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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    Titel :

    Pitch-yaw-roll coupling


    Weitere Titelangaben:

    AGARD -- Report


    Beteiligte:
    Cronvich, L.L. (Autor:in) / Amsler, B.E. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1961


    Format / Umfang :

    15 pages


    Medientyp :

    Report


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    An aerodynamic pitch-roll coupling in spinning vehicles.

    COVERT, E. E. / VLAJINAC, M. | AIAA | 1969


    Rotorcraft Pitch-Roll Cross Coupling Evaluation for Aggressive Tracking Manoeuvering

    Pausder, H. J. / Blanken, C. L. / Associazione Italiana di Aeronautica ed Astronautica et al. | British Library Conference Proceedings | 1993


    In-flight simulation investigation of rotorcraft pitch-roll cross coupling

    Watson, Douglas C. / Hindson, William S. | NTRS | 1988


    Nonlinear Coupling of Pitch and Roll Modes in Ship Motions

    All H. Nayfeh / Dean T. Mook / Larry R. Marshall | AIAA | 1973


    NATURAL PITCH AND ROLL

    KHRIPIN ALEX / RIZZI ALFRED ANTHONY | Europäisches Patentamt | 2023

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