31th Congress of the International Council of the Aeronautical Sciences

07 - Systems, Subsystems and Equipment


H.C. Moura¹, G.S.P. Alegre¹, J.H. Bidinotto¹, E.M. Belo¹; ¹University of São Paulo, Engineering School of São Carlos, Brazil

The present work proposes to investigate the relation between the longitudinal dynamics of Fly-by-Wire aircrafts and the resultant susceptibility to the Pilot Induced Oscillation phenomena. Different values of the stability derivatives will be simulated in software implementations with multiple theoretical pilot models. It is expected of these trials a range of values of the derivatives that must be avoided in future aircraft designs to minimize its occurrence.

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