• 한국통신학회논문지
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• 제30권10A호
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• pp.906-911
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• 2005

본 논문에서는 제한된 피드백 정보를 사용하는 공간 다중화 기법에 사용될 수 있는 부 공간 방식 기반 preceding 기법을 제안한다. 제안된 preceding 기법은 수신기에서 다수의 공통 기저 집합(common basis sets)으로 부터 용량을 최대로 하는 기저들을 선택하고, 선택된 기저들은 feedback 정보를 통해 송신기에 전달되곤 송신기에서는 선택된 기저들로 이루처진 preceding 행렬을 구성한다. 선택된 기저들은 해당 기저들이 속한 기저 집합의 index에 대한 feedback 정보와 선택된 기저 집합에서 각 기저들의 선택 여부에 대한 feedback 정보를 통해 송신기로 feedback된다. 선택된 기저 집합 index는 송수신기가 약속한 공통 기저 집합 중에서 해당 MIMP 채널의 부 공간의 좌표(coordinate)에 가장 적합한 좌표를 나타내고, 해당 좌표에서 상당한 양의 에너지를 포함하는 기저들을 선택함으로써 적은 feedback 정보량으로 MIMO 채널을 묘사한다. 시뮬레이션을 통해 제안된 부 공간 방식 기반 preceding 기법이 적은 feedback 정보량을 사용하면서 폐루프 MIMO 용량 (closed-loop MIMO capacity)에 근접하는 용량을 제공함을 보인다.

• 대한전기학회논문지:시스템및제어부문D
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• 제55권5호
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• pp.226-228
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• 2006

This paper deals with a linear matrix inequality (LMI) approach to the design of a static output feedback controller that simultaneously stabilizes a finite collection of linear time-invariant plants. Simultaneous stabilization by static ouput feedback is represented in terms of LMIs with a rank condition. An iterative penalty method is proposed to solve the rank-constrained LMI problem. Numerical experiments show the effectiveness of the proposed algorithm.

• Smart Structures and Systems
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• 제4권4호
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• pp.407-428
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• 2008

The nonlinear mechanics of cable vibration is caught either by analytical or numerical models. Nevertheless, the choice of the most appropriate method, in consideration of the problem under study, is not straightforward. A feedback control policy might even enhance the complexity of the system. Thus, in order to design a suitable controller, different approaches are here adopted. Devices mounted transversely to the cable in the two directions, close to one of its ends, supply the feedback control action based on the observation of the response in a few points. The low order terms of the control law are, at first, analyzed in the framework of linear models. Explicit analytic solutions are derived for this purpose. The effectiveness of high order terms in the control law is then explored by means of a finite element model(FEM), which accounts for high order harmonics. A suitably dimensional analytical Galerkin model is finally derived, to investigate the effectiveness of the proposed control strategy, when applied to a physical model.

• International Journal of Control, Automation, and Systems
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• 제2권4호
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• pp.475-484
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• 2004

In this paper, we present a dynamic output-feedback receding horizon $H_{\infty}$controller for linear discrete-time systems with disturbance. The controller is obtained numerically from the finite horizon output-feedback $H_{\infty}$optimization problem, which is, in fact, hardly solved analytically. Under a matrix inequality condition on the terminal weighting matrix, the monotonic decreasing property of the cost is shown. This property guarantees both the closed-loop stability and the $H_{\infty}$norm bound. Then, we extend the proposed design method to a reference tracking problem and a problem for time-varying systems. Numerical examples are given to illustrate the performance of the proposed controller.

• 한국정보통신학회논문지
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• 제9권6호
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• pp.1161-1166
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• 2005

