Development of a control system for multiple unmanned aerial vehicles
Background. The study considers the problem associated with the development of a control system for many unmanned aerial vehicles. An analysis of the possibilities of improving the efficiency of control of unmanned aerial vehicle systems is carried out. The role of classification methods in the rati...
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| Main Authors: | , , |
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| Format: | Article |
| Language: | English |
| Published: |
Science and Innovation Center Publishing House
2025-06-01
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| Series: | International Journal of Advanced Studies |
| Subjects: | |
| Online Access: | https://ijournal-as.com/jour/index.php/ijas/article/view/358 |
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| Summary: | Background. The study considers the problem associated with the development of a control system for many unmanned aerial vehicles. An analysis of the possibilities of improving the efficiency of control of unmanned aerial vehicle systems is carried out. The role of classification methods in the rating assessment of the system of flying objects is shown. The structure of interaction between the control center and a set of unmanned aerial vehicles is presented. A description of approaches related to the assignment of a rating is given. The control center maintains monitoring of the efficiency of the functioning of aircraft. It is shown how the various stages of rating management of a set of unmanned aerial vehicles are interconnected. The general integral assessment has an impact on the partial integral assessment. If the rating of the aircraft coincides with the maximum integral score, it will be considered as having the highest rating.
Purpose. Development of a system on the basis of which many unmanned aerial vehicles are controlled.
Materials and methods. The main research methods are related to the use of set theory, rating approaches and expert methods.
Results. In this paper, the basic principles and features of the formation of a control system for a set of unmanned aerial vehicles are considered in detail. Depending on the initial conditions, you must specify the parameters that should be taken into account in the model. The results of the work can be used for a wide range of unmanned aerial vehicles.
EDN: ZAYLET |
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| ISSN: | 2328-1391 2227-930X |