DocumentCode
767319
Title
Optimal Popov controller analysis and synthesis for systems with real parameter uncertainties
Author
How, Jonathan P. ; Collins, Emmanuel G. ; Haddad, Wassim M.
Author_Institution
Dept. of Mech. Eng., Stanford Univ., CA, USA
Volume
4
Issue
2
fYear
1996
fDate
3/1/1996 12:00:00 AM
Firstpage
200
Lastpage
207
Abstract
Robust performance analysis plays an important role in the design of controllers for uncertain multivariable systems. Recent research has investigated the use of absolute stability criteria to develop less conservative analysis tests for systems with linear and nonlinear real parameter uncertainties. This note extends previous work on optimal ℋ2 performance analysis using the Popov criterion by presenting a numerical homotopy algorithm that can be used to analyze systems with less restrictive assumptions on the structure of the uncertainty block. The technique is used to compare relative robustness capabilities of the various control algorithms that have been designed for the Middeck active control experiment (MACE). The analysis is combined with the previously presented Popov controller synthesis to yield compensators that guarantee robust performance for systems with real parameter uncertainty
Keywords
Popov criterion; absolute stability; aerospace control; compensation; control system analysis; control system synthesis; multivariable control systems; optimal control; robust control; uncertain systems; Middeck active control experiment; Popov criterion; absolute stability criteria; less conservative analysis tests; numerical homotopy algorithm; optimal H2 performance analysis; optimal Popov controller; parameter uncertainties; robust performance analysis; uncertain multivariable systems; Algorithm design and analysis; Control system analysis; Control system synthesis; Control systems; MIMO; Optimal control; Performance analysis; Robust control; Stability criteria; Uncertain systems;
fLanguage
English
Journal_Title
Control Systems Technology, IEEE Transactions on
Publisher
ieee
ISSN
1063-6536
Type
jour
DOI
10.1109/87.486347
Filename
486347
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