This paper presents the single-axis angular motion equations of a large space structure
assembled in orbit from separate elastic construction elements. We introduce a method to
calculate the parameters of discretely varying dynamical properties of an assembled structure
whose model has variable coefficients and inherent attributes of an elastic multi-frequency vibrating
system. In addition, we suggest a parametrically tuneable algorithm for powered gyro
control of such objects that guarantees desired dynamics at all steps of robotized assembly.
Simulation results demonstrate the efficiency of the suggested algorithm.