Title :
Robust partial pole assignment for vibrating systems with aerodynamic effects
Author :
Datta, Biswa N. ; Lin, Wen-Wei ; Wang, Jenn-Nan
Author_Institution :
Dept. of Math. Sci., Northern Illinois Univ., DeKalb, IL, USA
Abstract :
This paper proposes a novel algorithm for robust partial eigenvalue assignment (RPEVA) problem for a cubic matrix pencil arising from modeling of vibrating systems with aerodynamic effects. The RPEVA problem for a cubic pencil is the one of choosing suitable feedback matrices to reassign a few (say k < 3n) unwanted eigenvalues while leaving the remaining large number (3n - k) of them unchanged, in such a way that the the eigenvalues of the closed-loop matrix are as insensitive as possible to small perturbation of the data. The latter amounts to minimizing the condition number of the closed-loop eigenvector matrix. The problem is solved directly in the cubic matrix polynomial setting without making any transformation to a standard first-order state-space system. This allows us to take advantage of the exploitable structures such as the sparsity, definiteness, bandness, etc., very often offered by large practical problems. The major computational requirements are: (i)solutions of a small Sylvester equation, (ii) QR factorizations, and (iii) solutions or some standard least squares problems. The least-squares problems result from matrix rank-one and rank-two update techniques used in the algorithm for reassigning, respectively, simple and complex eigenvalues. The practical effectiveness of the method is demonstrated by implementational results on simulated data provided by the Boeing company.
Keywords :
aerodynamics; closed loop systems; eigenvalues and eigenfunctions; least squares approximations; pole assignment; polynomial matrices; vibrations; Boeing; QR factorizations; aerodynamic effects; condition number minimisation; cubic matrix pencil; cubic matrix polynomial; feedback matrices; matrix rank-one update techniques; matrix rank-two update techniques; robust partial pole assignment; small Sylvester equation; standard least squares problems; vibrating systems; Aerodynamics; Control systems; Damping; Eigenvalues and eigenfunctions; Feedback; Force control; Mathematics; Polynomials; Robustness; Symmetric matrices;
Conference_Titel :
Decision and Control, 2004. CDC. 43rd IEEE Conference on
Print_ISBN :
0-7803-8682-5
DOI :
10.1109/CDC.2004.1429663