Investigating the dynamic model of the flying object on the elastic background

Abstract

In the article, the dynamic model of the launcher on elastic ground is established using the Lagrange II equation. Using this model for the configuration of the airborne device launcher, the oscillation laws of the movements of the launch platform are determined. This allows for the assessment of the launcher’s oscillation on elastic ground during firing, serving as a basis for the design calculations of several structural components of the launcher, optimizing the firing for a class of launchers with the same structural principles and launching mechanisms.