• 제목/요약/키워드: Eigenstructure

검색결과 80건 처리시간 0.033초

병렬형 역진자 시스템 제작 및 분리제어 (Implementation of a Parallel Inverted Pendulum System with Decoupling Control)

  • 김주호;박운식;최재원
    • 한국정밀공학회지
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    • 제17권7호
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    • pp.162-169
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    • 2000
  • In this paper, we develop a parallel inverted pendulum system that has the characteristics of the strongly coupled dynamics of motion by an elastic spring, the time-variant system parameters, and inherent instability, and so on. Hence, it is possible to approximate some kinds of a physical system into this representative system and to apply the various control theories to this system in order to verie their fidelity and efficiency. For this purpose, an experimental system of the parallel inverted pendulum has been implemented, and a control scheme using the eigenstructure assignment for decoupling control is presented in comparison with the conventional LQR optimal control method. Furthermore, this system can be utilized as a testbed to develop and evaluate new control algorithms through various setups. Finally, in this paper, the results of the experiment are compared with those of numerical simulations for validation.

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ATM LAN 시스템에 위한 NEXT 억제 (NEXT Suppression for ATM LAN System)

  • 원희철;임기홍
    • 한국통신학회논문지
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    • 제25권11A호
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    • pp.1699-1708
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    • 2000
  • 본 논문은 ATM LAN 시스템의 NEXT(near-end crosstalk) 억제에 관한 연구로서, cyclostationary 근단 누화신혼(NEXT)가 존재하는 경우, NEXT 억제를 수행하는 PS-FSE (phase-splitting fractionally spaced equalizer)의 수렴 동작과 성능에 대하여 분석한다. 전체 수렴 속도와 수렴 후 성능은 신호와 근단 누화 신호와의 상대적 클락 페이즈(relative clock phase)에 따라 다르게 나타나고, 이러한 현상은 PS-FSE의 eigenstructure를 통해 설명할수 있다. Cyclostationary 근단 누화 신호과 존재하는 경우 PS-FSE는 stationary 잡음의경우와 다른 eigenstructure를 가진다. PS-FSE의 전체 수렴 속도는 근단 누화 신호 전력 스펙트럼에서 신호와 근단 누화 신호간의 cross 전력 스펙트럼을 뺀 값으로 구해지는 eigenvalue 값에 의해 결정되고, 따라서 신호와 근단 누화 신호간의 correlation에 의해 전체 수렴 속도가 좌우된다.

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[ $H_2$ ]-optimal Control with Regional Pole Assignment via State Feedback

  • Wang Guo-Sheng;Liang Bing;Duan Guang-Ren
    • International Journal of Control, Automation, and Systems
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    • 제4권5호
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    • pp.653-659
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    • 2006
  • The design of $H_2$-optimal control with regional pole assignment via state feedback in linear time-invariant systems is investigated. The aim is to find a state feedback controller such that the closed-loop system has the desired eigenvalues lying in some desired stable regions and attenuates the disturbance between the output vector and the disturbance vector. Based on a proposed result of parametric eigenstructure assignment via state feedback in linear systems, the considered $H_2$-optimal control problem is changed into a minimization problem with certain constraints, and a simple and effective algorithm is proposed for this considered problem. A numerical example and its simulation results show the simplicity and effectiveness of this proposed algorithm.

LQR 특성을 갖는 고유구조 지정 제어기법 및 자동차 능동 현가장치 제어에의 응용 (Eigenstructure Assignment Methodology with LQR Characteristics and Application to an Automotive Active Suspension Control)

  • 최재원;서영봉;유완석
    • 한국정밀공학회지
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    • 제15권11호
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    • pp.108-120
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    • 1998
  • In this paper, a new control system design algorithm, which has the advantages of the existing LQR and eigenstrcture assignment methods, is proposed. The method of the transformation matrix via block controller is utilized to develop the scheme. Using the proposed algorithm, LQR weighting matrices q and R, which satisfy the desired closed-loop eigenvalues and eigenvectors, can be achieved using only simple matrix computations. The usefulness of the proposed scheme is verified by applying to a numerical example and an automotive active suspension control system design.

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Robust Fault Detection Based on Aero Engine LPV Model

  • Linfeng, Gou;Xin, Wang;Liang, Chen
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.35-38
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    • 2008
  • This paper develops an aero engine LPV mathematical model to exactly describe aero engine dynamic process characteristics, eliminate the effect of modeling error. Design FDF with eigenstructure assignment. The simulation results of turbofan engine control system sensor fault show that this method has good performance in focusing discrimination in fault signal with modeling eror, enhancing the robustness to unknown input, detecting accuracy is high and satisfiying real-time requirement.

