Study is concerned with angular motion of rigid axisymmetrical body having thrust malalignment and another moment due to deflection of control surfaces or control jets; in linear feedback system which is used in control of spin-stabilized space vehicle, preferable combinations of control parameters, such as feedback gain, spin rate, feedback phase difference and damping of system, are obtained to optimize stability and control of vehicle.


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    Titel :

    Linear dynamic analysis of spinning axisymmetrical rocket or vehicle


    Weitere Titelangaben:

    Tokyo. Univ -- Inst Space Aeronautical Science -- Report


    Beteiligte:
    Azuma, A. (Autor:in)


    Erscheinungsdatum :

    1965


    Format / Umfang :

    57 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :