DocumentCode :
3112367
Title :
Robust Stability in a Classical and Modern Context
Author :
Halsey, Kelvin M.
Author_Institution :
Department of Electrical and Electronic Engineering, University of Melbourne, Melbourne, VIC 3010, Australia (e-mail: kmhalsey@ieee.org).
fYear :
2005
fDate :
12-15 Dec. 2005
Firstpage :
2308
Lastpage :
2313
Abstract :
Excluding the open loop gain of a feedback system from a region about the origin of the Nichols chart yields a natural guarantee of robust stability which is commonly used in the analysis of flight control systems. This paper shows that a generalised form of M-circle, based upon a contour of constant |S| + |T|, is symmetrical on the Nichols chart and yields a stability margin consistent with the gain and phase margin requirements of the USAF. This new margin, motivated on purely classical grounds, is shown to be equal to the robust stability margin associated with the loopshaping design procedure of McFarlane and Glover. A corresponding interpretation is obtained for the multivariable case.
Keywords :
Aerospace control; Australia; Control system analysis; Feedback loop; Frequency; Kelvin; Low-frequency noise; Robust stability; Stability criteria; Transfer functions;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Decision and Control, 2005 and 2005 European Control Conference. CDC-ECC '05. 44th IEEE Conference on
Print_ISBN :
0-7803-9567-0
Type :
conf
DOI :
10.1109/CDC.2005.1582506
Filename :
1582506
Link To Document :
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