NASA NTRS · 19980017840
LQR Control of Thin Shell Dynamics: Formulation and Numerical Implementation
Abstract
A PDE-based feedback control method for thin cylindrical shells with surface-mounted piezoceramic actuators is presented. Donnell-Mushtari equations modified to incorporate both passive and active piezoceramic patch contributions are used to model the system dynamics. The well-posedness of this model and the associated LQR problem with an unbounded input operator are established through analytic semigroup theory. The model is discretized using a Galerkin expansion with basis functions constructed from Fourier polynomials tensored with cubic splines, and convergence criteria for the associated approximate LQR problem are established. The effectiveness of the method for attenuating the coupled longitudinal, circumferential and transverse shell displacements is illustrated through a set of numerical examples.
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delRosario, R. C. H., Smith, R. C.. 1997-11-01. LQR Control of Thin Shell Dynamics: Formulation and Numerical Implementation. https://ntrs.nasa.gov/citations/19980017840
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