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.
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Original Russian Text © A.V. Bykov, G.V. Kondrashev, S.G. Parafes’, I.K. Turkin, 2016, published in Izvestiya Vysshikh Uchebnykh Zavedenii, Aviatsionnaya Tekhnika, 2016, No. 3, pp. 34–39.
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Bykov, A.V., Kondrashev, G.V., Parafes’, S.G. et al. Methods for investigating the unmanned aerial vehicle electric actuator performance in aeroelasticity tasks. Russ. Aeronaut. 59, 331–337 (2016). https://doi.org/10.3103/S1068799816030065
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DOI: https://doi.org/10.3103/S1068799816030065