DocumentCode
2359422
Title
Automatic landing control using particle swarm optimization
Author
Juang, Jih-Gau ; Lin, Bo-Shian ; Chin, Kuo-Chih
Author_Institution
Dept. of Commun. & Guidance Eng., Nat. Taiwan Ocean Univ., Keelung, Taiwan
fYear
2005
fDate
10-12 July 2005
Firstpage
721
Lastpage
726
Abstract
This paper proposes an intelligent aircraft automatic landing controller that uses fuzzy-neural controller with particle swarm optimization to improve the performance of conventional automatic landing system. Control gains are selected by a parameter searching method called particle swarm theory. Comparisons on different control schemes are given. Simulation results show that the proposed automatic landing controller can successfully expand the safety envelope of an aircraft to include severe wind disturbance environments without using the conventional gain scheduling technique.
Keywords
aircraft; control system analysis; evolutionary computation; fuzzy control; neurocontrollers; automatic landing control; fuzzy-neural controller; intelligent aircraft control; parameter searching method; particle swarm optimization; Adaptive control; Aerospace control; Aircraft; Airplanes; Automatic control; Control systems; Intelligent networks; Optimal control; Particle swarm optimization; Robust control;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics, 2005. ICM '05. IEEE International Conference on
Conference_Location
Taipei
Print_ISBN
0-7803-8998-0
Type
conf
DOI
10.1109/ICMECH.2005.1529350
Filename
1529350
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