DocumentCode
342718
Title
Anti-windup design for manual flight control
Author
Barbu, C. ; Reginatto, R. ; Teel, A.R. ; Zaccarian, L.
Author_Institution
Center for Control Eng. & Comput., California Univ., Santa Barbara, CA, USA
Volume
5
fYear
1999
fDate
1999
Firstpage
3186
Abstract
We address the windup problem arising from actuator rate and magnitude limits in the context of manual flight control for an open loop unstable aircraft. We present a new anti-windup solution tailored for this problem and we compare our result with an optimal solution
Keywords
aircraft control; attitude control; compensation; control system synthesis; dynamics; feedback; military aircraft; stability; actuator rate; antiwindup design; attitude control; compensation; dynamics; elevator deflection; feedback; manual flight control; military aircraft; stability; unstable aircraft; Aerospace control; Aircraft propulsion; Airplanes; Control engineering; Control engineering computing; Elevators; Military aircraft; Prototypes; Steady-state; Windup;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 1999. Proceedings of the 1999
Conference_Location
San Diego, CA
ISSN
0743-1619
Print_ISBN
0-7803-4990-3
Type
conf
DOI
10.1109/ACC.1999.782352
Filename
782352
Link To Document