Title :
Assignment of reduced sensitivity eigenstructure
Author :
Ensor, J. ; Davies, R.
Author_Institution :
Dept. of Electron., York Univ., UK
fDate :
1/1/2000 12:00:00 AM
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;
Journal_Title :
Control Theory and Applications, IEE Proceedings -
DOI :
10.1049/ip-cta:20000137