RESEARCH FEATURES OF AEROELASTIC OSCILLATIONS OF UNMANNED AERIAL VEHICLES WITH ELECTRIC ACTUATOR OF RUDDERS

Designing a modern flight vehicle is associated with the need to solve many scientific and technical problems. These tasks include the prevention of insecure self-oscillations in flight, taking into account the elasticity of the structure. These problems relate to dynamic aeroelasticity, a science t...

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Main Authors: A. V. Bykov, S. G. Parafes, V. I. Smyslov
Format: Artigo
Sprog:Russo
Udgivet: Moscow State Technical University of Civil Aviation 2018-08-01
Serier:Naučnyj Vestnik MGTU GA
Fag:
unmanned aerial vehicle (uav)
cross-shaped scheme
rudder
actuator
aeroelastic stability
flutter
laboratory experiment
self-oscillation
limit cycle
Online adgang:https://avia.mstuca.ru/jour/article/view/1330
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