이 있고 n축 자유도(degree of freedom)를 갖고 있는 로봇 동작부(manipulator)에 대해서 위치 정보만을 이용하여 가변 구조 제어기(variable structure controller)를 설계하였다. 모델의 불확실성이 존재하는 경우에도 제어기에 사용되는 속도를 잘예측하기 위해 고이득 관찰기를 사용 하였으며 고이득 관찰기를 사용할때 발생할 수 있는 상태변수의 피킹현상(peak phenomenon)를 적게 하게 하기위하여 제어기의 값을 제한 (globally bounded)하여 제어기를 설계하였다. 부하(payload)의 범위만 알고 있는 2축 자유도를 갖는 로봇 동작부에 대해서 제안된 제어 방법에 따라 제어기를 설계하여 그 성능를 확인 하였다.

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Design of Beacon System for Estim ating 6DOF and Central Management Based on the Convolutional Neural Network in an augmented reality environment (증강현실 환경에서 합성곱 신경망 기반 6 자유도 자세 추정 및 중앙 관리가 가능한 비콘 시스템 설계)

  • An, Hyeon Woo;Cho, Jae Hyeon;Moon, Nammee
    • Proceedings of the Korean Society of Broadcast Engineers Conference
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    • 2018.06a
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    • pp.178-179
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    • 2018
  • 증강현실 환경에서 현실 세계의 물체를 포착하여 디지털화 시키는 것은 몰입감 향상에 있어 매우 중요한 기술이다. Faster R - CNN 은 영상에서 여러 물체를 인식하는 기술 중 하나이며, 지금껏 많은 응용 기술의 개발과 함께 많은 연구가 진행되고 있다. 본 논문은 증강현실 환경에서 평면물체의 2D 변환관계를 설명하는 Homography 와 Faster R - CNN 을 활용하여 여러 개의 비콘에 대한 6 자유도(6DOF) 를 추정하는 방법을 제안한다. 또한 증강현실에서 주로 사용되는 마커 기술에 존재하는 단점들을 극복할 수 있는 비콘 구조를 소개하고 여러 개의 비콘을 용이하게 관리하는 시스템을 제안한다.

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Parameter Estimation of 2-DOF System Based on Unscented Kalman Filter (UKF 기반 2-자유도 진자 시스템의 파라미터 추정)

  • Seung, Ji-Hoon;Kim, Tae-Yeong;Atiya, Amir;Parlos, Alexander;Chong, Kil-To
    • Journal of the Korean Society for Precision Engineering
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    • v.29 no.10
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    • pp.1128-1136
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    • 2012
  • In this paper, the states and parameters in a dynamic system are estimated by applying an Unscented Kalman Filter (UKF). The UKF is widely used in various fields such as sensor fusion, trajectory estimation, and learning of Neural Network weights. These estimations are necessary and important in determining the stability of a mobile system, monitoring, and predictions. However, conventional approaches are difficult to estimate based on the experimental data, due to properties of non-linearity and measurement noises. Therefore, in this paper, UKF is applied in estimating the states and parameters needed. An experimental dynamic system has been set up for obtaining data and the experimental data is collected for parameter estimation. The measurement noises are primarily reduced by applying the Low Pass Filter (LPF). Given the simulation results, the estimated error rate is 39 percent more efficient than the results obtained using the Least Square Method (LSM). Secondly, the estimated parameters have an average convergence period of four seconds.

Integrated Design of Feed Drive Systems Using Discrete 2-D.O.F. Controllers (I) - Modeling and Performance Analysis - (이산형 2자유도 제어기를 이용한 이송계의 통합설계 (I) -모델링 및 성능해석-)

  • Kim, Min-Seok;Chung, Sung-Chong
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.28 no.7
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    • pp.1029-1037
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    • 2004
  • High-speed/precision servomechanisms have been widely used in the manufacturing and semiconductor industries. In order to ensure the required high-speed and high-precision specifications in servomechanisms, an integrated design methodology is required, where the interactions between mechanical and electrical subsystems will have to be considered simultaneously. For the first step of the integrated design process, it is necessary to obtain not only strict mathematical models of separate subsystems but also formulation of an integrated design problem. A two-degree-of-freedom controller described in the discrete-time domain is considered as an electrical subsystem in this paper. An accurate identification process of the mechanical subsystem is conducted to verify the obtained mathematical model. Mechanical and electrical constraints render the integrated design problem accurate. Analysis of the system performance according to design and operating parameters is conducted for better understanding of the dynamic behavior and interactions of the servomechanism. Experiments are performed to verify the validity of the integrated design problem in the x-Y positioning system.

Wing Optimization based on a Reduced System (축소시스템 기반 비행체 날개 최적화 연구)

  • Kim, Hyun-Gi;Choi, In-Ho
    • Journal of the Korea Academia-Industrial cooperation Society
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    • v.13 no.10
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    • pp.4411-4417
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    • 2012
  • The present study proposes the optimization of wing structure base on reduced model which assures the solution accuracy and computational efficiency. Well-constructed reduced model assures the accurate result in the eigenvalue problem, dynamic analysis or sensitivity of design optimization. Reduced system is classified into the reduce-order model based on structural modes and the reduced system based on degrees of freedom. Because this study uses the reduced system based on degrees of freedom, it is important to select the dominant degrees of freedom properly. For this work, robust selection method, two-level selection scheme, is employed and IRS(Improved Reduced System) is applied to construct the final reduced system. In the optimization process based on the reduced system, all of the equivalent stress, eigenvalue and design sensitivities are calculated from the reduced system. Through a numerical example, it is shown that the present optimization methodology based on the reduction method can provide an optimal results for objective function satisfying constraint condition.