An Avionics System for Light-Weight Multi-Rotor Unmanned Aerial Vehicles
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Tarih
2023
Yazarlar
Dergi Başlığı
Dergi ISSN
Cilt Başlığı
Yayıncı
Institute of Electrical and Electronics Engineers Inc.
Erişim Hakkı
info:eu-repo/semantics/closedAccess
Özet
Small and light unmanned aerial vehicles (UAV) are increasingly used because of a wide variety of advantages they provide. These vehicles, which are especially preferred in applications such as 3D mapping, atmospheric measurements, and intelligent transportation systems, are at the heart of many researches due to their easy accessibility and ease of use. Moreover, the importance of these vehicles becomes even more evident in situations and locations where human intervention is not possible. However, their ability to perform these tasks in an ideal way reveals the necessity of a good avionics system. In particular, when it comes to autonomous flight, this becomes even more important. A properly designed avionics system is the first step for a UAV in flight to successfully accomplish its mission. In other words, the performance of the UAV is directly related to the functionality of the avionics. In this study, an avionics system is designed for a small and light-weight UAV, through careful consideration of the systems and components needed for autonomous flight, navigation, and communication. Within the scope of application areas, the system requirements for the UAV have been determined, and a design has been made in accordance with its capacity. © 2023 IEEE.
Açıklama
1st International Conference of Intelligent Methods, Systems and Applications, IMSA 2023 -- 15 July 2023 through 16 July 2023 -- Giza -- 192003
Anahtar Kelimeler
aircraft electrical system, automation, avionics, control, printed circuit board, small UAV
Kaynak
1st International Conference of Intelligent Methods, Systems and Applications, IMSA 2023
WoS Q Değeri
Scopus Q Değeri
N/A
