By means of 3 magnetic aspect sensors, aspect of rocket can be computed for whole flight; as example, computation is exposed for Veronique rocket V 27; comparison of results with data given by instruments on board of V 27 shows excellent agreement; rocket remained nose up during all flight, until re-entry in dense layers (45 km); after some wavering, axis is placed on its precession cone; roll is about 55 rpm.


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    Titel :

    Results of measurements of attitude of rocket "Veronique" by magnetic means


    Weitere Titelangaben:

    Resultats concernant l'attitude d'une fusee Veronique obtenus au moyen de capteurs magnetiques


    Beteiligte:
    Israel, G. (Autor:in) / Vassy, A. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1962


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Französisch


    Schlagwörter :





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    R. A. Boudreaux / F. G. Etheridge | NTIS | 1966


    Application of Adaptive Control - Sounding Rocket Attitude

    Leite Filho, W. C. / International Federation of Automatic Control / Beijing Institute of Control Engineering | British Library Conference Proceedings | 1997