Wpływ zrzutu ładunków na dynamikę przestrzennego ruchu samolotu

Dynamics of spatial controlled and uncontrolled motion of an aeroplane is considered after release of loads. Complete nonlinear set of equations of motion is applied and initial conditions of motion of the aeroplane after the drop of loads are determined. A program for numerical integration of the equations of motion is developed making use of the Runge-Kutta-Gill method. A series of calculations have been performed. Their results demonstrate the effect of the release of loads on the motion of an aeroplane.