Biodynamic Adverse Rotorcraft-Pilot Coupling

Abstract: This work discusses the dependence of helicopter aeroelastic stability on the pilot's biodynamic feedthrough. Two rotorcraft specific problems are presented. The modeling approach used in the investigation is briefly described, along with the experimental setup used for pilot biodynamic feedthrough characterization and for closed-loop problem investigation is described. The need to perform closed-loop experiments is discussed.

Keywords: Helicopter Pilot, Rotorcraft-Pilot Couplings, Biodynamic Feedthrough

DOI: 10.54941/ahfe100607

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