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비행제어계에 대한 고유구조 할당의 응용 (The application of eigenstructure assignment to flight control system)

  • 박노웅;박정일;박종국
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1988년도 한국자동제어학술회의논문집(국내학술편); 한국전력공사연수원, 서울; 21-22 Oct. 1988
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    • pp.603-607
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    • 1988
  • On this paper, the application of Eiganstructure assignment to flight control system design is presents. Both output feedback and constrained output feedback are considered. The computer implimentation of the algorithm is discussed including the utilization of real arithmetic for complex conjugate eigenvalue. And the example include a stability augementation system, an autopilot decoupled mode control.

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지정된 고유구조를 갖는 선형 시불변 다입출력 시스템의 PID조정기의 설계 (Design of PID regulator for linear time invariant MIMO system with prescribed eigenstructure)

  • 손승걸;전기준
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1986년도 한국자동제어학술회의논문집; 한국과학기술대학, 충남; 17-18 Oct. 1986
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    • pp.86-89
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    • 1986
  • This paper presents a design methodology for a PID regulator. The parameters of the PID regulator are determined through equivalent structure to the closed-loop system whose feedback gain assigns prescribed eigenvalues of the closed-loop system and minimizes a given performance index.

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비 대각요소를 이용한 부공간에서의 적응 빔 형성 기법 (Subspace-Based Adaptive Beamforming with Off-Diagonal Elements)

  • 최양호;엄재혁
    • 한국통신학회논문지
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    • 제29권1A호
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    • pp.84-92
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    • 2004
  • 공분산 행렬의 고유구조에 기초한 뎀 형성 방법은 수렴속도가 빠르고 도래각 추정 오차에 둔감한 이점을 가지고 있다 그러나 Sl (signal Plus interference) 부공간에 대한 기저(basis)를 추정하기 위해 표본 행렬을 고유분해 하는 것을 필요로 하여 그 계산이 매우 복잡하다. 본 논문에서는 표본행렬의 비 대각 요소를 이용하여 턱 공간을 추정하는 간단한 빔 형성 기법을 제안한다. 제안한 방법에서는 중첩된 부어레이들의 빔을 결합하여 최종 적응 출력을 얻는다. 이와 같이 부어레이를 결합하면 하나의 부어레이를 이용하는 경우에 비해 SINR (signal-to-interference-plus-noise ratio) 성능을 증가시킬 수 있다. 고유분해에 의한 방법은 원가는 신호의 도래각, 신호 수 모두에 오차가 있으면 심하게 성능이 저하되지만, 비 대각방법에서는 효율적인 도래각 추정기법을 적용하여 이러한 오차에 매우 둔감하다.

Lateral Vehicle Control Based on Active Flight Control Technology

  • Seo Young-Bong;Choi Jae-Weon;Duan Guang Ren
    • Journal of Mechanical Science and Technology
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    • 제20권7호
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    • pp.981-992
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    • 2006
  • In this paper, a lateral vehicle control using the concept of control configured vehicle (CCV) is presented. The control objectives for the lateral dynamics of a vehicle include the ability to follow a chosen variable without significant motion change in other specified variables. The analysis techniques for decoupling of the aircraft motions are utilized to develop vehicle lateral control with advanced mode. Vehicle lateral dynamic is determined to have the steering input and control torque input. The additional vehicle modes are also defined to using CCV concept. We use right eigenstructure assignment techniques and command generator tracker to design a control law for an lateral vehicle dynamics. The desired eigenvectors are chosen to achieve the desired decoupling (i.e., lateral direction speed and yaw rate). The command generator tracker is used to ensure steady-state tracking of the driver's command. Finally, the developed design is utilized by using the lateral vehicle dynamic with four wheel.

능동비행제어기술에 기반한 자동차 횡방향 제어 (Lateral Vehicle Control Based on Active Flight Control)

  • 서영봉;;최재원
    • 제어로봇시스템학회논문지
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    • 제12권10호
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    • pp.1002-1011
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    • 2006
  • In this paper, a lateral vehicle control using the concept of control configured vehicle(CCV) is presented. The control objectives for the lateral dynamics of a vehicle include the ability to commend a chosen variable without significant motion change in other specified variables. The analysis techniques fur decoupling of the aircraft motions are utilized to develop vehicle lateral control with advanced mode. Vehicle lateral dynamic is determined to have the steering input and control torque input. The additional vehicle modes are also defined to using CCV concept. We use right eigenstructure assignment techniques and command generator tracker to design a control law for an lateral vehicle dynamics. The desired eigenvectors are chosen to achieve the desired decoupling(i.e., lateral direction speed and yaw rate). The command generator tracker is used to ensure steady-state tracking of the driver's command. Finally, the developed design is utilized by using the lateral vehicle dynamic with four wheel.