Title :
Modal decoupling insensitivity
Author :
Raman, K.V. ; Calise, A.J.
Author_Institution :
RCA Astro-Electronics, Princeton, NJ, USA
fDate :
6/1/1987 12:00:00 AM
Abstract :
This note deals with the design of an output feedback control system such that selected closed-loop eigenvalues are insensitive, while the corresponding eigenvectors preserve a prescribed decoupling under parameter variation. This results in restricting specified elements of an eigenvector to be insensitive, rather than the entire eigenvector. This requirement is henceforth referred to as modal decoupling insensitivity. Sufficient conditions for modal decoupling insensitivity are derived. These conditions offer the advantage of increased flexibility in eigenvector assignment, but the constraint on the feedback matrix is more restrictive. A numerical example is presented to illustrate the design procedure.
Keywords :
Decoupling of systems, linear; Eigenvalues/eigenvectors; Output feedback, linear systems; Sensitivity, linear systems; Adaptive control; Aerospace control; Aircraft; Control design; Control systems; Eigenvalues and eigenfunctions; Output feedback; Robust control; Sufficient conditions; System performance;
Journal_Title :
Automatic Control, IEEE Transactions on
DOI :
10.1109/TAC.1987.1104651