DocumentCode
1325018
Title
Assignment of reduced sensitivity eigenstructure
Author
Ensor, J. ; Davies, R.
Author_Institution
Dept. of Electron., York Univ., UK
Volume
147
Issue
1
fYear
2000
fDate
1/1/2000 12:00:00 AM
Firstpage
104
Lastpage
110
Abstract
The presented technique addresses the problem of maintaining the powerful design simplicity and visibility of eigenstructure assignment, while reducing closed-loop eigenstructure sensitivity to dominant parameter variations. The method results from consideration of the allowable eigenvector subspace as a complete description of the eigenstructure assignment problem. Variations in open-loop system dynamics can thus be visualised as movements of the closed-loop allowable subspace. If a nonlinear model is linearised about two operating points with intersecting subspaces, assignment from the intersection will yield the same closed-loop eigenstructure at both operating points. This hypothesis is proven, and the analysis extended to include the case of non-intersecting subspaces. This reduced subspace design method has been tested on an eighth-order helicopter model that exhibits significant nonlinearity when forward speed is varied. The results demonstrate a considerable reduction in variation of the closed-loop eigenstructure over conventional techniques
Keywords
aircraft control; closed loop systems; control system synthesis; dynamics; eigenstructure assignment; helicopters; linear systems; sensitivity analysis; state feedback; closed-loop systems; dynamics; eigenstructure assignment; eigenvectors; helicopter control; linear time invariant systems; sensitivity analysis; state feedback;
fLanguage
English
Journal_Title
Control Theory and Applications, IEE Proceedings -
Publisher
iet
ISSN
1350-2379
Type
jour
DOI
10.1049/ip-cta:20000137
Filename
838056
Link To Document