Human pilot´s dynamic response characteristics

The article is dedicated for identifying a mathematical model which describes the ensemble "pilot-aircraft" as an integrated system, being pointed out the pilot´s particularities for aircraft command. In the paper are presented two compensatory models, based on the aircraft dynamics. Several approaches of the pilot models (transfer function gain, lead and lag time constants) were considered to choose the methodology that better predicts the airplane dynamic handling quality requirements. Numerical investigations have been performed using Maplesoft environment.