The formation of the target function in the design of a small spacecraft for technological purposes

Abstract

Abstract The paper deals with the issues of forming and minimizing the target function in the process of creating a small spacecraft for technological purposes. The main difference between such a spacecraft is the need to meet specific requirements for micro-accelerations. These requirements provide favorable conditions for the implementation of gravity-sensitive processes on board a small spacecraft. The constructed objective function allowed us to determine the design appearance of a small spacecraft for technological purposes. The results of the work can be used in the design of small spacecraft.