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Lqr control of thin shell dynamics: formulation and numerical implementation
| Content Provider | NASA Technical Reports Server (NTRS) |
|---|---|
| Author | Smith, R. C. delRosario, R. C. H. |
| Copyright Year | 1997 |
| Description | 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. |
| File Size | 1654150 |
| Page Count | 34 |
| File Format | |
| Alternate Webpage(s) | http://archive.org/details/NASA_NTRS_Archive_19980017840 |
| Archival Resource Key | ark:/13960/t6xw9c00r |
| Language | English |
| Publisher Date | 1997-11-01 |
| Access Restriction | Open |
| Subject Keyword | Numerical Analysis Actuators Partial Differential Equations Control Systems Design Feedback Control Piezoelectric Ceramics Convergence Cylindrical Shells Thin Walled Shells Donnell Equations Dynamic Models Galerkin Method Polynomials Linear Quadratic Regulator Ntrs Nasa Technical Reports ServerĀ (ntrs) Nasa Technical Reports Server Aerodynamics Aircraft Aerospace Engineering Aerospace Aeronautic Space Science |
| Content Type | Text |
| Resource Type | Technical Report |