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

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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Bibliographic Details
Main Authors: S. G. Parafes’, D. N. Ivanov, A. S. Oparin
Format: Article
Language:Russian
Published: Moscow State Technical University of Civil Aviation 2016-12-01
Series:Naučnyj Vestnik MGTU GA
Subjects:
unmanned aerial vehicle (uav)
rudder
actuator
aeroelastic stability
Online Access:https://avia.mstuca.ru/jour/article/view/888

Internet

https://avia.mstuca.ru/jour/article/view/888

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