DocumentCode
834793
Title
Feedback properties of multivariable systems: The role and use of the return difference matrix
Author
Safonov, Michael G. ; Laub, Alan J. ; Hartmann, Gary L.
Author_Institution
University of Southern California, Los Angeles, CA, USA
Volume
26
Issue
1
fYear
1981
fDate
2/1/1981 12:00:00 AM
Firstpage
47
Lastpage
65
Abstract
For linear time-invariant multivariable feedback systems, the feedback properties of plant disturbance attenuation, sensor noise response, stability margins, and sensitivity to plant and sensor variation are quantitatively related to the Bode magnitude versus frequency plots of the singular values of the return difference matrix
and of the associated inverse-return difference matrix
. Implied fundamental limits of feedback performance are quantitatively described and design tradeoffs are discussed. The penalty function in the stochastic linear quadratic Gaussian (LQG) optimal control problem is found to be a weighted-sum of the singular values, with the weights determined by the quadratic cost and noise intensity matrices. This enables systematic "tuning" of LQG cost and noise matrices so that the resulting optimal return difference and inversereturn difference meet inequality constraints derived from design specifications on feedback properties. The theory has been used to synthesize a multivariable automatic controller for the longitudinal dynamics of an advanced fighter aircraft.
and of the associated inverse-return difference matrix
. Implied fundamental limits of feedback performance are quantitatively described and design tradeoffs are discussed. The penalty function in the stochastic linear quadratic Gaussian (LQG) optimal control problem is found to be a weighted-sum of the singular values, with the weights determined by the quadratic cost and noise intensity matrices. This enables systematic "tuning" of LQG cost and noise matrices so that the resulting optimal return difference and inversereturn difference meet inequality constraints derived from design specifications on feedback properties. The theory has been used to synthesize a multivariable automatic controller for the longitudinal dynamics of an advanced fighter aircraft.Keywords
Aircraft control; Feedback systems; Linear quadratic Gaussian (LQG) control; Linear systems; Matrices; Multivariable systems; Attenuation; Cost function; Feedback; Frequency; Linear matrix inequalities; MIMO; Optimal control; Sensor systems; Stability; Stochastic resonance;
fLanguage
English
Journal_Title
Automatic Control, IEEE Transactions on
Publisher
ieee
ISSN
0018-9286
Type
jour
DOI
10.1109/TAC.1981.1102566
Filename
1102566
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