Helmi Abrougui, S. Nejim, Anis Charrada, Habib Dallagi
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Sliding Mode Control for Hexacopter Autopilot design
This paper proposes an approach for modeling and controlling the attitude of a hexacopter. An autopilot is designed using sliding mode control. It consists of a low-level controller for attitude stabilization and a high-level controller for position tracking control. Simulations are carried out to show the effectiveness of the designed autopilot.
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