Calculation of the landing area for a small asymmetric martian probe under the action of the Magnus gyroscopic moment

The perturbed motion of a small descending asymmetric probe in the Martian atmosphere at arbitrary angles of attack is considered. The low-frequency nonlinear system of differential equations of probe motion relative to the center of mass is used. The aim of the work is to determine the size of the landing area of a small asymmetric probe to Mars under the action of the Magnus gyroscopic moment. It should be noted that numerical results of calculation of the probe landing area are obtained taking into account the moment of Magnus.