• 제목/요약/키워드: Minimum phase system

검색결과 328건 처리시간 0.023초

증분형 추정기를 사용한 오프세트의 일반화 최소분산형 자기동조제어 (Generalized Minimum Variance Self-tuning Control of Offset Using Incremental Estimator)

  • 박정일;최계근
    • 대한전자공학회논문지
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    • 제25권4호
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    • pp.372-378
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    • 1988
  • The elimination of offsets such as those induced by load disturbance is a principal requirement in the control of industrial processes. In this paper we propose a self-tuning minimum variance control in the two tuypes of k-incremental and integrating form. Since the objective of control design in this paper is a generalized minimum variance control, it can be applied to nonminimum phase system. And we compare the proposed algorithm wiht that of the positional self-tuning control and show that it can also be applied to nonminimum phase system by computer simulation.

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비최소위상 비선형 시스템의 출력궤환 안정화 (Output Feedback Stabilization of Non-Minimum phase Nonlinear Systems)

  • 조남훈
    • 제어로봇시스템학회논문지
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    • 제9권12호
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    • pp.977-983
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    • 2003
  • An output feedback stabilizing controller far non-minimum phase nonlinear systems is presented. We first perform the standard input-output linearization of the system and then transform the zero dynamics into a special normal form in which the antistable part is not affected by the stable part and the antistable part is given in approximately linear form. Under the assumption that the nonlinear system satisfies the observability rank condition, we can design an observer f3r the extended system that is made of the augmentation of a chain of integrators. The proposed output feedback stabilizing controller can then be designed by combining the observer and the state feedback controller.

C(sI-A)-1B가 최소위상이 될 LMI 조건을 이용한 해석과 설계 (Analysis and Design Using LMI Condition for C (sI-A)^{-1} to Be Minimum Phase)

  • 이재관;최한호
    • 제어로봇시스템학회논문지
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    • 제11권11호
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    • pp.895-900
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    • 2005
  • We derive a linear matrix inequality(LMI) condition guaranteeing that any invariant zeros of a triple (A, B, C) lie in the open left half plane of the complex plane, i.e. $C(sI-A)^{-1}B$ is minimum phase. The LMI condition is equivalent to a certain constrained Lyapunov matrix equation which can be found in many results relating to stability analysis or control design. We show that the LMI condition can be used to simplify various control engineering problems such as a dynamic output feedback control problem, a variable structure static output feedback control problem, and a nonlinear system observer design problem. Finally, we give some numerical examples.

시간 지연을 갖는 2차 시스템 모델링 기법을 이용한 외란 관측기 설계 (Design of a Disturbance Observer Using a Second-Order System Plus Dead Time Modeling Technique)

  • 정구종;손영익
    • 전기학회논문지
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    • 제58권1호
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    • pp.187-192
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    • 2009
  • This paper presents a method for designing a robust controller that alleviates disturbance effects and compensates performance degradation owing to the time-delay. Disturbance observer(DOB) approach as a tool of robust control has been widely employed in industry. However, since the Pade approximation of time-delay makes the plant non-minimum phase, the classical DOB cannot be applied directly to the system with time-delay. By using a new DOB structure for non-minimum phase systems together with the Smith Predictor, we propose a new controller for reducing the both effects of disturbance and time-delay. Moreover, the closed-loop system can be made robust against uncertain time-delay with the help of a Pill controller tuning method that is based on a second-order plus dead time modeling technique.

비정방 선형 시스템의 강인 제어기 설계 및 그 응용 (Robust Controller Design of Non-Square Linear Systems and Its Applications)

  • 손영익;심형보;조남훈
    • 대한전기학회논문지:시스템및제어부문D
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    • 제52권4호
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    • pp.189-197
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    • 2003
  • The problem of designing a parallel feedforward compensator (PFC) is considered for a class of non-square linear systems such that the closed-loop system is strictly passive. If a given square system has (vector) relative degree one and is weakly minimum phase, the system can be rendered passive by a state feedback. However, when the system states are not always measurable and the given output is considered, passivation (i.e. rendering passive) of a non-minimum phase system or a system with high relative degree cannot be achieved by any other methodologies except by using a PFC. To passivate a non-square system we first determine a squaring gain matrix and design a PFC such that the composite system has relative degree one and is minimum phase. Then the system is rendered strictly passvie by a static output feedback law. Necessary and sufficient conditions for the existence of the PFC and the squaring gain matrix are given by the static output feedback formulation, which enables to utilize linear matrix inequality (LMI). As an application of the scheme, an alternative way of replacing the role of velocity measurements is provided for the PD-control law of a convey-crane system.

