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Open AccessArticle10.32620/oikit.2024.102.09

ІННОВАЦІЙНІ ПІДХОДИ ДО ЗАПУСКУ ЛЕГКИХ БЕЗПІЛОТНИХ ЛІТАЛЬНИХ АПАРАТІВ МАЛОГО ТА СЕРЕДНЬОГО РАДІУСУ ДІЇ У РІЗНИХ УМОВАХ

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The subject of this study is the analysis of existing methods for launching unmanned aerial vehicles (UAVs) in modern conditions that require high precision, safety, and flexibility. The article discusses three main approaches: manual launch, launch from a launcher, and the use of catapults. The aim of the research is to assess the advantages and disadvantages of these methods, as well as to develop design solutions to improve the UAV launch process. Special attention is given to launching using catapults, as the most universal method for UAVs of different classes. In the course of the study, an analysis of the structural features of catapults is conducted, including systems that use pneumatic principles to provide the launch impulse and their ability to operate in rugged terrain. The paper examines the technical characteristics of modern catapults, which include the use of standardized components, the ability to adjust the launch angle, ensuring remote control, and enhancing operator

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The subject of this study is the analysis of existing methods for launching unmanned aerial vehicles (UAVs) in modern conditions that require high precision, safety, and flexibility. The article discusses three main approaches: manual launch, launch from a launcher, and the use of catapults. The aim of the research is to assess the advantages and disadvantages of these methods, as well as to develop design solutions to improve the UAV launch process. Special attention is given to launching using catapults, as the most universal method for UAVs of different classes. In the course of the study, an analysis of the structural features of catapults is conducted, including systems that use pneumatic principles to provide the launch impulse and their ability to operate in rugged terrain. The paper examines the technical characteristics of modern catapults, which include the use of standardized components, the ability to adjust the launch angle, ensuring remote control, and enhancing operator

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