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A robust control design approach for altitude control and trajectory tracking of a quadrotor
2021
Electrical Engineering & Electromechanics
Introduction. Unmanned aerial vehicles as quadcopters, twin rotors, fixed-wing crafts, and helicopters are being used in many applications these days. Control approaches applied on the quadrotor after decoupling the model or separate altitude control and trajectory tracking have been reported in the literature. A robust linear H∞ controller has been designed for both altitude control and circular trajectory tracking at the desired altitude. Problem. The ability of the quadrotor system to hover
doi:10.20998/2074-272x.2021.5.03
fatcat:ewljiccybjcjnpybufkggz4syq