Abstract
Some questions related with designing of software for on-board computer in control loop are considered. Software consists of several procedures corresponding to control tasks: navigation, guidance and orientation and also it includes control laws (algorithms) of measurement and executive subsystems. Implementations of suggested procedures and approaches are given. Detailed simulation both time processes of spacecraft dynamics and inner processes of computer having its own operating system is used as an analysis instrument of overall performance. Some results of investigation are given.
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