• 제목/요약/키워드: Approximate Feedback Linearization

검색결과 18건 처리시간 0.024초

Nonlinear Time-Varying Control Based on Differential Geometry

  • Lee, Jong-Yong;Jung, Kye-dong;Cho, Seongsoo;Strzelecki, Michat
    • International Journal of Internet, Broadcasting and Communication
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    • 제6권2호
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    • pp.1-9
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    • 2014
  • This paper presents a study on nonlinear time varying systems based on differential geometry. A brief introduction about controllability and involutivity will be presented. As an example, the exact feedback linearization and the approximate feedback linearization are used in order to show some application examples.

비선형 시스템의 근사 선형화 (Approximate Linearization of Nonlinear Systems)

  • 남광희;이균경;탁민제
    • 대한전기학회논문지
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    • 제40권7호
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    • pp.690-695
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    • 1991
  • The ability to linearize a nonlinear system by feedback and coordinate change reduces to finding an integrating factor for a one-form which is determined from the system dynamics. Utilizing Taylor series expansion of this one-form, we characterize approximate linearizabilitu. A constructive method is derived for approximate linearization up to order 2.

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자코비안 및 2단 선형화 기법과 부분 상태궤환을 이용한 볼-빔 시스템의 스위칭 제어 (Switching Control of Ball and Beam System using Partial State Feedback: Jacobian and Two-Step Linearization Methods)

  • 이경태;최호림
    • 전기학회논문지
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    • 제66권5호
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    • pp.819-832
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    • 2017
  • We propose a new switching control scheme for a ball and beam system by utilizing two linearization methods. First, the Jacobian linearization is applied and state observer is developed afterward. Then, motivated [6], the approximate input-output linearization is carried out, and after that, the Jacobian linearization is applied along with the design of state observer. Since the second approach requires two linearizations, it is called a two-step linearization method. The state observer is needed for the estimation of the velocities of ball and motor movement. Since the Jacobian linearization based controller tends to provide faster response at the initial time, and after that, the two-step linearization based controller tends to provide better response in terms of output overshoot and convergence to the origin, it is natural to give a switching control scheme to provide the best overall control response. The validity of our control scheme is shown in both simulation and experimental results.

근사 비선형 궤환 선형화를 이용한 도립 진자 계통의 제어 (The Control of Inverted Pendulum System Using Approximated Nonlinear Feedback Linearization)

  • 이종용;이상효
    • 한국통신학회논문지
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    • 제18권3호
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    • pp.372-384
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    • 1993
  • 로보트 제어와 로케트의 자세 제어에 관련하여 도립 진자 시스템은 제어 이론과 응용면에서 흥미 있는 문제이다. 일반적으로 도립 진자 시스템을 제어하기 위하여 소신호 모델에 의한 근사화 모델이 사용되었다. 본 논문에서는 미분 다양체 이론을 기초로 한 비선형 제어 이론을 도입 진자 시스템에 적용하고자 한다. 먼저 비선형 모델을 비선형 상태 궤환을 이용하여 근사 선형화 모델로 변환시키고, 선형화 모델에 극점 배치를 통하여 선형 제어기를 설계하였다. 컴퓨터 시뮬레이션을 통하여 제안된 기법을 Tayler 급수의 3차 선형화모델과 비교하였다.

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비선형 시스템 계통에서 신경망에 근거한 가변구조 제어 (Neural Network based Variable Structure Control for a Class of Nonlinear Systems)

  • 김현호;이천희
    • 정보처리학회논문지A
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    • 제8A권1호
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    • pp.56-62
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    • 2001
  • This paper presents a neural network based variable structure control scheme for nonlinear systems. In this scheme, a set of local variable structure control laws are designed on the basis of the linear models about preselected representative points which cover the range of the system operation of interest. From the combination of the set of local variable structure control laws, neural networks infer the approximate control input in between the operating points. The neural network based variable structure control alleviates the effects of model uncertainties, which cannot be compensated by the control techniques using feedback linearization. It also relaxes the discontinuity in the system’s behavior that appears when the control schemes based on the family of the linear models are applied to nonlinear systems. Simulation results of a ball and beam system, to which feedback linearization cannot be applied, demonstrate the feasibility of the proposed method.

