Analysis of Dynamics of Angular Motion of Uncontrollable Flying Vehicle Using Methods of Qualitative Theory of Systems

Dynamics of an angular motion of a flying vehicle is analyzed qualitatively from the point of view of a motion of a dynamical system considering the influence of various asymmetries and eccentricities of thrust. It is shown that the availability of various eccentricities of thrust and small asymmetries not only changes the angle of attack value in resonant modes of the flying vehicle motion but also induces the formation of critical points.