The complex problem about parameters choice of general aviation airplane flying with low speed is considered with the purpose to improve passengers comfort during flight in conditions of turbulence. As a model the system of differential equations of first order is used. It describes the longitudinal motion of an airplane in turbulent atmosphere with application of lift force direct control system and acceleration loads perception by human organism. For the problem solution the results of aerodynamic performances calculations obtained by the author in his previous works are used.

Матеріали VIII міжнародної науково-технічної конференції "ABІА-2007", 25-27 квітня 2007 року [Текст] / Бабак В.П., гол. оргком.; Національний авіаційний університет. — Київ, 2007.