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Calculation of the Height and Response Time of the Missile Initialization Device

https://doi.org/10.35596/1729-7648-2022-20-3-63-68

Abstract

The purpose of this article is to present a method for improving the accuracy of calculating the height and response time of the missile initialization device at a given height, as well as a method for its structural implementation. The paper considers a time option for calculating the response height. I**-t is based on measuring the height of the projectile's flight at five points equidistant in time, from which the negative increment in heights is calculated, a formula that describes the vertical component of the projectile flight is drawn, the numerical calculation of which allows us to determine the projectile response time at a given height. As a structural diagram of the device, it is proposed to use a homodyne structure, the main advantages of which are easiness to implement, a small number of components and, as a consequence, small dimensions.

About the Authors

S. S. Solonovich
Belarusian State University of Informatics and Radioelectronics
Belarus

Solonovich Sergey Sergeevich, Postgraduate at the Information Radiotechnologies Department

220013, Minsk, P. Brovka St., 6
tel. +375-29-187-68-36



I. I. Zabenkov
Belarusian State University of Informatics and Radioelectronics
Belarus

Zabenkov I.I., Professor at the Information Radiotechnologies Department

220013, Minsk, P. Brovka St., 6
tel. +375-29-187-68-36



D. V. Arkhipenkov
Belarusian State University of Informatics and Radioelectronics
Belarus

Arkhipenkov D.V., Postgraduate at the Information Radiotechnologies Department

220013, Minsk, P. Brovka St., 6
tel. +375-29-187-68-36



References

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2. Krivonos O.K., Ilyushchenko A.F., Petyushik E.E., Konoplyanik V.A. [The main directions of development of unguided aircraft missiles of the S-8 type]. Bulletin of the Military Academy of the Republic of Belarus. 2018;1(58):89-97. (In Russ.)

3. Nefyodov D.S., Milets A.F. [Experimental studies on assessing the flight speed of unguided aircraft missiles using a passive electrostatic location module]. Bulletin of the Military Academy of the Republic of Belarus. 2015;4(58):96-103. (In Russ.)

4. Zabenkov I.I., Solonovich S.S., Isakovich N.N., Zabenkov A.I. [Calculation and justification of the initialization criterion at a given altitude of the non-contact sensor of an aircraft with a response delay]. Bulletin of the Military Academy of the Republic of Belarus. 2019;2(63):71-78. (In Russ.)

5. Zabenkov I.I., Solonovich S.S. [The effect of auto-correction of the height of the fuse of a rocket projectile with a diving trajectory]. Science and military security. 2019;2(60):37-40. (In Russ.)


Review

For citations:


Solonovich S.S., Zabenkov I.I., Arkhipenkov D.V. Calculation of the Height and Response Time of the Missile Initialization Device. Doklady BGUIR. 2022;20(3):63-68. (In Russ.) https://doi.org/10.35596/1729-7648-2022-20-3-63-68

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ISSN 1729-7648 (Print)
ISSN 2708-0382 (Online)