DocumentCode :
3644562
Title :
A simulation study of a helicopter in hover subjected to air blasts
Author :
Dariusz Król;Jarosław Gołaszewski
Author_Institution :
Institute of Informatics, Wroclaw University of Technology, Poland
fYear :
2011
Firstpage :
2387
Lastpage :
2392
Abstract :
This paper discusses the performance of a tuned fuzzy regulator applied to control a single-rotor PZL Kania helicopter. Based on the results of numerical simulation of the helicopter in hover when subjected to longitudinal, lateral and diagonal air blasts, the effectiveness of the proposed solution is successfully confirmed by calculated mean squared error values.
Keywords :
"Helicopters","Regulators","Atmospheric modeling","Angular velocity","Damping","Vectors","Accuracy"
Publisher :
ieee
Conference_Titel :
Systems, Man, and Cybernetics (SMC), 2011 IEEE International Conference on
ISSN :
1062-922X
Print_ISBN :
978-1-4577-0652-3
Type :
conf
DOI :
10.1109/ICSMC.2011.6084035
Filename :
6084035
Link To Document :
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