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
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;
Conference_Titel :
American Control Conference, 1999. Proceedings of the 1999
Conference_Location :
San Diego, CA
Print_ISBN :
0-7803-4990-3
DOI :
10.1109/ACC.1999.782352
