Currently, the drone is used in many situations where a manned flight is considered difficult, too risky, or in some cases impossible. In recent years, drones (drones) have become very popular due to their ease of use and their versatility. The urgency of the task of synthesis of control systems for unmanned aerial vehicles is characterized by the complexity of their mathematical model and a large number of experimentally determined parameters. This article proposes a methodology for designing a model of a regulatory system with a fuzzy logical controller. The results of simulation of a system with a fuzzy logic controller are presented.

Keywords: quadrotor, UAV, fuzzy-logical control, dynamics, roll, pitch, Yaw