SCHEMO-TECHNICAL SOLUTIONS FOR DESIGNING NATIONAL FLIGHT CARDS FOR UAVS

Abstract

The control system based on the STM32 microcontroller is analyzed in detail on the specific example presented in the article. In this system, the integration of components such as IMU, GPS module, barometer and magnetometer is explained. Aspects such as system architecture and control implementation, PID controller, and sensor data fusion are emphasized. Real-time flight path optimization with machine learning algorithm and ability to adapt to environmental information is explained. General information about unmanned aerial vehicles is given, the main features and parameters of STM32F405 and STM32F722 flight control cards are shown. The basic principles of designing national flight cards used for reconnaissance UAV were reviewed. In addition, the analysis and research of the applied control systems of unmanned aerial vehicles (UAVs) is discussed. Basic components of control systems, sensor integration and flight control algorithms are explored.