Kim O. The technique to estimate the influence of light aircraft dynamic performances on a human perception of the atmospheric disturbances

The thesis is dedicated to investigation of light airplane dynamic performances influence on human perception of the atmospheric disturbances and to decrease of the influence on the flight safety level and comfort level, to development of the technique to estimate such influence. The complex mathematical model takes into account disturbed longitudinal motion of an airplane under the turbulent conditions, lift force direct control system operation and atmospheric disturbances perception by a human. The comfort criterion is developed considering the fundamental psychophysics laws. It can be used for estimation of comfort level for selection of airplane performances, modes of flight and processes of flight control.