The problems of criteria for the objects state reasonable choice, taking into account the external and internal disturbances action, are considered. The main problems of the functioning of UAV-type objects are given. Damages classifications and such damages manifestations are considered. Aircraft and rotary type UAVs mathematical models have been developed. Damage indicators have been studied; the most significant indicators have been selected. Approaches to the reliability indicators, risks, residual service life assessment based on forecasting methods within the framework of data mining approaches are proposed. Alternative approaches to assessing reliability by various indicators are shown.
REFERENCES
1.
Romanova
I.K.
Modern approaches to detecting changes in shape and other damage to flight vehicle during movement
. AIP Conference Proceedings
2318
, 110001
(2021
); 2.
Romanova
I.K.
Study of the influence of deformations and asymmetry on aircraft movement parameters/
AIP Conference Proceedings
2171
, 130001
(2019
); 3.
Romanova
I.K.
Modeling of motion stability of deformed elongated bodies based on variations of roll angular velocities
. Proceedings of SPIIRAS.
Issue 18
(3
), 2019
.4.
Malysheva
G.V.
, Romanova
I.K.
optimization of the choice of parameters characterizing the state of the object when solving reliability problems
. REPAIR. RECOVERY. MODERNIZATION.
Number: 6 Year: 2015
. Pages: 33
–38
5.
Romanova
I.K.
PARETO OPTIMAL SOLUTIONS AND THEIR APPLICATION IN DESIGNING ROBOTS AND ROBOTIC SYSTEMS. STUDIES IN SYSTEMS, DECISION AND CONTROL
: Springer Nature
Switzerland
. 272
: 2020
. Pp: 25
–39
6.
Sun
H.
, Yu
J
, Siyu
Zhang
S. The Control of Asymmetric Rolling Missiles Based on Improved Trajectory Linearization Control Method
//J. Aerosp. Technol. Manag., São José dos Campos
, Vol. 8
, No 3
, pp. 319
–327
, Jul.-Sep., 2016
7.
Abbas
L.K.
, Chen
D.
, Rui
X.
Numerical Calculation of Effect of Elastic Deformation on Aerodynamic Characteristics of a Rocket
. Hindawi Publishing Corporation
International Journal of Aerospace Engineering Volume 2014
, Article ID 478534, 11
p.8.
Dongyang
C.
, Abbas
L.K.
, Xiaoting
R.
Numerical simulation of a spinning stabilized projectile aerodynamic characteristics effected by structure errors
// Acta Aerodynamica Sinica
32
(5
):705
–711
. October 2014
. DOI: 9.
Ogunwa
T.
, Abdullah
E.J.
Flight dynamics and control modelling of damaged asymmetric aircraft
//Article (PDF Available) · October 2016
. DOI: 10.
Nguyen
N.
, Krishnakumar
K.
, Kaneshige
J.
Dynamics and Adaptive Control for Stability Recovery of Damaged Asymmetric Aircraft
// NASA Ames Research Center, Moffett Field, CA 94035. University of California
, Davis, CA 95616
11.
Dykes
J.W.
Projectile linear theory for aerodynamically asymmetric projectiles
// Georgia Institute of Technology. December
2011
12.
Hodges
D.
A New Approach to Aeroelastic Response, Stability and Loads of Missiles and Projectiles.
Final Report, U.S. Army Research Office Grant 40448-EG. 15 July 2015
[Electronic resource]. – Access mode http://www.researchgate.net/publication/235079207 (date of access: 01/28/2019)13.
Yi
W.
, Sun
D.
, Tan
J.
, Yuan
D.
Experimental research on aeroelasticity of a large length to diameter ratio projectile
. Fourth International Symposium on Physics of Fluids (ISPF4) International Journal of Modern Physics: Conference Series
Vol. 19
(2012
) p. 270
–275
14.
Tihomirov
D.
, Raveh
D.
Nonlinear Aerodynamic Effects on Static Aeroelasticity of Flexible Missiles
// Conference: AIAA Scitech 2019
. Conference Paper. January 2019. DOI: 15.
Kitson
R.C.
, Cesnik
C.E.S.
Multidisciplinary Effects on High-Speed Vehicle Performance and Stability
// Conference: 2018 AIAA/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Conference Paper
. January 2018
. DOI: 16.
Kiran
K.
, Cholleti
R.
Static Aeroelastic Analysis on Two Stage Rocket Body
// International Journal of Engineering Research & Technology (IJERT)
. ISSN: 2278-0181. November 2015
. Vol. 4
. Issue 11
.17.
Dongyang
C.
, Abbas
L.K.
, Xiaoting
R.
, Guoping
W.
Aerodynamic and static aeroelastic computations of a slender rocket with all-movable canard surface
// First Published June 12, 2017 Research Article. 18.
RuHao
H
, Zheng
Y.Y.
, Lei
Y.
Effect of elastic deformation on flight dynamics of projectiles with large slenderness ratio
//Aerospace Science and Technology.
September 2017
. DOI: 19.
Brejão
L.F.
, Manoel
R.
A 2-DOF model of an elastic rocket structure excited by a follower force
// XVIII Brazilian Colloquium on Orbital Dynamics (2016). IOP Conf. Series: Journal of Physics: Conf. Series
911
(2017
) 012020
doi: 20.
Mokin
YU.A.
Vliyanie malyh uglov ataki i skol’zheniya na moment krena pri giperzvukovom obtekanii tel vrashcheniya
// Teplofizika i aehromekhanika.
2009
. tom 16
. № 1
. (In Russ.)21.
Komissarenko
A. I.
, Maksimov
F. A.
Osobennosti dinamiki poleta tela pri nalichii asimmetrij // XL Akademicheskie chteniya po kosmonavtike, posvyashchennye pamyati akademika S.P. Korolyova i drugih vydayushchihsya otechestvennyh uchenyh – pionerov osvoeniya kosmicheskogo prostranstva: sbornik tezisov
. M.:MGTU im. N.EH. Baumana
. 2015
.22.
Fresconi
F.
, Guidos
B.
, Celmins
I.
, Hathaway
W.
Flight Behavior of an Asymmetric Body through Spark Range Experiments using Roll-Yaw Resonance for Yaw Enhancement
// AIAA Atmospheric Flight Mechanics Conference
San Diego, California
, USA
. AIAA SciTech Forum. January 2016
. (AIAA 2016-0782). 23.
Tong
L.
, Ji
H.
Multi-body dynamic modelling and flight control for an asymmetric variable sweep morphing UAV
// The Aeronautical Journal
June 2014
Volume 118
No 1204
24.
Jamie
Coble
and J. Wesley
Hines
. Dentifying Optimal Prognostic Parameters from Data: A Genetic Algorithms Approach
. Annual Conference of the Prognostics and Health Management Society
, 2009
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