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