Method of predictive studies of the effectiveness of spacecraft modifications with integrated subsystem replacement

Abstract

The article reviews application features of the method of bilevel coordinated optimization of spacecraft modification parameters during integrated replacement of subsystems. The algorithm for problem solution is presented in the article. It is shown that in the case of implementation of a balanced bilevel schematic of optimization search, the agreement of project solutions for spacecraft modification is provided by integrated replacement of subsystems. Project models are shown for the problem solution of optimization parameters for spacecraft modification with the integrated replacement of subsystems of the payload equipment module and a unified space platform.