One significant coupling problem in missile experience is that which results from interaction between pitch, yaw and roll modes of motion; geometric, aerodynamic and control system couplings and their mutual interactions which give rise to overall system stability problems are considered; supersonic aerodynamic static stability and control characteristics of configuration which experiences aerodynamic coupling in attitude and in control are discussed; functional block diagram of missile steering and roll control system.


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    Title :

    Pitch-yaw-roll coupling


    Additional title:

    AGARD -- Report


    Contributors:

    Published in:

    Publication date :

    1961


    Size :

    15 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English




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