• 제목/요약/키워드: Control law approach

검색결과 228건 처리시간 0.073초

SYNTHESIS OF DISCRETE TIME FLIGHT CONTROL SYSTEM USING NONLINEAR MODEL MATCHING

  • Aoi, Kazunari;Osa, Yasuhiro;Uchikado, Shigeru
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2000년도 제15차 학술회의논문집
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    • pp.460-460
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    • 2000
  • Until now various model matching systems have been proposed for linear system, but very little has been done for nonlinear system In this paper, a design method of discrete time flight control system using nonlinear model matching is proposed. This method is based on Hirschorn's algorithm and facilitates easy determination of the control law using the relationship, between the output and the input, which is obtained by the time shift of the output. Also as a result, this method is the extension of the linear model matching control system proposed by Wolovich, in which the control law is obtained by left-multiplying the output by the interactor matrix. At the end of paper, the proposed control system is applied to CCV flight control system of an aircraft and the feasibility of the proposed approach is shown by the numerical simulations.

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항공기 자동착륙 유도 법칙에 관한 연구 (Guidance Laws for Aircraft Automatic Landing)

  • 민병문;노태수;송기정
    • 한국항공우주학회지
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    • 제30권5호
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    • pp.41-47
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    • 2002
  • 본 논문에서는 일반항공기나 무인항공기의 자동착륙에 적용할 수 있는 착륙 유도 법칙을 제안하고 기존의 일반적인 착륙 과정과의 비교를 통하여 성능을 확인하였다. 착륙 유도법칙은 미사일 요격에서 사용되는 Miss distance 개념과 Lyapunov 안정성 이론에 근거하여 궤환 형태의 속도 및 비행 경로각 명령을 생성할 수 있도록 구성하였다. 기존 문헌에 제시된 항공기의 자동착륙 시뮬레이션을 이용하여 착륙 접근 및 착지 기동 과정을 모사하였다. 착륙 접근의 제U 목적인 강하로 이탈 거리 제거와, 착지 기동시 제어 목적인 고도 제어의 관점에서 새로이 제안하고 있는 착륙 유도 법칙은 기존 방법에 대등 또는 우수한 결과를 얻을 수 있었다. 기준 궤적의 설정에 따라 다양한 비행 궤적 추종이 가능하므로 향후 무인기의 자동 착륙이나 기동 비행의 설계시 적용할 수 있을 것이다.

A dynamic game approach to robust stabilization of time-varying discrete linear systems via receding horizon control strategy

  • Lee, Jae-Won;Kwon, Wook-Hyun
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1995년도 Proceedings of the Korea Automation Control Conference, 10th (KACC); Seoul, Korea; 23-25 Oct. 1995
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    • pp.424-427
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    • 1995
  • In this paper, a control law based on the receding horizon concept which robustly stabilizes time-varying discrete linear systems, is proposed. A dynamic game problem minimizing the worst case performance, is adopted as an optimization problem which should be resolved at every current time. The objective of the proposed control law is to guarantee the closed loop stability and the infinite horizon $H^{\infty}$ norm bound. It is shown that the objective can be achieved by selecting the proper terminal weighting matrices which satisfy the inequality conditions proposed in this paper. An example is included to illustrate the results..

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Robust Predictive Feedback Control for Constrained Systems

  • Giovanini, Leonardo;Grimble, Michael
    • International Journal of Control, Automation, and Systems
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    • 제2권4호
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    • pp.407-422
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    • 2004
  • A new method for the design of predictive controllers for SISO systems is presented. The proposed technique allows uncertainties and constraints to be concluded in the design of the control law. The goal is to design, at each sample instant, a predictive feedback control law that minimizes a performance measure and guarantees of constraints are satisfied for a set of models that describes the system to be controlled. The predictive controller consists of a finite horizon parametric-optimization problem with an additional constraint over the manipulated variable behavior. This is an end-constraint based approach that ensures the exponential stability of the closed-loop system. The inclusion of this additional constraint, in the on-line optimization algorithm, enables robust stability properties to be demonstrated for the closed-loop system. This is the case even though constraints and disturbances are present. Finally, simulation results are presented using a nonlinear continuous stirred tank reactor model.

회전행렬과 쿼터니언에 근거한 비행체 제어기 설계 (Controller Design for Aircraft Based on Rotational Matrix and Quaternion)

  • 함운철;후렐바타르
    • 로봇학회논문지
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    • 제4권2호
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    • pp.88-96
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    • 2009
  • In this paper, we present a linear controller for attitude of aircraft. We use a rotational matrix in one approach and a quaternion in the other approach. We also find some interesting mathematical properties concerning a symmetric rotational matrix and we use these properties to analyze the stability of the proposed control law. We find that the quaternion approach is better than rotational matrix approach because there exists no singular region problem in quaternion approach. On the other hand, singular region problem may happens in rotational matrix approach. The controller structure of the quaternion is also very simple compared with the one proposed by using a rotational matrix approach. We make use Matlab Simulink to simulate and illustrate the theoretical claims. The graphic animation program is developed based on Open-GL for the computer simulation of the proposed control algorithm.

