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Построение многоцелевой системы крылатых ракет…

Инженерный журнал: наука и инновации

# 10·2017 13

Constructing a multipurpose system of cruise missiles

within the conditions of multifactorial uncertainty

© V.M. Balyk

1

, A.A. Malenkov

1

, V.S. Petrovskiy

2

, A.S. Stanchenko

1

1

Moscow Aviation Institute (National Research University), Moscow, 125993, Russia

2

Joint stock company Military and industrial corporation NPO Mashinostroyenia,

Reutov, Moscow region, 143966, Russia

The article considers the problem of constructing a system of cruise missiles resistant to

the change of the external target environment. We have formulated a criterion of stability

that allows selecting such design decisions which increase the feasibility of accomplish-

ing the target by the system. Our work defines the statistical functional interconnection

between the optimality criterion and the design decision, which provides an opportunity

for finding a reasonable stable design decision. We introduce a criterion of the design

decision immunity to the multifactorial uncertainty that is dependent on the impact of the

uncontrolled factors related to the target. A large variety of such factors, different nature

of their origin and the incompleteness of knowledge of their laws dictate the need for

considering the multifactorial uncertainty from more common positions connected with

the notion of the design decision immunity to the perturbing factors. As the criterion of

immunity we examine a regularity criterion written in relation to the Lipschitz constant

characterizing the degree of the criterion scores immunity to the variations of the multi-

factorial uncertainty.

Keywords:

cruise missile, optimal target allocation, multifactorial uncertainty, functional

stability

REFERENCES

[1]

Ilyukhin I.M., Kostylev N.M.

Inzhenernyy zhurnal: nauka i innovatsii — Engi-

neering journal: science and innovation,

2013, iss. 9. Available at: http://

engjournal.ru/catalog/pribor/optica/919.html

(accessed August 4, 2017).

[2]

Kureychik V.M.

Izvestiya Rossiiskoy Akademii nauk.

Teoriya i sistemy uprav-

leniya — Journal of Computer and Systems Sciences International,

1999, no. 1,

pp. 144–160.

[3]

Ivakhnenko A.G.

Induktivnyy metod samoorganizatsii modeley slozhnykh system

[Induction method of complicated systems models self-ogranization]. Kyiv,

Naukova dumka Publ., 1981, 296 p.

[4]

Abgaryan K.A., Rapoport I.M.

Dinamika raket

[Missile dynamics]. Moscow,

Mashinostroenie Publ., 1969, 378 p.

[5]

Tikhonov A.N., Arsenin V.Ya.

Metody resheniya nekorrektnykh zadach

[Meth-

ods for solving ill-conditioned problems]. Moscow, Nauka Publ., 1979, 285 p.

[6]

Samarskiy A.A., Vabishevich P.N.

Chislennye metody resheniya obratnykh

zadach matematicheskoy fiziki

[Numerical computations of inverse problems in

mathematical physics]. Moscow, URRS Publ., 2007, 478 p.

[7]

Balyk V.M., Kalutskiy N.S.

Vestnik Moskovskogo aviatsionnogo instituta —

Bulletin of Moscow Aviation Institute,

2008, vol.15, no. 1, pp. 29–36.

[8]

Balyk V.M., Vedenkov K.V., Kulakova R.D.

Vestnik Moskovskogo aviatsion-

nogo instituta — Bulletin of Moscow Aviation Institute,

2014, vol. 21, no. 4,

pp. 49–58.