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Система многоуровневой импульсной коррекции

Инженерный журнал: наука и инновации

# 3·2016 13

A system of multi-level impulse correction

©

Yu.V. Velikiy, A.N. Klishin

Bauman Moscow State Technical University, Moscow, 105005, Russia

Current political situation and counter-terrorist measures lead to the majority of warfare

being carried out locally, and, as a rule, in densely populated areas. This trend formed

the grounds for developing new artillery and mortar systems and updating older ones

with guided munitions. The necessity of employing guided munitions, in its turn, is due to

high mobility of contemporary weapon systems and improvements in their protection.

Given that artillery and mortar munitions are small in size and have to be well-suited for

mass production, be simple in design and boast low production costs, their guidance sys-

tem should be cheap, simple, reliable and at the same time able to ensure high efficiency

of target defeat. The article deals with the problem of defeating a target with a given ac-

curacy in the case of insufficient prior information on its actual position. It must be noted

that an impulse correction system features a fixed value of the correction push, which

leads to the issues of “under-“ or “over-correction”. We suggest introducing a multi-

level correction system to solve this non-trivial problem, employing correction engines of

varied thrust.

Keywords:

guided munition, impulse correction system, multi-impulse correction, correc-

tion engines.

REFERENCES

[1]

Kazakovtsev V.P., Zhileykin V.D.

Obrabotka strelb: Metodicheskie ukazaniya k

laboratornym rabotam

[Processing shooting data: laboratory work guidelines].

Moscow, BMSTU Publ., 2009

[2]

Benevolskiy S.B., Burlov V.V., Kazakovtsev V.P.

Ballistika: Uchebnik dlya

kursantov i slushateley GRAU

[Ballistics: a textbook for students and cadets of

the Main Missile and Artillery Directorate]. Lysenko L.H., ed. Penza, Penza

Artillery Engineering Institute Publ., 2005.

[3]

Platunova A.V., Klishin A.N., Ilyukhin S.N. Osnovy adaptivnogo upravleniya

vysokotochnymi letatelnymi apparatami [Basic aspects of adaptive control of

precision-guided airborne devices].

Materialy XXXIX akademicheskikh chteniy

po kosmonavtike

[Proc. of the 39

th

Academic Lections on Cosmonautics].

Moscow, BMSTU Publ., 2015, pp. 333–334.

[4]

Lysenko L.N.

Navedenie i navigatsiya ballisticheskikh raket

[Guidance and

navigation for ballistic missiles]. Moscow, BMSTU Publ., 2007, 672 p.

[5]

Lebedev A.A., Karabanov V.A.

Dinamika sistem upravleniya bespilotnymi

letatelnymi apparatami

[Guidance system dynamics for unmanned aircraft].

Moscow, Mashinostroenie Publ., 1965.

[6]

Dmitrievskiy A.A., Lysenko L.N., Ivanov N.M. et al.

Ballistika i navigatsiya

raket

[Ballistics and navigation for rockets]. Moscow, Mashinostroenie Publ.,

1985.

[7]

Volkov E.A.

Chislennye metody: ucheb.posobie

[Numerical techniques: a

workbook]. 5th edition. Saint Petersburg, Lan Publ., 2008.

[8]

Sikharulidze Yu.G.

Ballistika letatelnykh apparatov

[Aircraft ballistics].

Moscow, Nauka Publ., 1982.