The article covers the study of the characteristics of the longitudinal motion of a guided aviation bomb by numerical simulation to determine the parameters of stabilization and control in order to ensure more effective implementation of modern programs for development and modernization of weapons in service. The influence of the sampling frequency of the solution of the control problem on the stability and quality of control of the guided aviation bomb is analyzed. Based on the results of modeling the longitudinal motion of the guided aviation bomb, a method for determining the optimal parameters of stabilization and control to ensure longitudinal stability of flight, as well as requirements for balancing rudder deflection, wing area and c...