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