Controller design for bilinear systems with parametric uncertainties.
Shi, Peng, Shue, Shyh-Pyng, Shi, Yan, Agarwal, Ramesh K. (1999)
Mathematical Problems in Engineering
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Shi, Peng, Shue, Shyh-Pyng, Shi, Yan, Agarwal, Ramesh K. (1999)
Mathematical Problems in Engineering
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Lan Zhou, Jinhua She, Shaowu Zhou (2014)
International Journal of Applied Mathematics and Computer Science
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Lubomír Bakule (2009)
Kybernetika
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This special issue provides information on current and future research directions in the emerging field of Decentralized Control of Large Scale Complex Systems. There is generally adopted view that a dynamic system is large scale complex whenever it is necessary to partition its analysis or synthesis problem to manageable subproblems. Its fundamental characteristics in modeling and control are high dimensionality, uncertainty, information structure constraints, and delays. Theory of...
Semba, Tetsuo, Furuta, Katsuhisa (1996)
Mathematical Problems in Engineering
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Lan Zhou, Jinhua She, Shaowu Zhou (2014)
International Journal of Applied Mathematics and Computer Science
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This paper is concerned with the problem of designing a robust modified repetitive-control system with a dynamic outputfeedback controller for a class of strictly proper plants. Employing the continuous lifting technique, a continuous-discrete two-dimensional (2D) model is built that accurately describes the features of repetitive control. The 2D control input contains the direct sum of the effects of control and learning, which allows us to adjust control and learning preferentially....
Erik Etien, Sébastien Cauet, Laurent Rambault, Gérard Champenois (2002)
International Journal of Applied Mathematics and Computer Science
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Nonlinear control of the squirrel induction motor is designed using sliding mode theory. The developed approach leads to the design of a sliding mode controller in order to linearize the behaviour of an induction motor. The second problem described in the paper is decoupling between two physical outputs: the rotor speed and the rotor flux modulus. The sliding mode tools allow us to separate the control from these two outputs. To take account of parametric variations, a model-based approach...
Yong He, Chunjuan Li, Weiguo Zhang, Jingping Shi, Yongxi Lü (2016)
Kybernetika
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In flight control of a morphing aircraft, the design objective and the dynamics may be different in its various configurations. To accommodate different performance goals in different sweep wing configurations, a novel switching strategy, mode dependent average dwell time (MDADT), is adopted to investigate the flight control of a morphing aircraft in its morphing phase. The switching signal used in this note is more general than the average dwell time (ADT), in which each mode has its...
Marian J. Błachuta, Valery D. Yurkevich, Konrad Wojciechowski (1999)
Kybernetika
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In the paper the design of an aircraft motion controller based on the Dynamic Contraction Method is presented. The control task is formulated as a tracking problem for Euler angles, where the desired decoupled output transients are accomplished under assumption of high-level, high-frequency sensor noise and incomplete information about varying parameters of the system and external disturbances. The resulting controller has a simple form of a combination of a low-order linear dynamical...
Franco Blanchini, S. Cotterli, G. Koruza, S. Miani, R. Siagri, Luciano Tubaro (1999)
Kybernetika
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In this work we consider the problem of determining and implementing a state feedback stabilizing control law for a laboratory two-tank dynamic system in the presence of state and control constraints. We do this by exploiting the properties of the polyhedral Lyapunov functions, i. e. Lyapunov functions whose level surfaces are polyhedra, in view of their capability of providing an arbitrarily good approximation of the maximal set of attraction, which is the largest set of initial states...
Francis Clarke, Richard Vinter (2009)
Control and Cybernetics
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