Abstract: The quadrotor is known for its mechanical simplicity. However, the control mechanism is complex due to six degree of freedom i.e. X, Y and Z axis that represent the motion control of ...
Abstract: In this letter, we propose a multivariable disturbance observer-based finite-time sliding mode attitude control (MDOB-FT-SM-AC) for fixed-wing UAVs in the presence of both matched and ...
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