CONTROL POR PLANOS DESLIZANTES DIFUSOS DE UN HELICÓPTERO CON UN GRADO DE LIBERTAD Sliding Mode Fuzzy Control of a Helicopter with One Degree of Freedom

This article presents an implementation of a fuzzy control as sliding control of the helicopter academic model. The performance test has temporal perturbations. The advantage of the implemented control is that it does not need a prior knowledge of the complete mathematical model of the plant.

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