DocumentCode :
3406752
Title :
Sketching rules for the multivariable root locus design technique
Author :
Newman, Brett ; Fu, Dongyu
Author_Institution :
Dept. of Aerosp. Eng., Old Dominion Univ., Norfolk, VA, USA
Volume :
4
fYear :
1998
fDate :
21-26 Jun 1998
Firstpage :
2040
Abstract :
New results are summarized which extend the Evans (1950) root locus design technique to fully coupled, two-channel control law architectures. The new results are based upon various root migration plots, and the underlying framework concerning how the plots influence one another, for the closed-loop poles and zeros in each channel, as key system gains are varied. The new theory facilitates closure of all loops simultaneously, allowing efficient assessment of stability and performance in all channels. The closed-loop pole migration behavior is uniquely interesting in that poles “track moving zeros”. A typical root migration features include direction reversal on real axis loci. Root locus sketching rules for this new framework are developed to assist the designer in implementing gain and compensation strategies by anticipating effects upon system stability and performance. The new theory is demonstrated with a lateral-directional flight control example
Keywords :
aircraft control; closed loop systems; compensation; feedback; multivariable control systems; poles and zeros; stability; stability criteria; aircraft control; closed-loop systems; compensation; direction reversal; feedback; multivariable root locus; poles; root migration plots; sketching rules; stability; two-channel control; zeros; Aerospace control; Aerospace engineering; Automotive engineering; Design engineering; Feedback loop; Performance gain; Poles and zeros; Stability; Systems engineering and theory; Vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
American Control Conference, 1998. Proceedings of the 1998
Conference_Location :
Philadelphia, PA
ISSN :
0743-1619
Print_ISBN :
0-7803-4530-4
Type :
conf
DOI :
10.1109/ACC.1998.702985
Filename :
702985
Link To Document :
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