A simulation study of a helicopter in hover subjected to air blasts
Dariusz Król, Jarosław Gołaszewski · 2011
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.