An approach to forming the design performance of the attitude control system for small spacecraft |
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| Authors: | O. M. Alifanov Yu. G. Egorov V. M. Kul’kov V. V. Terent’ev S. O. Firsyuk |
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| Affiliation: | 1.Moscow Aviation Institute (National Research University),Moscow,Russia |
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| Abstract: | ![]()
The elements for various types of attitude control systems used in a number of small spacecraft are considered. An approach for assessment of such system effectiveness based on design requirements for spacecraft purpose and restriction in accuracy, mass and energy is proposed. |
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