Methods for investigating the unmanned aerial vehicle electric actuator performance in aeroelasticity tasks
- Авторы: Bykov A.V.1, Kondrashev G.V.1, Parafes’ S.G.1, Turkin I.K.1
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Учреждения:
- Moscow Aviation Institute
- Выпуск: Том 59, № 3 (2016)
- Страницы: 331-337
- Раздел: 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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Аннотация
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.
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Об авторах
A. Bykov
Moscow Aviation Institute
Автор, ответственный за переписку.
Email: a.bikov@mail.ru
Россия, Volokolamskoe shosse 4, Moscow, 125993
G. Kondrashev
Moscow Aviation Institute
Email: a.bikov@mail.ru
Россия, Volokolamskoe shosse 4, Moscow, 125993
S. Parafes’
Moscow Aviation Institute
Email: a.bikov@mail.ru
Россия, Volokolamskoe shosse 4, Moscow, 125993
I. Turkin
Moscow Aviation Institute
Email: a.bikov@mail.ru
Россия, Volokolamskoe shosse 4, Moscow, 125993
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