The article researches the character of the influence basic components of the main moment quantity movement shell, its spatial rotational motion in the air. It also conducts generalization of differential equations of mathematical model of the spatial rotational motion of the shells, with a gyroscopic stabilization by Lagrange equations of the second kind. Determined by analytical dependences for the generalized forces and the rotational kinetic energy of the shell.
mathematical model, the rotational motion of the shell, the overturning moment, the polar and equatorial damping moments, a moment Magnus, Lagrange equations of the second kind
"Matematychna model obertalnoho rukhu snariadiv z hiroskopichnoiu stabilizatsiieiu" [Mathematical model of rotational motion shells with gyroscopic stabilization],
Systems of Arms and Military Equipment,