Identification of structural parameters for active vibration control
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The study of algorithms for active vibration control in flexible structures became an area of enormous interest for some researchers due to the innumerable requirements for better performance in mechanical systems, as for instance, aircrafts and aerospace structures. Intelligent systems, constituted for a base structure with sensors and actuators connected, are capable to guarantee the demanded conditions, through the application of diverse types of controllers. For the project of active controllers it is necessary, in general, to know a mathematical model that enable the representation in the space of states, preferential in modal coordinates to permit the truncation of the system and reduction in the order of the controllers. For practical applications of engineering, some mathematical models based in discrete-time systems cannot represent the physical problem, therefore, techniques of identification of system parameters must be used. The techniques of identification of parameters determine the unknown values through the manipulation of the input (disturbance) and output (response) signals of the system. Recently, some methods have been proposed to solve identification problems although, none of them can be considered as being universally appropriate to all the situations. This paper is addressed to an application of linear quadratic regulator controller in a structure where the damping, stiffness and mass matrices were identified through Chebyshev's polynomial functions.
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Active vibration controls, Discrete time system, Identification of systems, Identification problem, Linear quadratic regulator controllers, Polynomial functions, Sensors and actuators, Structural parameter, Digital control systems, Discrete time control systems, Flexible structures, Identification (control systems), Intelligent systems, Mathematical models, Vibration control, Parameter estimation
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Inglês
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13th International Congress on Sound and Vibration 2006, ICSV 2006, v. 5, p. 3626-3633.
