Dynamic characteristics modeling of rotary platform installed on board of a small spacecraft

Abstract

Abstract The paper analyzes the capabilities of an automatic rotary platform of the "Flyuger" type to reduce micro-accelerations in a protected area when it is installed on a small spacecraft of the "Aist-2" type. The micro-accelerations field of the working volume of scientific equipment of the "Growth installation" type has been modeled. The comparison with flight test data is made. The results of the work can be used in the design of small technological spacecraft.