DocumentCode
2468415
Title
Control reconfiguration with actuator rate saturation
Author
Pachter, M. ; Chandler, P.R. ; Mears, M.
Author_Institution
Dept. of Electr. & Comput. Eng., Air Force Inst. of Technol., Wright-Patterson AFB, OH, USA
Volume
5
fYear
1995
fDate
21-23 Jun 1995
Firstpage
3495
Abstract
Online system identification and online optimization is used to maximize aircraft tracking performance before and after control surface failure, yet prevent departure. The online optimization consists of receding horizon/model predictive optimal control with one-step-ahead actuator rate constraint enforcement. Such hard constraint enforcement is rigorous through use of a linear programming algorithm to include rate saturation in the design
Keywords
aircraft control; identification; linear programming; optimal control; predictive control; real-time systems; tracking; actuator rate constraint enforcement; actuator rate saturation; aircraft tracking; control reconfiguration; linear programming; model predictive optimal control; online optimization; online system identification; receding horizon; Actuators; Aerospace control; Aircraft; Algorithm design and analysis; Constraint optimization; Control systems; Linear programming; Optimal control; Predictive models; System identification;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, Proceedings of the 1995
Conference_Location
Seattle, WA
Print_ISBN
0-7803-2445-5
Type
conf
DOI
10.1109/ACC.1995.533786
Filename
533786
Link To Document