DocumentCode
3246443
Title
Aircraft landing control based on adaptive CMAC
Author
Yang, Teng-Chieh ; Juang, Jih-Gau
Author_Institution
Dept. of Commun. & Guidance Eng., Nat. Taiwan Ocean Univ., Keelung, Taiwan
fYear
2009
fDate
14-17 July 2009
Firstpage
791
Lastpage
796
Abstract
This paper presents an intelligent control scheme that uses an adaptive cerebellar model articulation controller (CMAC) in aircraft automatic landing system. The proposed intelligent controller can act as an experienced pilot and guide the aircraft to a safe landing in severe turbulence environment. Current flight control law is adopted in the intelligent design. Lyapunov theory is applied to obtain adaptive learning rule and stability analysis is also provided. Performance on tracking desired path and environment adaptive capability are demonstrated through software simulations.
Keywords
Lyapunov methods; adaptive systems; aircraft landing guidance; cerebellar model arithmetic computers; neurocontrollers; stability; Lyapunov theory; adaptive cerebellar model articulation controller; adaptive learning rule; aircraft automatic landing system; aircraft landing control; flight control law; intelligent control scheme; intelligent design; software simulations; stability analysis; Accidents; Adaptive control; Aerospace control; Aerospace safety; Aircraft; Automatic control; FAA; Intelligent control; Neural networks; Programmable control;
fLanguage
English
Publisher
ieee
Conference_Titel
Advanced Intelligent Mechatronics, 2009. AIM 2009. IEEE/ASME International Conference on
Conference_Location
Singapore
Print_ISBN
978-1-4244-2852-6
Type
conf
DOI
10.1109/AIM.2009.5229913
Filename
5229913
Link To Document