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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| Institution: | 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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