• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 1996년도 한국자동제어학술회의논문집(국내학술편); 포항공과대학교, 포항; 24-26 Oct. 1996
• /
• pp.569-572
• /
• 1996

Explicit state-space formulate for an H$_{.inf}$ based two-degrees-of-freedom robust controller are derived in discrete-time. The controller provides robust stability against coprime factor uncertainty, and a degree of robust performance in the sense of making the closed-loop system match a prespecified reference model. It is shown that the controller consists of a plant observer, the chosen reference model, and a generalized state feedback law associated with the plant and model states. The controller structure is shown to be relatively simple and thus may reduce the computational load on the digital control processor.

• International Journal of Fuzzy Logic and Intelligent Systems
• /
• 제8권2호
• /
• pp.151-157
• /
• 2008

A non-fragile guaranteed cost control (GCC) problem is presented for a class of discrete time-delay nonlinear systems described by Takagi-Sugeno (T-S) fuzzy model. The systems are assumed to have norm-bounded time-varying uncertainties in the matrices of state, delayed state and control gains. Sufficient conditions are first obtained which guarantee that the closed-loop system is asymptotically stable and the closed-loop cost function value is not more than a specified upper bound. Then the design method of the non-fragile guaranteed cost controller is formulated in terms of the linear matrix inequality (LMI) approach. A numerical example is given to illustrate the effectiveness of the proposed design method.

• 한국시뮬레이션학회논문지
• /
• 제22권2호
• /
• pp.11-19
• /
• 2013

본 논문에서는 전장 환경 요소 및 플랫폼 모델 간 상호 교환 정보를 통합하여 관리하는 전투 공간 모델(Battle Space Model)을 제안한다. 전투 공간 모델은 전장의 지형 정보와 환경 요소를 저장하는 Geographic Information System(GIS) Model, 플랫폼 모델 간 상호 교환 정보에 전장 환경 요소의 영향을 고려하는 Propagator Model, 플랫폼 모델 간 상호 교환 정보를 저장하는 Logger Model, 그리고 플랫폼 모델 간의 상호 작용(encounter) 시점을 예측하고 상호 작용 시점까지 시간을 건너뛰는 Spatial Encounter Predictor(SEP) Model로 구성된다. 또한 이산 사건 및 이산 시간 혼합형 시뮬레이션 모델 구조로 구성되어 있는 플랫폼 모델과 추가 작업 없이 직접 연결하기 위해, 전투 공간 모델 또한 이산 사건 및 이산 시간 혼합형 시뮬레이션 모델 구조로 구성하였다. 본 연구에서는 전투 공간 모델을 적용하여 수중운동체 교전 시뮬레이션을 수행하였다. 이를 통해 플랫폼 모델 각자가 반영하던 전장 환경 요소를 전투 공간 모델이 일괄적으로 반영함으로써 플랫폼 모델 개발을 단순화 할 수 있었다. 또한 각 플랫폼 모델은 다른 플랫폼 모델과의 정보 교환을 고려하지 않고 전투 공간 모델과의 정보 교환만을 고려하면 되므로, 플랫폼 모델을 중립적으로 구성할 수 있었다.

• Kyungpook Mathematical Journal
• /
• 제47권4호
• /
• pp.601-608
• /
• 2007

In this paper we introduce a discrete model of brucellosis happened in Korean livestock farms and numerically analyze its dynamical features. To do it, we consider parameters data supported by Livestock Cooperatives. To control brucellosis, we investigate the relationship among key parameters, as applications of our model. We hope that our model may be used to reduce brucellosis in Korean livestock farms.

