DocumentCode
2563563
Title
A structured singular value approach to missile autopilot analysis
Author
Hewer, G.A. ; Klabunde, R. ; Kenney, C.
Author_Institution
US Naval Weapons Center, China Lake, CA, USA
fYear
1988
fDate
7-12 Feb. 1988
Lastpage
1711
Abstract
The authors examine a variety of novel techniques for assessing the stability robustness of linear multivariable feedback control systems. The conservatism of various robustness tests is discussed. A nonconservative measure of robustness called the structured singular value test is introduced. An interconnected structure that applies to real and complex stability tests is demonstrated. Some remarks are made concerning the computability of various tests. It is concluded that structured singular values are less conservative than singular values, but are still conservative when compared to algorithms that attempt to compute an exact stability margin for a combination of parameter variations.<>
Keywords
aerospace control; feedback; military equipment; missiles; multivariable control systems; stability; interconnected structure; linear multivariable feedback control systems; linear systems; military equipment; missile autopilot; multivariable systems; robustness tests; stability robustness; structured singular value; Computer errors; Lakes; Missiles; Open loop systems; Robust control; Robust stability; Robustness; Testing; Uncertainty; Weapons;
fLanguage
English
Publisher
ieee
Conference_Titel
Aerospace Applications Conference, 1988. Digest., 1988 IEEE
Conference_Location
Park City, UT, USA
Type
conf
DOI
10.1109/AERO.1988.38673
Filename
38673
Link To Document