The problems of attitude control of a Skylark rocket are considered on the specific occasion of a night flight during which, of course, the sun was not available as a pointing vector. Pointing was achieved using magnetometers, while roll control was obtained using a suitably placed moon sensor. The logical sequence, as well as the electronic solution, that insured the acquisition of the correct payload orientation is presented.


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    Titel :

    Attitude Control of a Skylark Rocket Using Magnetometers and a Moon Sensor


    Beteiligte:
    Janes, A.F. (Autor:in) / Smith, A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1978-11-01


    Format / Umfang :

    973154 byte




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch