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Inertial aircraft guidance method, taking into account the inconsistencies of dynamic properties of the target and interceptor

DOI 10.18127/j20700814-201901-01

Keywords:

V.I. Merkulov – Dr.Sc.(Eng.), Professor, Deputy General Product Engineer, JSC «Corporation «Vega» (Moscow)
E-mail: from_fn@mail.ru
D.I. Ievlev – Engineer, JSC «Corporation «Vega» (Moscow)
E-mail: idi.96@mail.ru


The process of intercepting an air target is the result of the interaction of various subsystems that make up a single information and control chain, the beginning of which is the target, and the final link is the combat part that causes the defeat of the target. The degree to which all subsystems are consistent in terms of dynamics, characterizing their ability to respond to changes in input signals, depends on the perfection of the guidance system as a whole. However, it is not possible to solve this problem by technological means within the framework of modern unified production. In this regard, the problem of accounting for these inconsistencies by algorithmic methods is very urgent.
The article describes the synthesis of such an algorithm on the example of the formation of the guidance method, taking into account the discrepancy between the dynamic properties of the target and the interceptor. The study of the obtained method of guidance and analysis of the results.

References:
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June 24, 2020
May 29, 2020

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