Analysis and Simulation of Route Trajectory Option for Aircraft-Type Drones

Abstract

In the course of this work, an analysis of typical route trajectories of aircraft-type drones was carried out, with the help of which it was revealed that, regardless of the type of tasks performed, the trajectories consist of certain sections that can be described in spatio-temporal parameters. The mathematical description and programming options for these sections were considered, taking into account the fact that all typical trajectories can be considered as closed curvilinear contours described in three-dimensional space. In the MatLab environment, a data generation program for navigation drone navigation and motion control, an algorithm and a program for determining the current coordinates and ground speed components were developed and tested. The obtained results are supposed to be used in flight preparation and in flight control of drones.