ТЕХНІЧНІ АСПЕКТИ РЕАЛІЗАЦІЇ АПАРАТНО-ПРОГРАМНОГО КОМПЛЕКСУ ДЛЯ ТЕСТУВАННЯ FPV ДРОНІВ МУЛЬТИРОТОРНОГО ТИПУ

Abstract

This article is devoted to the development of a hardware and software complex (HMC) for testing multi-rotor FPV drones. The main goal of the study was to create an effective tool for assessing the dynamic characteristics of drones, including the analysis of torque, angular acceleration and stability of the control system. The complex is based on a three-axis gimbal equipped with high-precision measuring equipment, including optical encoders and a MinIMU-9 inertial unit. The article describes the design features of the suspension, including its modular architecture, vibration minimization and measurement accuracy. The proposed solutions made it possible to test drones in conditions close to real operating conditions, including the impact of vibrations, wind and other external factors. HMC software collects and processes data, simulates ideal trajectories, and automatically adjusts control parameters. The synchronization of the gimbal, sensors and control computer ensures high measurement accuracy and allows for early detection of possible defects. The results confirmed the effectiveness of the developed complex for testing FPV drones, making it a promising tool for improving the reliability and efficiency of these devices in various applications, including combat missions.