DocumentCode
487246
Title
A Structured Singular Value Approach to Missile Autopilot Analysis II
Author
Hewer, G.A. ; Klabunde, Richard ; Kenney, Charles
Author_Institution
Naval Weapons Center, Code 39102, China Lake, CA 93555
fYear
1988
fDate
15-17 June 1988
Firstpage
323
Lastpage
327
Abstract
A state space model for additive errors that is algebraically and dynamically equivalent to Doyle´s structured singular value is presented. Using this theory a new algorithm based on a Monte Carlo eigenvalue search is presented. Some examples are included that illustrate the convergence properties of the Monte Carlo technique.
Keywords
Control systems; Eigenvalues and eigenfunctions; Lakes; Missiles; Monte Carlo methods; Output feedback; Robust control; Robustness; State-space methods; Weapons;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1988
Conference_Location
Atlanta, Ga, USA
Type
conf
Filename
4789737
Link To Document