신경회로망 기반 미사일 적응제어기의 모델 불확실 상황에 대한 시뮬레이션 연구 (Simulation Analysis of the Neural Network Based Missile Adaptive Control with Respect to the Model Uncertainty)

  • 성재민;김병수
    • 제어로봇시스템학회논문지
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    • 제16권4호
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    • pp.329-334
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    • 2010
  • This paper presents the design of a neural network based adaptive control for missile. Acceleration of missile by tail fin control cannot be controllable by DMI (Dynamic Model Inversion) directly because it is non-minimum phase system. To avoid the non-minimum phase system, dynamic model inversion is applied with output-redefinition method. In order to evaluate performance of the suggested controllers we selected the three cases such as control surface fail, control surface loss and wing loss for model uncertainty. The corresponding aerodynamic databases to the failure cases were calculated by using the Missile DATACOM. Using a high fidelity 6DOF simulation program of the missile the performance was evaluates.

기존제어기와 신경회로망의 혼합제어기법을 이용한 미사일 적응 제어기 설계 (Adaptive Control Design for Missile using Neural Networks Augmentation of Existing Controller)

  • 김광찬;성재민;김병수
    • 제어로봇시스템학회논문지
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    • 제14권12호
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    • pp.1218-1225
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    • 2008
  • This paper presents the design of a neural network based adaptive control for missile is presented. The application model is Exocet MM40, which is derived from missile DATCOM database. Acceleration of missile by tail Fin control cannot be controllable by DMI (Dynamic Model Inversion) directly because it is non-minimum phase system. So, the inner loop consists of DMI and NN (Neural Network) and the outer loop consists of PI controller. In order to satisfy the performances only with PI controller, it is necessary to do some additional process such as gain tuning and scheduling. In this paper, all flight area would be covered by just one PI gains without tuning and scheduling by applying mixture control technique of conventional controller and NN to the outer loop. Also, the simulation model is designed by considering non-minimum phase system and compared the performances to distinguish the validity of control law with conventional PI controller.

이산시간 비 최소현상 시스템의 직지 적응 극배룰 및 안전팡에 관한 연구 (Direct Adaptive Pole-Placement and Stability of Discrete-time Non-minimum Phase Systems)

  • 최종호;최진영
    • 대한전기학회논문지
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    • 제33권5호
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    • pp.193-199
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    • 1984
  • This paper presents a direct adaptive pole placement control scheme which is applicable to discretetime non-minimum phase systems. It is proved that by this scheme the poles can be placed at the desired locations and the overall state vector of the system is uniformly bounded if the reference input is sufficiently rich, and also proved that in case of insufficiently rich reference input the overall system can still be stabilized though the poles may not be placed exactly at the desired locations. The effectiveness of this scheme is verified by digital computer simulations.

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적응제어를 이용한 유압 액츄에이터의 특성개선에 관한 연구 (A Study on the Characteristics Improvement of Fluid Power Actuator Using Adaptive Control)

  • 염만오;윤일로
    • 한국정밀공학회지
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    • 제21권1호
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    • pp.124-132
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    • 2004
  • A hydraulic system is difficult to keep the performance due to non-linearity, load pressure which changes according to working condition and system parameter variation, the requirement of control algorithm has been risen in order to satisfy them. An adaptive control is a control method which is suggested to achieve a control object though plant characteristics change. In spite of the case that plant characteristics and the degree of variation are difficult to grasp, adaptive control can keep the characteristics of closed-loop system regularly. In this study GMVAC(generalized minimum variance adaptive control) combined with output error feedback is proposed in order to solve problems of non-minimum phase, vibration and overshoot in initial response of the plant. The control performance according to the variation of characteristics of the plant is evaluated by changing the supply pressure only.