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
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;
Conference_Titel :
American Control Conference, 2005. Proceedings of the 2005
Print_ISBN :
0-7803-9098-9
Electronic_ISBN :
0743-1619
DOI :
10.1109/ACC.2005.1470283
