Математична модель руху автономного БПЛА літакового типу в режимі заходу на посадку

Abstract

The current research state in the field of autonomous landing of various categories aerodynamic objects, including aircraft-type UAVs, is characterized by different approaches to improving the procedures for controlling their air movement. One of the ways to increase the reliability of UAV operation is to create decision support systems at various stages of flight task execution. The objective of this study is to develop and validate the motion mathematical model of an autonomous fixed-wing UAV during the landing approach, which adequately reflects the dynamics of the process and provides a basis for constructing optimal automated landing algorithms.