In this research paper, trajectory following control of the quadrotor unmanned aerial vehicle (UAV) is carried out using the sliding mode controller (SMC) to control the position and attitude of the quadrotor, including the impact of disturbances. Due to their low cost, simplicity configuration of the structure, ability to hover, maneuverability, vertical take-off, and landing (VTOL) capability, and the ability to accomplished a variety of tasks, Quadrotor UAV has become an increasingly common research subject in recent years. The complex model of the quadrotor, including aerodynamic effects, was derived using Newton-Euler formalization. Here, SMC controllers were designed to track reference trajectories for the nonlinear model. The robustness and reliability of the controller are checked by applying external random disturbances to the quadrotor’s position and attitude. Finally, by using MATLAB /Simulink, the action of the quadrotor/quadcopter under the suggested control scheme has been implemented. The results show that all control system becomes stable and robust in terms of disturbance rejection.
Trajectory Tracking Control of Quadrotor Unmanned Aerial Vehicle Using Sliding Mode Controller with the Presence of Gaussian Disturbance
Lect.Notes Social.Inform.
International Conference on Advances of Science and Technology ; 2020 ; Bahir Dar, Ethiopia October 02, 2020 - October 04, 2020
15.07.2021
16 pages
Aufsatz/Kapitel (Buch)
Elektronische Ressource
Englisch
Quadrotor Unmanned Aerial Vehicle Trajectory Tracking Under Event-Triggered Sliding Mode Control
Springer Verlag | 2025
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