F. Adamo, G. Andria, A. Di Nisio, C. G. C. Carducci, A. Lanzolla, Giuseppe Mattencini
{"title":"Development and characterization of a measurement instrumentation system for UAV components testing","authors":"F. Adamo, G. Andria, A. Di Nisio, C. G. C. Carducci, A. Lanzolla, Giuseppe Mattencini","doi":"10.1109/METROAEROSPACE.2017.7999596","DOIUrl":null,"url":null,"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.","PeriodicalId":229414,"journal":{"name":"2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","volume":"56 1","pages":"0"},"PeriodicalIF":0.0000,"publicationDate":"2017-06-01","publicationTypes":"Journal Article","fieldsOfStudy":null,"isOpenAccess":false,"openAccessPdf":"","citationCount":"5","resultStr":null,"platform":"Semanticscholar","paperid":null,"PeriodicalName":"2017 IEEE International Workshop on Metrology for AeroSpace (MetroAeroSpace)","FirstCategoryId":"1085","ListUrlMain":"https://doi.org/10.1109/METROAEROSPACE.2017.7999596","RegionNum":0,"RegionCategory":null,"ArticlePicture":[],"TitleCN":null,"AbstractTextCN":null,"PMCID":null,"EPubDate":"","PubModel":"","JCR":"","JCRName":"","Score":null,"Total":0}
引用次数: 5
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.