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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Bibliografische Detailangaben

Hauptverfasser:	A. V. Bykov, S. G. Parafes, V. I. Smyslov
Format:	Artigo
Sprache:	Russo
Veröffentlicht:	Moscow State Technical University of Civil Aviation 2018-08-01
Schriftenreihe:	Научный вестник МГТУ ГА
Schlagworte:	unmanned aerial vehicle (uav) cross-shaped scheme rudder actuator aeroelastic stability flutter laboratory experiment self-oscillation limit cycle
Online-Zugang:	https://avia.mstuca.ru/jour/article/view/1330
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