Controof the orientation of aircraft and spacecraft by one rotation around an axis has the best potential possibilities by comparison with the usually used three successive rotations with respect to the orthogonal axes connected to the vehicle. This article contains an analytical solution of the problem of synthesizing the orientation control algorithm. (Author)


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    Titel :

    Analytical Solution of the Problem of Controlling a Spatial Turning Maneuver


    Beteiligte:
    B. N. Petrov (Autor:in) / V. A. Bodner (Autor:in) / K. B. Alekseev (Autor:in)

    Erscheinungsdatum :

    1970


    Format / Umfang :

    9 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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