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This works deals with the problem to stabilize a Quad rotor-UAV in presence of time-delay and disturbances. The proposed controller is based on the reduction approach, i.e. the system transformation into one without delay which might be stabilized using a regular controller. Mathematical induction method allows to develop a new transformation based on the fundamental theorem of calculus. A closed-loop...
A Sliding Mode Control (SMC) is modified in order to address the input delay in the control of quadrotor educational platform. The proposed scheme uses a predictor that compensates the delay effect on the input control which can appear for example when the control law is computed in a ground station. A Lyapunov stability analysis is presented to prove the exponential closed-loop stability in presence...
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