Control algorithms and capabilities of universal UAV

Abstract

The area of unmanned aerial vehicles (UAV) has been studied for a long time. They are actively used for military purposes. Nowadays, their application in everyday life to solve the problems of ordinary people has become relevant. There are many UAV designs, but the issue of an effective universal UAV design has not been fully addressed. In this paper, it is proposed to consider a variant of the universal UAV design, which differs from existing solutions and requires the development of its own rules for generating a PWM signal, control and stabilization algorithms, and the assessment of technical characteristics and application possibilities. The paper provides a brief description of the main differences of the proposed universal design from other solutions. It is proposed to consider the necessary control algorithms for UAVs of universal design, which were tested on the developed mathematical model of the UAV flight process of universal design. The basic equations of motion of this UAV are presented. The optimal technical characteristics and examples of using the electric version of the UAV of universal design to solve the problem of processing the field when powered by rechargeable batteries or an electric cable are considered.