Conrol Of He Laeral And Longitudinal Dynamics Of Autonomous Drone
Résumé: The research on autonomous miniature flying robots has intensified considerably thanks to the recent growth of civil and military interest in Unmanned Aerial Vehicles (UAV). This work is interested principally in dynamic modeling of the four rotor mini aircraft named as a quadrotor. The dynamical model is obtained by Newton-Euler methodology. Based on the mathematical model, linear and nonlinear control techniques are used to design and simulate robust controllers along this work. Proportional Derivative Control and the Backstepping algorithm methods have been elucidated and implemented in MATLAB and SIMULINK. Finally, simulation results are also provided in order to illustrate the performances of each controller.
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