Methods for investigating the unmanned aerial vehicle electric actuator performance in aeroelasticity tasks

A. V. Bykov; G. V. Kondrashev; S. G. Parafes’; I. K. Turkin

doi:10.3103/S1068799816030065

Methods for investigating the unmanned aerial vehicle electric actuator performance in aeroelasticity tasks

作者: Bykov A.V.¹, Kondrashev G.V.¹, Parafes’ S.G.¹, Turkin I.K.¹
隶属关系:
1. Moscow Aviation Institute
期: 卷 59, 编号 3 (2016)
页面: 331-337
栏目: Flight Dynamics and Control of Flight Vehicles
URL: https://journals.rcsi.science/1068-7998/article/view/229748
DOI: https://doi.org/10.3103/S1068799816030065
ID: 229748

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详细

Theoretical and experimental methods of investigating the performance of an electric actuator of maneuverable unmanned aerial vehicle (UAV) is considered in order to solve the aeroelasticity tasks. Models of the stability analysis for the rudder–actuator system as well as the examples of numerical and experimental studies of this system performance are given.