DocumentCode
3550863
Title
Reconfigurable GPC with application to flight control
Author
Shi, Jianjun ; Kelkar, Atul G. ; Soloway, Don
Author_Institution
Dept. of Mech. Eng., Iowa State Univ., Ames, IA, USA
fYear
2005
fDate
8-10 June 2005
Firstpage
2116
Abstract
This paper presents multi-input multi-output (MIMO) generalized predictive control (GPC) law and its application to reconfigurable control. A method to compute the desired end-point state from the desired output and end-point state weighting matrix is given. In particular, an application to flight control with actuator saturation failure is presented. A numerical simulation using a short-period approximation model of a civil transport aircraft is presented to demonstrate the reconfigurable control architecture.
Keywords
MIMO systems; aircraft control; predictive control; actuator saturation failure; civil transport aircraft; flight control; generalized predictive control; multi-input multi-output control; numerical simulation; reconfigurable GPC; short-period approximation model; Actuators; Aerospace control; Computer architecture; Control systems; MIMO; Mechanical engineering; NASA; Numerical simulation; Predictive control; Stability;
fLanguage
English
Publisher
ieee
Conference_Titel
American Control Conference, 2005. Proceedings of the 2005
ISSN
0743-1619
Print_ISBN
0-7803-9098-9
Electronic_ISBN
0743-1619
Type
conf
DOI
10.1109/ACC.2005.1470283
Filename
1470283
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