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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    Titel :

    An approach to forming the design performance of the attitude control system for small spacecraft


    Beteiligte:
    Alifanov, O. M. (Autor:in) / Egorov, Yu. G. (Autor:in) / Kul’kov, V. M. (Autor:in) / Terent’ev, V. V. (Autor:in) / Firsyuk, S. O. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    2015-10-01


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




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