Paper Contents
Abstract
This system presents animplementation of gyroscope-based control and stabilization systems for unmanned aerial mini-vehicles (mini-UAVs), focusing on the use of a compact gyroscope with three degrees of freedom. The gyroscope serves as the primary reference frame for the UAVs navigation system, enabling precise orientation and attitude control. A control algorithm is developed to generate corrective control moments based on gyroscopic input, which in turn determines the deflection angles of the UAVs control surfaces. This mechanism allows the vehicle to maintain stable flight, respond to disturbances, and perform controlled maneuvers. A mini autopilot system is integrated to ensure that the UAVs longitudinal axis remains aligned with the gyroscopes reference axis, enhancing flight accuracy and stability. The project also explores both remote and pre-programmed navigation modes, evaluating system performance under various conditions. Furthermore, considerations of structural integrity, response durability, and overall system reliability are addressed, demonstrating the effectiveness of gyroscopic stabilization in improving UAV flight performance, especially in dynamic or unpredictable environments.
Copyright
Copyright © 2025 SUBIN RAJ M. This is an open access article distributed under the Creative Commons Attribution License.
