Methodology and practical application of the automation system for unmanned spacecraft design

The problem of automation of design of automatic spacecraft structures taking into account their dynamic characteristics are considered. According to the results of the research, the procedure of unification of the method of automatic formation of stiffness and inertia matrices of complex spatial structure is proposed. The procedure based on the transfer functions method allows to determine the level of loads of a certain type. The proposed approach shows the best results in bench tests of automatic spacecraft structures and can be used to calculate complex mechanical systems of machines and assemblies for various purposes.