Determination of attitude of rocket with progressive method, using only two vectors of reference; in Pt 1 of paper, it is shown how it is possible to determine progressively attitude of rocket with only 3 magnetic aspect sensors; in Pt 2, supplementary information, given by solar cell, is introduced.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Determination of attitude of rocket with progressive method, using only two vectors of reference


    Additional title:

    Determination de l'attitude d'une fusee par une methode progressive utilisant deux vecteurs de reference


    Contributors:
    Bertin, F. (author)

    Published in:

    Astronautica Acta ; 9 , n 5-6 ; p 371-384


    Publication date :

    1963


    Size :

    14 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    French






    Satellite Attitude Determination Using Magnetometer Data Only

    Hart, C. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 2009



    Angles Only Three-Axis Attitude Determination

    Tanygin, S. / American Institute of Aeronautics and Astronautics; American Astronautical Society | British Library Conference Proceedings | 2010