Design principles of control and management system for satellites usage.

Аuthors

Kravchuk S. V.^1*, Shatsky M. A.¹, Kovalev A. Y.^2**

1. Moscow Experimental Design Bureau “Mars”, 1-st Shemilovsky lane 16, building 2, Moscow, 127473, Russia
2. Moscow Aviation Institute (National Research University), 4, Volokolamskoe shosse, Moscow, А-80, GSP-3, 125993, Russia

*e-mail: otdel246.mars@mail.ru
**e-mail: alexeykoval@gmail.com

Abstract

Principles of software design for hierarchical satellite control and management system are described in the article. The created system coordinates the operations of different subsystems of satellite (stabilization, navigation and other subsystems) in order to accomplish the target satellite function on different periods of flight and operations (goal satellite purpose, orbit correction, failure counter etc.). The described principles are invented in satellite control systems produced in MOKB MARS

Keywords:

Satellite; control and management system; spacecraft computer system

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