About revising the computational dynamic scheme of an unmanned aerial vehicle based on the results of ground-based modal test operations in the aeroelasticity problems
The problem of revising the computational dynamic scheme of an unmanned aerial vehicle (UAV), based on the results of ground-based modal test operations, in order to study the UAV flutter and to assess the aeroelastic stability of an UAV with an automatic control system (ACS), is considered. It is n...
Main Author: | S. G. Parafes’ |
---|---|
Format: | Article |
Language: | Russian |
Published: |
Moscow State Technical University of Civil Aviation
2022-06-01
|
Series: | Научный вестник МГТУ ГА |
Subjects: | |
Online Access: | https://avia.mstuca.ru/jour/article/view/2023 |
Similar Items
-
RESEARCH FEATURES OF AEROELASTIC OSCILLATIONS OF UNMANNED AERIAL VEHICLES WITH ELECTRIC ACTUATOR OF RUDDERS
by: A. V. Bykov, et al.
Published: (2018-08-01) -
Maneuverable unmanned aerial vehicle "rudder - drive” system design for aeroelastic stability
by: V. N. Akimov, et al.
Published: (2019-08-01) -
MODEL OF STABILITY STUDY OF RUDDER ACTUATOR SYSTEM OF MANEUVERABLE UNMANNED AERIAL VEHICLE
by: S. G. Parafes’, et al.
Published: (2016-12-01) -
NONLINEAR MODEL OF STABILITY STUDY OF SYSTEM "SURFACE CONTROL – ACTUATOR" OF MANEUVERABLE UNMANNED AERIAL VEHICLE
by: V. N. Akimov, et al.
Published: (2018-01-01) -
FLIGHT DYNAMICS MODEL OF ONE CLASS OF AIRCRAFT WITH A VIEW OF ELASTIC CONSTRUCTION
by: A. I. Nikitin
Published: (2016-11-01)