An integrated method to design a spacecraft vibration protection system

Abstract

The article proposes an integrated method to design a spacecraft vibration protection system which includes the rational use and combination of well-known methods such as the method of amplitude-frequency characteristics of an oscillator, the finite element method and the machine learning method. The analysis of the effectiveness of using each method in the design of a vibration protection system is carried out, depending on the mass-dimensional and physical characteristics of spacecrafts, as well as on the levels of vibration disturbances coming to them. While developing the proposed integrated method, the limitations imposed on vibration protection systems, as well as limitations depending on the objectives of spacecrafts, are taken into account