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로봇 매니퓰레이터의 새로운 견실제어기 설계 (New Robust Control Fesigns of Robot Manipulators)

  • 한명철
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국내학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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    • pp.666-671
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    • 1993
  • A new robust control law is proposed for uncertain rigid robots and two composite robust control laws for flexible-joint manipulators which contain uncertainties. The uncertainty, is nonlinear and (possibly fast) time-varying. Therefore, the uncertain factors such as imperfect modeling, function, payload change, and external disturbances are all addressed. Based only on the possible bound of the uncertainty, a robust controller is constructed for the rigid counterpart of the flexible-joint robot Some feedback control terms are then added to the robust control law to stabilize the elastic vibrations at the joints. To show that the proposed composite robust control laws are indeed applicable to flexible-joint robots, a singular perturbation approach and the stability study based on Lyapunov function are proposed.

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Controlling robot by image-based visual servoing with stereo cameras

  • Fan, Jun-Min;Won, Sang-Chul
    • 한국정보기술응용학회:학술대회논문집
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    • 한국정보기술응용학회 2005년도 6th 2005 International Conference on Computers, Communications and System
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    • pp.229-232
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    • 2005
  • In this paper, an image-based "approach-align -grasp" visual servo control design is proposed for the problem of object grasping, which is based on the binocular stand-alone system. The basic idea consists of considering a vision system as a specific sensor dedicated a task and included in a control servo loop, and we perform automatic grasping follows the classical approach of splitting the task into preparation and execution stages. During the execution stage, once the image-based control modeling is established, the control task can be performed automatically. The proposed visual servoing control scheme ensures the convergence of the image-features to desired trajectories by using the Jacobian matrix, which is proved by the Lyapunov stability theory. And we also stress the importance of projective invariant object/gripper alignment. The alignment between two solids in 3-D projective space can be represented with view-invariant, more precisely; it can be easily mapped into an image set-point without any knowledge about the camera parameters. The main feature of this method is that the accuracy associated with the task to be performed is not affected by discrepancies between the Euclidean setups at preparation and at task execution stages. Then according to the projective alignment, the set point can be computed. The robot gripper will move to the desired position with the image-based control law. In this paper we adopt a constant Jacobian online. Such method describe herein integrate vision system, robotics and automatic control to achieve its goal, it overcomes disadvantages of discrepancies between the different Euclidean setups and proposes control law in binocular-stand vision case. The experimental simulation shows that such image-based approach is effective in performing the precise alignment between the robot end-effector and the object.

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연소공간 변화를 보상하는 가스발생기 압력 제어기법 (Pressure Control Law of Gas Generator Considering Combustion Volume Change)

  • 박익수;이재윤;최호진;김중회;윤현걸;임진식
    • 한국추진공학회지
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    • 제16권3호
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    • pp.34-40
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    • 2012
  • 가스발생기의 압력 제어기법을 제안하였다. 모델기반 제어법칙을 설계하기 위하여 Robert 식과 보존 방정식을 이용하여 가스발생기의 모델을 구성하였고, 연소시험을 통하여 모델의 정확성을 검증하였다. 모델은 연소 공간이 증가함에 따라 시스템의 고유 특성이 변화하게 되는데, 이러한 특성으로 인한 폐루프 구조에서 나타나는 응답특성을 해석하기 위하여 PID 및 비선형 적응 제어법칙을 설계하였다. 수치 시뮬레이션 결과 두 방법이 각각 제어 성능과 실제 시스템 적용에 문제가 있음을 알 수 있었고, 이를 극복하기 위한 새로운 제어기법을 제안하였다. 새롭게 제안된 이득계획 제어기법의 수치 시뮬레이션 결과 외란 및 측정 잡음의 영향에서도 우수한 제어 응답성능을 보였다.

연소공간 변화를 보상하는 가스발생기 압력 제어기법 (Pressure control law of gas generator considering combustor volume change)

  • 박익수;이재윤;최호진;박근홍;윤현걸;임진식
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제37회 추계학술대회논문집
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    • pp.618-623
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    • 2011
  • 가스발생기의 압력 제어기법을 제안하였다. 모델기반 제어법칙을 설계하기 위하여 Robert 식과 보존방정식을 이용하여 가스발생기의 모델을 구성하였고, 연소시험을 통하여 모델의 정확성을 검증하였다. 모델은 연소 공간이 증가함에 따라 시스템의 고유 특성이 변화하게 되는데, 이러한 특성으로 인한 폐루프 구조에서 나타나는 응답특성을 평가하기 위하여 PID 및 비선형 적응 제어법칙을 설계하였다. 수치 시뮬레이션 결과 두 방법이 각각 제어 성능과 실제 시스템 적용에 문제가 있음을 알 수 있었고, 이를 극복하기 위한 새로운 제어기법을 제안하였다. 새롭게 제안된 이득계획 제어기법의 수치 시뮬레이션 결과 외란 및 측정 잡음의 영향에서도 우수한 제어 응답성능을 보였다.

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불확실성 및 관절 유연성을 고려한 로봇의 견실제어기 설계 (Robust control design for robots with uncertainty and joint-flexibility)

  • M.C. Han
    • 한국정밀공학회지
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    • 제12권5호
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    • pp.117-125
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    • 1995
  • An improved robust control law is proposed for uncertain rigid robots. The uncertainty is nonlinear and (possibly fast) time-varying. Therefore, the uncertain factors such as imperfect modeling, friction, payload change, and external disturbances are all addressed. Based on the possible bound of the uncertainty, the controller is constructed. For uncertain flexible-joint robots, some feedback control terms are then added to the proposed robust control law in order to stabilize the elastic vibrations at the joints. To show that the proposed control laws are indeed applicable, the stability study based on Lyapunov function, a singular perturbation approach, and simulation results are presented.

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