• 제어로봇시스템학회논문지
• /
• 제10권2호
• /
• pp.112-124
• /
• 2004

A neural network based adaptive reconfigurable flight controller is presented for a class of discrete-time nonlinear flight systems in the presence of variations of aerodynamic coefficients and control effectiveness decrease caused by control surface damage. The proposed adaptive nonlinear controller is developed making use of the backstepping technique for the angle of attack, sideslip angle, and bank angle command following without two time separation assumption. Feedforward multilayer neural networks are implemented to guarantee reconfigurability for control surface damage as well as robustness to the aerodynamic uncertainties. The main feature of the proposed controller is that the adaptive controller is developed under the assumption that all of the nonlinear functions of the discrete-time flight system are not known accurately, whereas most previous works on flight system applications even in continuous time assume that only the nonlinear functions of fast dynamics are unknown. Neural networks learn through the recursive weight update rules that are derived from the discrete-time version of Lyapunov control theory. The boundness of the error states and neural networks weight estimation errors is also investigated by the discrete-time Lyapunov derivatives analysis. To show the effectiveness of the proposed control law, the approach is i]lustrated by applying to the nonlinear dynamic model of the high performance aircraft.

• 대한수학회지
• /
• 제48권4호
• /
• pp.775-795
• /
• 2011

The disturbance attenuation problem for a class of discretetime switched linear systems with exponential uncertainties via switched state feedback and switched dynamic output feedback is investigated, respectively. By using Taylor series approximation and convex polytope technique, exponentially uncertain discrete-time switched linear system is transformed into an equivalent switched polytopic model with additive norm bounded uncertainty. For such equivalent switched model, one designs its switching strategy and associated state feedback controllers and dynamic output feedback controllers so that whole switched model is asymptotical stabilization with H-in nity disturbance attenuation base on switched Lyapunov function and LMI approach. Finally, two numerical examples are presented to illustrate our results.

• 한국마린엔지니어링학회:학술대회논문집
• /
• 한국마린엔지니어링학회 2005년도 전기학술대회논문집
• /
• pp.314-320
• /
• 2005

In this paper, a methodology for estimating the parameters of a discrete-time system and designing a digital PID controller based on the estimated model and a genetic algorithm is presented. To deal with optimization problems occurring regarding parameter estimation and controller design, a pseudo parallel genetic algorithm (PPGA) is used. The parameters of a discrete-time system are estimated using both the model technique and a PPGA. The digital PID controller is described by the pulse transfer function and its parameters are tuned based on both the model reference technique and another PPGA. A set of experimental works on two processes are carried out to illustrate the performance of the proposed method.

• International Journal of Control, Automation, and Systems
• /
• 제6권2호
• /
• pp.180-185
• /
• 2008

A new method for relative error continuous and discrete time model order reduction is proposed. The reduction technique is based on two recently developed methods, namely frequency domain balanced truncation within a frequency bound and inner-outer factorization techniques. The proposed method is of interest for practical model order reduction because in this context it shows to keep the accuracy of the approximation as high as possible without sacrificing the computational efficiency. Numerical results show the accuracy and efficiency enhancement of the method.

• 물과 미래
• /
• 제24권3호
• /
• pp.61-70
• /
• 1991

본 연구는 이산형 선형 대체함수(discrete linear transfer function)를 이용하여 수문시스템의 입력과 출력으로 나타낼 수 있는 강우와 유출의 관계를 통계학적으로 분석하고 모형화 하는 것이다. 모형의 설정 및 특정(identification), 추정(estimation) 및 검토(diagnostic checking) 과정이 제시되었으며 모형에 대한 적합성은 시계열 분석에서 이용되고 있는 통계량으로 판정하였다.

• 제어로봇시스템학회:학술대회논문집
• /
• 제어로봇시스템학회 1990년도 한국자동제어학술회의논문집(국제학술편); KOEX, Seoul; 26-27 Oct. 1990
• /
• pp.1139-1144
• /
• 1990

In this paper, we consider linear periodic discrete-time control systems under periodic compensation. Such a closed-loop system generally represents a periodic time-varying system. We examine the problem of finding a compensator such that the closed-loop system is realized as LTI model (if possible) with the closed-loop stability being satisfied. We present a necessary and sufficient condition for solving such problem and also give the characterization of realizable LTI models.