DocumentCode
702388
Title
Receding horizon control of an F-16 aircraft: A comparative study
Author
Keviczky, T. ; Balas, G.J.
Author_Institution
Department of Aerospace Engineering and Mechanics, University of Minnesota, 107 Akerman Hall, 110 Union Street S.E., Minneapolis, Minnesota 55455
fYear
2003
fDate
1-4 Sept. 2003
Firstpage
2656
Lastpage
2661
Abstract
A comparison between Receding Horizon Control (RHC) approaches is presented for the longitudinal axis control of an F-16 aircraft. The results suggest that the flexibility provided by an adaptive RHC scheme based on flight condition dependent linear prediction models is a necessary requirement for achieving good performance as opposed to a single LTI model based method. The adaptive scheme offers an attractive alternative to a full nonlinear model based RHC approach by trading off an acceptable degradation in performance to modest computational complexity and real-time implementability.
Keywords
Adaptation models; Aerospace control; Aircraft; Atmospheric modeling; Mathematical model; Optimization; Predictive models; Flight Control; Optimization; Receding Horizon Control;
fLanguage
English
Publisher
ieee
Conference_Titel
European Control Conference (ECC), 2003
Conference_Location
Cambridge, UK
Print_ISBN
978-3-9524173-7-9
Type
conf
Filename
7086442
Link To Document