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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    Title :

    Linear dynamic analysis of spinning axisymmetrical rocket or vehicle


    Additional title:

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


    Contributors:
    Azuma, A. (author)


    Publication date :

    1965


    Size :

    57 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :