期刊名称：Journal of Theoretical and Applied Information Technology
印刷版ISSN：1992-8645
电子版ISSN：1817-3195
出版年度：2021
卷号：99
期号：9
语种：English
出版社：Journal of Theoretical and Applied
摘要：The objective of this research study based on numerical results is to validate the feasibility and effectiveness of a new method for controlling Hexacopter type UAVs, which belong to the family of multirotor established on laws fractional control (FOC) and to establish a comparison between three types of controllers used to control the attitude of a UAV under different conditions, known as the Hexacopter platform, which is part of the multi-rotor UAV family. The three types of controllers considered in this work are a conventional linear-quadratic LQR controller, the proportional-integral-derivative PID method and a controller based on fractional control laws. The control method asserts advantages regarding of response time and stabilisation at the desired altitude and attitude. This control is intended to be used to control and maintain the desired trajectory during several manoeuvres while minimising energy consumption. The system's performance and stability are analysed with several tests, from simple hovering flight. This new solution applied to multi-rotor UAVs will totally revolutionise this technology in terms of stability and solve the problem for many industries. All the simulations discussed in this article were performed in the MATLAB/Simulink environment.
