NONLINEAR MODEL OF STABILITY STUDY OF SYSTEM "SURFACE CONTROL – ACTUATOR" 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 system "surface control – actuat...

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Bibliografske podrobnosti
Main Authors: V. N. Akimov, D. N. Ivanov, A. S. Oparin, S. G. Parafes’
Format: Artigo
Jezik:Russo
Izdano: Moscow State Technical University of Civil Aviation 2018-01-01
Serija:Naučnyj Vestnik MGTU GA
Teme:
unmanned aerial vehicle (uav)
surface control
electric actuator
aeroelastic stability
system "surface control – actuator"
nonlinear model
Online dostop:https://avia.mstuca.ru/jour/article/view/1164
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