MODEL OF STABILITY STUDY OF RUDDER ACTUATOR SYSTEM OF MANEUVERABLE UNMANNED AERIAL VEHICLE

One of the important problems of the designing of maneuverable unmanned aerial vehicles (UAV) is to ensure aeroelastic stability with automatic control system (ACS). One of the possible types of aeroelastic instability of UAV with ACS is loss of stability in the «rudder-actuator» system. To study th...

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Autores principales: S. G. Parafes’, D. N. Ivanov, A. S. Oparin
Formato: Artigo
Lenguaje:Russo
Publicado: Moscow State Technical University of Civil Aviation 2016-12-01
Colección:Naučnyj Vestnik MGTU GA
Materias:
unmanned aerial vehicle (uav)
rudder
actuator
aeroelastic stability
Acceso en línea:https://avia.mstuca.ru/jour/article/view/888
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