DocumentCode :
3305703
Title :
Convergence based anti-windup design method and its application to flight control
Author :
Andrievsky, B.R. ; Kuznetsov, N.V. ; Leonov, G.A. ; Pogromsky, A.Y.
Author_Institution :
Math. & Mech. Fac., St.-Petersburg State Univ., St. Petersburg, Russia
fYear :
2012
fDate :
3-5 Oct. 2012
Firstpage :
212
Lastpage :
218
Abstract :
A convergence-based anti-windup control strategy is presented and demonstrated by the example of aircraft yaw control problem.
Keywords :
aircraft control; convergence; convergence-based antiwindup control strategy; flight control; Aerospace control; Aircraft; Atmospheric modeling; Servomotors; Stability criteria; anti-windup correction; convergent systems; flight control; integrator windup;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Ultra Modern Telecommunications and Control Systems and Workshops (ICUMT), 2012 4th International Congress on
Conference_Location :
St. Petersburg
ISSN :
2157-0221
Print_ISBN :
978-1-4673-2016-0
Type :
conf
DOI :
10.1109/ICUMT.2012.6459667
Filename :
6459667
Link To Document :
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