30th Congress of the International Council of the Aeronautical Sciences

06 - Systems, Subsystems and Equipment

EXPERIMENTAL AND SIMULATION STUDY OF THE DYNAMICS OF AN ELECTRO-MECHANICAL LANDING GEAR ACTUATOR

G. Di Ritoš, R. Galatološ, F. Schettiniš; šUniversitā di Pisa - Dip. Ingegneria Civile ed Industriale, Italy

The paper deals with the study of an EMA for helicopter landing gear. The aim was to obtain an experimentally-validated model, to be used for design enhancement and development of similar systems. Experimental data, obtained by a specific hardware-in-the-loop rig capable of testing the EMA at different voltage supply and loads, are used to tune the EMA model parameters obtaining accurate results.


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