Abstract
This paper is devoted to the analysis of the existing eVTOL flying vehicles and consideration of the capabilities of the flight controller based on the STM32F722 microcontroller, as well as the evaluation of the characteristics of various sensors and devices and the study of their capabilities using the BetaFlight firmware. The main result of this work is the development of a prototype (prototype) of the flying transportation platform of the future, for which both hardware and software parts of the flying vehicle system have been developed and tested. Within the framework of the research there was created an interface between the flight controller based on STM32F722 and BetaFlight, worked out all technologies and systems for creating eVTOL-based flight vehicles. Also, comprehensive testing of the prototype system was performed and data transfer technologies were worked out. Functional and circuit diagrams of the prototype were also developed, as well as the simulation of mechanical-physical properties of the aircraft's frame reactions. An important result of this work is experimental research, the results of which show that the force structure is able to withstand the design loads. The results make it possible to improve the design of eVTOL aircraft and create more efficient data transfer systems. The results of the experimental studies show that the force structure is capable of withstanding the design loads.