Modeling, Identification and Control of a Quadrotor Aircraft
Thepresentworkreferstothemathematicalmodeling,experimentalidentificationandcontroldesignofasmallunmannedindoorsquadrotoraircraft,atlowtranslationalspeedsaroundthehoveringcondition,wheretheaerodynamicforcesontheairframearedisregarded.AKalmanfilterisimplementedforstateestimationandnoisefi
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