Article 6421

Title of the article

OPTIMIZATION OF THE INFORMATION AND MEASUREMENT SYSTEM OF AN UNMANNED AIRCRAFT 

Authors

Aleksandr V. Poltavskiy, Doctor of technical sciences, leading researcher, V. A. Trapeznikov Institute of Management Problems of the Russian Academy of Sciences (65 Profsoyuznaya street, Moscow, Russia), E-mail: avp57avp@yandex.ru
Andrey A. Tyugashev, Doctor of technical sciences, associate professor, professor of the sub-department of computer technology, Samara State Technical University (244 Molodogvardeyskaya street, Samara, Russia), E-mail: tau797@mail.ru
Nikolay K. Yurkov, Doctor of technical sciences, professor, the honoured worker of science of the Russian Federation, head of the sub-department of radio equipment design and production, Penza State University (40 Krasnaya street, Penza, Russia), E-mail: yurkov_NK@mail.ru 

Index UDK

519.873 

DOI

10.21685/2307-4205-2021-4-6 

Abstract

Background. Today, there is another historical surge in the development of unmanned aerial vehicles and many models for unmanned aircraft systems. These developments are advanced in the field of unmanned aviation, they are rapidly changing their structure and appearance, as well as blocks for control and guidance systems with hardware and software for them, which are directly related to the performance of the main task. As a rule, the main blocks for the guidance systems links contain objects of information-measuring and control systems (IIUS), which are also an integral part of the automatic control system in the UAV. Materials and methods. The need to obtain an objective assessment for these systems, namely at the early stages of design, the solution of a number of tasks for analysis for the preparation of management decisions of the LPR, leads developers to a more complete account of their assessments with characteristics and parameters. It should be noted that in the press, scientific papers, etc., there is also a surge of interests and various approaches to solving such problems, in particular, on the choice of the structure and parameters of the IIUS. Each of these approaches and methods for evaluating object models for IIUS has its own advantages and disadvantages, at the same time, any such research should be supported by an experiment, usually computational. Unfortunately, there are few works among these methods and approaches, especially on the structuralparametric optimization of nonlinear, non-stationary and stochastic models of IIUS objects. Results and conclusions. This article considers one of the approaches to the solutions of structural-parametric optimization of object models for the information-measuring and control system of the IIUS as part of the units of the automatic control system of an unmanned aerial vehicle. The approach is based on the complex use of simulation (and computer) modeling algorithms for statistical synthesis and analysis of stochastic systems of variable structure. 

Key words

information design, modeling, system, technical level, complex of unmanned aerial vehicles, optimization, quality indicators, criteria 

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Дата создания: 16.02.2022 13:08
Дата обновления: 16.02.2022 13:40