We present algorithms for attitude guidance and economical digital control of an information satellite at initial modes – during from its separation from a launcher rocket up to its regular attitude stabilization in orbital reference frame. We represent the computer simulation results on the initial orientation modes of a land-survey satellite on sun-synchronous orbit.


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    Titel :

    Spacecraft attitude guidance and economical digital control in initial modes


    Beteiligte:
    Somova, Tatyana (Autor:in) / Sivasundaram, Seenith (Herausgeber:in)

    Kongress:

    ICNPAA 2018 WORLD CONGRESS: 12th International Conference on Mathematical Problems in Engineering, Aerospace and Sciences ; 2018 ; Yerevan, Armenia


    Erschienen in:

    Erscheinungsdatum :

    04.12.2018


    Format / Umfang :

    7 pages





    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch





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    Sorensen, A.A. / Elbert, J.D. / Wheeler, P.C. | Tema Archiv | 1972


    spacecraft digital attitude control

    Sorensen, A. / Elbert, J. / Wheeler, P. | Tema Archiv | 1972