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
Link To Document :
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