Email this article Methods for investigating the unmanned aerial vehicle electric actuator performance in aeroelasticity tasks
- Authors: Bykov A.V.1, Kondrashev G.V.1, Parafes’ S.G.1, Turkin I.K.1
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Affiliations:
- Moscow Aviation Institute
- Issue: Vol 59, No 3 (2016)
- Pages: 331-337
- Section: Flight Dynamics and Control of Flight Vehicles
- URL: https://journal-vniispk.ru/1068-7998/article/view/229748
- DOI: https://doi.org/10.3103/S1068799816030065
- ID: 229748
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Abstract
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.
About the authors
A. V. Bykov
Moscow Aviation Institute
Author for correspondence.
Email: a.bikov@mail.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
G. V. Kondrashev
Moscow Aviation Institute
Email: a.bikov@mail.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
S. G. Parafes’
Moscow Aviation Institute
Email: a.bikov@mail.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
I. K. Turkin
Moscow Aviation Institute
Email: a.bikov@mail.ru
Russian Federation, Volokolamskoe shosse 4, Moscow, 125993
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