A benchtop test and certification system for motors and propellers assemblies of small and medium size UAVs (Unmanned Aerial Vehicles) is proposed in this work. In particular, the design and the development of a sensors head and an original embedded test system able to optimally characterize the electrical and the mechanical performances of UAV (voltage supplied to the motor, absorbed current, rotational speed, lift force produced by the propulsion subsystem, etc.) is here presented. Preliminary results relevant to data obtained from the test bench are illustrated.
Development and characterization of a measurement instrumentation system for UAV components testing / Adamo, Francesco; Andria, Gregorio; Di Nisio, Attilio; Guarnieri Calo' Carducci, Carlo; Lanzolla, Anna Maria Lucia; Mattencini, Giuseppe. - (2017), pp. 355-359. (Intervento presentato al convegno 4th IEEE International Workshop on Metrology for AeroSpace, MetroAeroSpace 2017 tenutosi a Padova, Italy nel June 21-23, 2017) [10.1109/MetroAeroSpace.2017.7999596].
Development and characterization of a measurement instrumentation system for UAV components testing
Adamo, Francesco;Andria, Gregorio;Di Nisio, Attilio;Guarnieri Calo' Carducci, Carlo;Lanzolla, Anna Maria Lucia;Mattencini, Giuseppe
2017-01-01
Abstract
A benchtop test and certification system for motors and propellers assemblies of small and medium size UAVs (Unmanned Aerial Vehicles) is proposed in this work. In particular, the design and the development of a sensors head and an original embedded test system able to optimally characterize the electrical and the mechanical performances of UAV (voltage supplied to the motor, absorbed current, rotational speed, lift force produced by the propulsion subsystem, etc.) is here presented. Preliminary results relevant to data obtained from the test bench are illustrated.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
