Akademik Veri Yönetim Sistemi
Advanced in Engineering Research, Victoria M. Petrova, Editör, Nova Publisher, New York, ss.137-164, 2022
In
this study, a non-standard multicopter design, production and control was
carried out, which can be used both for educational purposes and in many
fields. The multicopter system, designed in a universal structure, allows the
formation of multicopter models with different rotor numbers by changing only
one parameter in software. The solid model of the system was created in the
computer aided design program as the first stage, and the simulation was
carried out in the computer environment. The simulations were carried out for
two cases, where no disturbance effect was applied and disturbance effect was
applied to the mass centers of the vehicles, and the performances of the system
were examined. The results obtained in autonomous flight simulations were obtained
both graphically and numerically. As the second stage, this tool was produced
in accordance with the solid model obtained by the computer aided design
program. The real flight tests of the system, which was made ready for flight,
were carried out for three drone models. In the flight tests, both graphical
and numerical results were obtained and the performances of the drone models
were compared. As a result of both simulation and experimental studies, an
increasing flight performance with the number of rotors has been observed. In
addition, it has been seen that different configurations can be applied on a
single platform thanks to its universal structure.