본 논문에서는 제한된 피드백 정보를 사용하는 공간 다중화 기법에 사용될 수 있는 부 공간 방식 기반 preceding 기법을 제안한다. 제안된 preceding 기법은 수신기에서 다수의 공통 기저 집합(common basis sets)으로부터 용량을 최대로 하는 기저들을 선택하고, 선택된 기저들은 feedback 정보를 통해 송신기에 전달되고, 송신기에서는 선택된 기저들로 이루어진 precoding 행렬을 구성한다. 선택된 기저들은 해당 기저들이 속한 기저 집합의 index에 대한 feedback 정의와 선택된 기저 집합에서 각 기저들의 선택 여부에 대한 feedback 정보를 통해 송신기로 feedback된다. 선택된 기저 집합 index는 송수신기가 약속한 공통 기저 집합중에서 해당 MIMO 채널의 부 공간의 좌표(coordinate)에 가장 적합한 좌표를 나타내고, 해당 좌표에서 상당한 양의 에너지를 포함하는 기저들을 선택함으로써 적은 feedback 정보량으로 MIMO 채널을 묘사하다. 시뮬레이션을 통해 제안된 부 공간 방식 기반 precoding 기법이 적은 feedback 정보량을 사용하면서 폐루프 MIMO 용량 (closed-loop MIMO capacity)에 근접하는 용량을 제공함을 보인다.

• Structural Engineering and Mechanics
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• 제12권2호
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• pp.135-156
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• 2001

Analytical solutions and finite element results of laminated composite plates with smart material layers embedded in them are presented in this study. The third-order plate theory of Reddy is used to study vibration suppression characteristics. The analytical solution for simply supported boundary conditions is based on the Navier solution procedure. The velocity feedback control is used. Parametric effects of the position of the smart material layers, material properties, and control parameters on the suppression time are investigated. It has been found that (a) the minimum vibration suppression time is achieved by placing the smart material layers farthest from the neutral axis, (b) using thinner smart material layers have better vibration attenuation characteristics, and, (c) the vibration suppression time is larger for a lower value of the feedback control coefficient.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2001년도 춘계학술대회 논문집(한국공작기계학회)
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• pp.3-8
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• 2001

This study is an investigation for the ADS optimum design by using FEA. We write out program which express ADS perfectly and reduce the required time for correcting of model to the minimum in solution and manufacture result. We complete algorithm which can plan optimum forming of model by feedback error information in CAE. Then we correct model by feedback date obtaining in solution process, repeat course following stress solution again and do modeling rachet wheel for optimum forming. That is our aim. In rachet wheel, greatest equivalence stress originates in key groove corner and KS standard is proved the design for security.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 2003년도 ICCAS
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• pp.1911-1916
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• 2003

Parameter set of an LPV system is divided into a number of subsets so that robust feedback gains may be designed for each subset of parameters. A concept of quasi-invariant set is introduced, which allows finite steps of delay in reentrance to the set. A feasible and positively invariant set with respect to a gain-scheduled state feedback control can be easily obtained from the quasi-invariant set. A receding horizon control strategy can be derived based on this feasible and invariant set.

• 대한수학회지
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• 제34권4호
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• pp.841-857
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• 1997

We present analysis and some computational methods for boundary optimal and feedback control problems for Navier-Stokes equations. We use one example to illustrate our methodology and ideas which are applicable to general control problems for Navier-Stokes equations. First, we discuss the existence of optimal solutions and derive an optimality system of equations from which an optimal solution may be computed. Then we present a gradient type iterative method. Finally, we present some numerical results.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2004년도 춘계 학술대회논문집
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• pp.113-118
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• 2004

This paper presents a two-dimensional edge tone to predict the frequency characteristics of the discrete oscillations of a jet-edge feedback cycle by the finite difference lattice Boltzmann method (FDLBM). We use a new lattice BGK compressible fluid model that has an additional term and allow larger time increment comparing the conventional FDLBM, and also use a boundary fitted coordinates. The jet is chosen long enough in order to guarantee the parabolic velocity profile of the jet at the outlet, and the edge consists of a wedge with an angle of $\alpha=23^0$. At a stand-off distance $\omega$, the edge is inserted along the centreline of the jet, and a sinuous instability wave with real frequency f is assumed to be created in the vicinity of the nozzle and th propagate towards the downstream. We have succeeded in capturing very small pressure fluctuations result from periodically oscillation of jet around the edge. That pressure fluctuations propagate with the sound speed. Its interaction with the wedge produces an irrotational feedback field which, near the nozzle exit, is a periodic transverse flow producing the singularities at the nozzle lips. The lattice BGK model for compressible fluids is shown to be one of powerful tool for computing sound generation and propagation for a wide range of flows.