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출력기반 적응제어기법을 이용한 틸트로터 항공기의 회전익 모드 설계연구 (Flight Control of Tilt-Rotor Airplane In Rotary-Wing Mode Using Adaptive Control Based on Output-Feedback)

  • 하철근;임재형
    • 한국항공우주학회지
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    • 제38권3호
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    • pp.228-235
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    • 2010
  • 본 논문에서는 틸트로터 항공기의 회전익 모드에 대한 자율비행 유도제어 알고리즘을 적응제어기법을 이용하여 설계하는 것이다. 이를 위해 우선 출력기반 근사적 궤환선형화 기법을 통하여 알고리즘의 내부루프를 구성하고 그로부터 발생하는 모델오차를 단일 은닉층-신경망을 적용하여 상쇄하였다. 그리고 리아푸노프 안정성 이론에 따른 적응제어 갱신법칙은 선형 관측기를 기반으로 설계하였다. 나아가 외부루프는 경로점 유도법칙으로부터 생성되는 궤적을 추종하도록 하였으며 특히 엄밀한 자동착륙 궤적추종 성능 향상을 위하여 방향각 및 비행경로각 시선유도법칙을 설계하였다. 틸트로터 비선형 모델 시뮬레이션 결과는 콜렉티브 입력에서 보이는 순간적인 작동기 포화현상 이외에는 만족할 만한 안정성과 추종성능을 보여 주고 있다.

Anticontrol of Chaos for a Continuous-time TS Fuzzy System via Time-delay Feedback

  • Zhong Li;Park, Jin-Bea;Joo, Young-Hoon
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2001년도 ICCAS
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    • pp.108.1-108
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    • 2001
  • A time-delay feedback control approach is proposed for making a given stable continuous-time Takagi-Sugeno (TS) fuzzy system chaotic, which is based on the fuzzy feedback linearization and a suitable approximate relationship between a time-delay differential equation and a discrete map. The time-delay feedback controller, chosen among several candidates, is a simple sinusoidal function of the delay states of the system, which has small amplitude. This approach is mathematically proven for rigorous generation of chaos from stable continuous-time TS fuzzy systems, where the generated chaos is in the sense of Li and Yorke. Numerical examples are included to visualize the theoretical analysis and the controller design.

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심한 비선형성을 갖는 시스템의 시간지연 출력궤환을 이용한 추종제어기의 설계 (Tracking Controller Design Using Delayed Output Feedback For Systems With Stiff Nonlinearities)

  • 나승유
    • 한국통신학회논문지
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    • 제16권4호
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    • pp.342-349
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    • 1991
  • 본 논문에서는 동작점에서 근사적인 선형화를 할수 없는 심한 비선형성을 갖는 시스템에 대하여 추종 및 외란제거 제어기의 설계방법을 제안한다. 제어기 합성에는 관측가능한 양만이 사용된다. 추종성과 외란의 제거가 가능하도록 시스템의 출력단에 보상기를 추가하여 비선형성을 제외한 전체 시스템에 시간지연 출력궤환제어를 사용하며, 기술함수방법을 사용하여 출력이 정격내의 값이 되도록 궤환매개변수를 선택하여 비선형성의 난점을 극복한다.

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피이드백 선형화를 위한 안정한 적응 신경회로망 구현 (Implementation of Stable Adaptive Neural Networks for Feedback Linearization)

  • 김동헌;양혜원
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1996년도 추계학술대회 논문집 학회본부
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    • pp.58-61
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    • 1996
  • For a class of single-input single-output continuous-time nonlinear systems, a multilayer neural network-based controller that feedback-linearizes the system is presented. Control action is used to achieve tracking performance for a state-feedback linearizable but unknown nonlinear system. The multilayer neural network(NN) is used to approximate nonlinear continuous function to any desired degree of accuracy. The weight-update rule of multilayer neural network is derived to satisfy Lyapunov stability. It is shown that all the signals in the closed-loop system are uniformly bounded. Initialization of the network weights is straightforward.

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수직다관절 매니퓰레이터에 대한 비선형 되먹임제어의 응용 (Application of Nonlinear Feedback Control to an Articulated Manipulator)

  • Y.S. Baek;C.I. Yang;H.S. Aum
    • 한국정밀공학회지
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    • 제12권9호
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    • pp.104-114
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    • 1995
  • Mathematical models of industrial robots or manipulators are composed of highly nonlinear equations with nonlinear couplings between the variables of motions. These nonlin- earities were not considered important in the first stage that the working speed of the manipulator was not so fast, but the effect of nonlinear forces has become serious, as the working speed has been increased. So more improvement of performance cannot be expected by the control of manipulator using approximate linearization. As an approach for solving these problems, there is a method that eliminates nonlinear theory, which makes possible cecoupling of coupling terms and arbitrary arranging of poles is briefly introduced in this study. When the theory is applied to design the control law, its feasibility is examined whether the reasonable control results are obtained by simulating position, velocity, torque and tracing trajectory. The relations between the coefficients of the linearized differential equations and the maximum error and torque for the prescribed trajectory are also examined. Finally, the method for selecting the values for getting the most rapid and precise response within maximum torque of each drive is suggested in the choice of coefficients of characteristic equations which are obtained as a result of the control.

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