DocumentCode :
3632128
Title :
Determination of the speed parameter of flight control system by using adaptif network based fuzzy inference system
Author :
Mehmet Konar;Aytekin Bagis
Author_Institution :
U?ak Elektrik-Elektronik B?l?m?, Sivil Havac?l?k Y?ksekokulu, Erciyes ?niversitesi, KAYSER?, Turkey
fYear :
2009
fDate :
4/1/2009 12:00:00 AM
Firstpage :
993
Lastpage :
996
Abstract :
Flight control parameters have a very important task for a safe and quality flight of the air vehicles. In this study, ANFIS is used for determination of the flight parameters. The system modelled by ANFIS for Boeing B-737-300 type planes has four inputs (height, temperature in Fahrenheit, angle of flaps, weight) and one output (flying speed). The simulation results are comparatively presented for the real results.
Keywords :
"Aerospace control","Fuzzy control","Fuzzy neural networks","Fuzzy systems","Vehicle safety","Temperature","Performance evaluation","Testing","Adaptive systems"
Publisher :
ieee
Conference_Titel :
Signal Processing and Communications Applications Conference, 2009. SIU 2009. IEEE 17th
ISSN :
2165-0608
Print_ISBN :
978-1-4244-4435-9
Type :
conf
DOI :
10.1109/SIU.2009.5136565
Filename :
5136565
Link To Document :
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